Перевод: со всех языков на английский

с английского на все языки

developed fuel

  • 1 выдача горючего

    Русско-английский военно-политический словарь > выдача горючего

  • 2 испарение горючего

    Русско-английский военно-политический словарь > испарение горючего

  • 3 клапан горючего

    Русско-английский военно-политический словарь > клапан горючего

  • 4 скопление горючего

    Авиация и космонавтика. Русско-английский словарь > скопление горючего

  • 5 бак горючего

    Авиация и космонавтика. Русско-английский словарь > бак горючего

  • 6 совершивший посадку из-за нехватки горючего

    Авиация и космонавтика. Русско-английский словарь > совершивший посадку из-за нехватки горючего

  • 7 бак для пускового горючего

    Авиация и космонавтика. Русско-английский словарь > бак для пускового горючего

  • 8 созданный вид топлива

    1) Atomic energy: newly developed fuel (контекстуальный перевод на англ. язык)
    2) Nuclear physics: newly developed fuel type

    Универсальный русско-английский словарь > созданный вид топлива

  • 9 разработанный вид топлива

    Универсальный русско-английский словарь > разработанный вид топлива

  • 10 Hamilton, Harold Lee (Hal)

    [br]
    b. 14 June 1890 Little Shasta, California, USA
    d. 3 May 1969 California, USA
    [br]
    American pioneer of diesel rail traction.
    [br]
    Orphaned as a child, Hamilton went to work for Southern Pacific Railroad in his teens, and then worked for several other companies. In his spare time he learned mathematics and physics from a retired professor. In 1911 he joined the White Motor Company, makers of road motor vehicles in Denver, Colorado, where he had gone to recuperate from malaria. He remained there until 1922, apart from an eighteenth-month break for war service.
    Upon his return from war service, Hamilton found White selling petrol-engined railbuses with mechanical transmission, based on road vehicles, to railways. He noted that they were not robust enough and that the success of petrol railcars with electric transmission, built by General Electric since 1906, was limited as they were complex to drive and maintain. In 1922 Hamilton formed, and became President of, the Electro- Motive Engineering Corporation (later Electro-Motive Corporation) to design and produce petrol-electric rail cars. Needing an engine larger than those used in road vehicles, yet lighter and faster than marine engines, he approached the Win ton Engine Company to develop a suitable engine; in addition, General Electric provided electric transmission with a simplified control system. Using these components, Hamilton arranged for his petrol-electric railcars to be built by the St Louis Car Company, with the first being completed in 1924. It was the beginning of a highly successful series. Fuel costs were lower than for steam trains and initial costs were kept down by using standardized vehicles instead of designing for individual railways. Maintenance costs were minimized because Electro-Motive kept stocks of spare parts and supplied replacement units when necessary. As more powerful, 800 hp (600 kW) railcars were produced, railways tended to use them to haul trailer vehicles, although that practice reduced the fuel saving. By the end of the decade Electro-Motive needed engines more powerful still and therefore had to use cheap fuel. Diesel engines of the period, such as those that Winton had made for some years, were too heavy in relation to their power, and too slow and sluggish for rail use. Their fuel-injection system was erratic and insufficiently robust and Hamilton concluded that a separate injector was needed for each cylinder.
    In 1930 Electro-Motive Corporation and Winton were acquired by General Motors in pursuance of their aim to develop a diesel engine suitable for rail traction, with the use of unit fuel injectors; Hamilton retained his position as President. At this time, industrial depression had combined with road and air competition to undermine railway-passenger business, and Ralph Budd, President of the Chicago, Burlington \& Quincy Railroad, thought that traffic could be recovered by way of high-speed, luxury motor trains; hence the Pioneer Zephyr was built for the Burlington. This comprised a 600 hp (450 kW), lightweight, two-stroke, diesel engine developed by General Motors (model 201 A), with electric transmission, that powered a streamlined train of three articulated coaches. This train demonstrated its powers on 26 May 1934 by running non-stop from Denver to Chicago, a distance of 1,015 miles (1,635 km), in 13 hours and 6 minutes, when the fastest steam schedule was 26 hours. Hamilton and Budd were among those on board the train, and it ushered in an era of high-speed diesel trains in the USA. By then Hamilton, with General Motors backing, was planning to use the lightweight engine to power diesel-electric locomotives. Their layout was derived not from steam locomotives, but from the standard American boxcar. The power plant was mounted within the body and powered the bogies, and driver's cabs were at each end. Two 900 hp (670 kW) engines were mounted in a single car to become an 1,800 hp (l,340 kW) locomotive, which could be operated in multiple by a single driver to form a 3,600 hp (2,680 kW) locomotive. To keep costs down, standard locomotives could be mass-produced rather than needing individual designs for each railway, as with steam locomotives. Two units of this type were completed in 1935 and sent on trial throughout much of the USA. They were able to match steam locomotive performance, with considerable economies: fuel costs alone were halved and there was much less wear on the track. In the same year, Electro-Motive began manufacturing diesel-electrie locomotives at La Grange, Illinois, with design modifications: the driver was placed high up above a projecting nose, which improved visibility and provided protection in the event of collision on unguarded level crossings; six-wheeled bogies were introduced, to reduce axle loading and improve stability. The first production passenger locomotives emerged from La Grange in 1937, and by early 1939 seventy units were in service. Meanwhile, improved engines had been developed and were being made at La Grange, and late in 1939 a prototype, four-unit, 5,400 hp (4,000 kW) diesel-electric locomotive for freight trains was produced and sent out on test from coast to coast; production versions appeared late in 1940. After an interval from 1941 to 1943, when Electro-Motive produced diesel engines for military and naval use, locomotive production resumed in quantity in 1944, and within a few years diesel power replaced steam on most railways in the USA.
    Hal Hamilton remained President of Electro-Motive Corporation until 1942, when it became a division of General Motors, of which he became Vice-President.
    [br]
    Further Reading
    P.M.Reck, 1948, On Time: The History of the Electro-Motive Division of General Motors Corporation, La Grange, Ill.: General Motors (describes Hamilton's career).
    PJGR

    Biographical history of technology > Hamilton, Harold Lee (Hal)

  • 11 Ricardo, Sir Harry Ralph

    [br]
    b. 26 January 1885 London, England
    d. 18 May 1974 Graffham, Sussex, England
    [br]
    English mechanical engineer; researcher, designer and developer of internal combustion engines.
    [br]
    Harry Ricardo was the eldest child and only son of Halsey Ricardo (architect) and Catherine Rendel (daughter of Alexander Rendel, senior partner in the firm of consulting civil engineers that later became Rendel, Palmer and Tritton). He was educated at Rugby School and at Cambridge. While still at school, he designed and made a steam engine to drive his bicycle, and by the time he went up to Cambridge in 1903 he was a skilled craftsman. At Cambridge, he made a motor cycle powered by a petrol engine of his own design, and with this he won a fuel-consumption competition by covering almost 40 miles (64 km) on a quart (1.14 1) of petrol. This brought him to the attention of Professor Bertram Hopkinson, who invited him to help with research on turbulence and pre-ignition in internal combustion engines. After leaving Cambridge in 1907, he joined his grandfather's firm and became head of the design department for mechanical equipment used in civil engineering. In 1916 he was asked to help with the problem of loading tanks on to railway trucks. He was then given the task of designing and organizing the manufacture of engines for tanks, and the success of this enterprise encouraged him to set up his own establishment at Shoreham, devoted to research on, and design and development of, internal combustion engines.
    Leading on from the work with Hopkinson were his discoveries on the suppression of detonation in spark-ignition engines. He noted that the current paraffinic fuels were more prone to detonation than the aromatics, which were being discarded as they did not comply with the existing specifications because of their high specific gravity. He introduced the concepts of "highest useful compression ratio" (HUCR) and "toluene number" for fuel samples burned in a special variable compression-ratio engine. The toluene number was the proportion of toluene in heptane that gave the same HUCR as the fuel sample. Later, toluene was superseded by iso-octane to give the now familiar octane rating. He went on to improve the combustion in side-valve engines by increasing turbulence, shortening the flame path and minimizing the clearance between piston and head by concentrating the combustion space over the valves. By these means, the compression ratio could be increased to that used by overhead-valve engines before detonation intervened. The very hot poppet valve restricted the advancement of all internal combustion engines, so he turned his attention to eliminating it by use of the single sleeve-valve, this being developed with support from the Air Ministry. By the end of the Second World War some 130,000 such aero-engines had been built by Bristol, Napier and Rolls-Royce before the piston aero-engine was superseded by the gas turbine of Whittle. He even contributed to the success of the latter by developing a fuel control system for it.
    Concurrent with this was work on the diesel engine. He designed and developed the engine that halved the fuel consumption of London buses. He invented and perfected the "Comet" series of combustion chambers for diesel engines, and the Company was consulted by the vast majority of international internal combustion engine manufacturers. He published and lectured widely and fully deserved his many honours; he was elected FRS in 1929, was President of the Institution of Mechanical Engineers in 1944–5 and was knighted in 1948. This shy and modest, though very determined man was highly regarded by all who came into contact with him. It was said that research into internal combustion engines, his family and boats constituted all that he would wish from life.
    [br]
    Principal Honours and Distinctions
    Knighted 1948. FRS 1929. President, Institution of Mechanical Engineers 1944–5.
    Bibliography
    1968, Memo \& Machines. The Pattern of My Life, London: Constable.
    Further Reading
    Sir William Hawthorne, 1976, "Harry Ralph Ricardo", Biographical Memoirs of Fellows of the Royal Society 22.
    JB

    Biographical history of technology > Ricardo, Sir Harry Ralph

  • 12 gas combustible

    (n.) = fuel gas
    Ex. In the far term novel techniques are being developed to remove carbon dioxide from fuel gas or flue gas from energy conversion systems.
    * * *
    (n.) = fuel gas

    Ex: In the far term novel techniques are being developed to remove carbon dioxide from fuel gas or flue gas from energy conversion systems.

    Spanish-English dictionary > gas combustible

  • 13 Siemens, Sir Charles William

    [br]
    b. 4 April 1823 Lenthe, Germany
    d. 19 November 1883 London, England
    [br]
    German/British metallurgist and inventory pioneer of the regenerative principle and open-hearth steelmaking.
    [br]
    Born Carl Wilhelm, he attended craft schools in Lübeck and Magdeburg, followed by an intensive course in natural science at Göttingen as a pupil of Weber. At the age of 19 Siemens travelled to England and sold an electroplating process developed by his brother Werner Siemens to Richard Elkington, who was already established in the plating business. From 1843 to 1844 he obtained practical experience in the Magdeburg works of Count Stolburg. He settled in England in 1844 and later assumed British nationality, but maintained close contact with his brother Werner, who in 1847 had co-founded the firm Siemens \& Halske in Berlin to manufacture telegraphic equipment. William began to develop his regenerative principle of waste-heat recovery and in 1856 his brother Frederick (1826–1904) took out a British patent for heat regeneration, by which hot waste gases were passed through a honeycomb of fire-bricks. When they became hot, the gases were switched to a second mass of fire-bricks and incoming air and fuel gas were led through the hot bricks. By alternating the two gas flows, high temperatures could be reached and considerable fuel economies achieved. By 1861 the two brothers had incorporated producer gas fuel, made by gasifying low-grade coal.
    Heat regeneration was first applied in ironmaking by Cowper in 1857 for heating the air blast in blast furnaces. The first regenerative furnace was set up in Birmingham in 1860 for glassmaking. The first such furnace for making steel was developed in France by Pierre Martin and his father, Emile, in 1863. Siemens found British steelmakers reluctant to adopt the principle so in 1866 he rented a small works in Birmingham to develop his open-hearth steelmaking furnace, which he patented the following year. The process gradually made headway; as well as achieving high temperatures and saving fuel, it was slower than Bessemer's process, permitting greater control over the content of the steel. By 1900 the tonnage of open-hearth steel exceeded that produced by the Bessemer process.
    In 1872 Siemens played a major part in founding the Society of Telegraph Engineers (from which the Institution of Electrical Engineers evolved), serving as its first President. He became President for the second time in 1878. He built a cable works at Charlton, London, where the cable could be loaded directly into the holds of ships moored on the Thames. In 1873, together with William Froude, a British shipbuilder, he designed the Faraday, the first specialized vessel for Atlantic cable laying. The successful laying of a cable from Europe to the United States was completed in 1875, and a further five transatlantic cables were laid by the Faraday over the following decade.
    The Siemens factory in Charlton also supplied equipment for some of the earliest electric-lighting installations in London, including the British Museum in 1879 and the Savoy Theatre in 1882, the first theatre in Britain to be fully illuminated by electricity. The pioneer electric-tramway system of 1883 at Portrush, Northern Ireland, was an opportunity for the Siemens company to demonstrate its equipment.
    [br]
    Principal Honours and Distinctions
    Knighted 1883. FRS 1862. Institution of Civil Engineers Telford Medal 1853. President, Institution of Mechanical Engineers 1872. President, Society of Telegraph Engineers 1872 and 1878. President, British Association 1882.
    Bibliography
    27 May 1879, British patent no. 2,110 (electricarc furnace).
    1889, The Scientific Works of C.William Siemens, ed. E.F.Bamber, 3 vols, London.
    Further Reading
    W.Poles, 1888, Life of Sir William Siemens, London; repub. 1986 (compiled from material supplied by the family).
    S.von Weiher, 1972–3, "The Siemens brothers. Pioneers of the electrical age in Europe", Transactions of the Newcomen Society 45:1–11 (a short, authoritative biography). S.von Weihr and H.Goetler, 1983, The Siemens Company. Its Historical Role in the
    Progress of Electrical Engineering 1847–1980, English edn, Berlin (a scholarly account with emphasis on technology).
    GW

    Biographical history of technology > Siemens, Sir Charles William

  • 14 вес


    weight (wt)
    - без топлива (ла) — zero fuel weight
    - брутто — gross weight
    - в зависимости от высоты (давления) и температуры на аэродроме, максимальный (допустимый) взлетный (параграф разд. 5 рлэ) — takeoff weight-altitude-temperature (wat) curves the wat curves should be provided which limit the weight to an extent necessary to ensure compliance with the airworthiness climb requirements appropriate to takeoff.
    - в зависимости от высоты (давления) и температуры на аэродроме, максимальный (допустимый) взлетный (надпись к графику разд. 5 рлэ) — maximum takeoff weight for altitude and temperature the curves should be drawn having the altitude of the airdrome as the ordinate and airplane weight as abscissa, with lines of constant temperature.
    - в зависимости от высоты (давления) и температуры на аэродроме, максимальный (допустимый) посадочный (параграф разд. 5 рлэ) — landing weight-altitude-temperature (wat) curves the curves should be drawn to the same specification as for the takeoff wat curves.
    - в зависимости от высоты (давления) и температуры на аэродроме, максимально (допустимый) посадочный (график к разд. 5 рлэ) — maximum landing weight for altitude and temperature the graph title should be "maximum landing weight for altitude and temperature".
    -, взлетный — takeoff weight
    - в тысячах кг (на графике) — weight - thousands of kg
    -, выбранный заявителем — weight selected by the applicant
    -, гарантированный — guaranteed weight
    - десантной нагрузки — air delivery load weight
    - загруженного самолета, без топлива, максимальный — maximum zero fuel operational weight
    - заправляемого топлива, максимальный (в кг) — maximum fuel load weight
    - из условия располагаемой энергоемкости тормозов (колес), максимально допустимый взлетный — maximum allowable takeoff weight restricted /permitted/ by brake kinetic energy absorption (capacity)
    -, завышенный (напр. при посадке) — overweight
    -, максимальный взлетный — maximum takeoff weight
    -, максимально допустимый взлетный — maximum allowable takeoff weight
    -, максимальный посадочный — maximum landing weight
    -, максимальный расчетный полетный — maximum design flight weight (mfw)
    максимальный расчетный вес, ограниченный условиями прочности ла и другими требованиями летной годности. — the maximum weight for flight as limited by aircraft strength and other airworthiness requirements.
    -, максимальный (расчетный) рулежный — maximum (design) taxi weight
    максимальный предвзлетный вес ла, включающий вес топлива на выруливание и опробование двигателей. — the maximum weight allowed for ground maneuver includes weight of taxi and run-up fuel.
    -, максимальный сертифицированный (установленный в соответствии с нормами летной годности) — maximum certificate(d) weight maximum certificate weights are determined in accordance with the airworthiness requirements.
    -, маршрутный (полетный) — en-route weight
    -, минимальный — minimum weight
    -, наибольший — highest weight
    -, наименьший — lowest weight
    - начала перекачки топлива, максимальный расчетный — maximum design fuel transfer weight (mftw)
    -, ограниченный заявителем, наибольший — highest weight selected by the applicant
    -, ограниченный по набору высоты, максимально допустимый взлетный — maximum allowable takeoff weight restricted /permitted/ by climb performance
    -, ограниченный по набору высоты при уходе на второй круг, максимально допустимый посадочный — maximum allowable landing weight restricted by climb performance during go-around (сша)

    maximum landing weight permitted by balked landing climb performance (англ.)
    -, ограниченный располагаемой длиной впп, максимально допустимый посадочный — maximum allowable landing weight permitted by landing field length available
    -, ограниченный располагаемой энергоемкостью колес (тормозов), максимально допустимый взлетный — maximum allowable takeoff weight restricted /permitted/ by brake kinetic energy absorption capacity
    -, ограниченный скоростью вращения колес максимально допустимый взлетный — maximum allowable takeoff weight restricted by tire speed
    - перегрузочный — overload weight, overweight
    - по формуляру — logged weight, weight specified in log book
    - полезной нагрузки — useful load weight
    -, полетный (в рлэ, на графиках) — gross weight (gw)
    -, полетный (по британским нормам летной годности bcar) — en-route weight
    - полной нагрузки (вес экипажа, топлива и полезной нагрузки) — full load weight
    -, посадочный (нормальный) — landing weight
    - предельный — maximum weight
    - предельный, взлетный — maximum takeoff weight
    - предельный /полный/ полетный — gross weight
    - при начальном наборе высоты — climbout weight
    -, приведенный взлетный — factored takeoff weight
    - пустого самолета — empty weight
    - пустого самолета, базовый — basic empty weight (bew)
    - пустого самолета в состоянии поставки — delivery empty weight (dew) manufacturer's empty weight less any shortages, plus those standard items and operational items in aircraft at time of delivery.
    - пустого самолета, основной — basic empty weight (bew) standard basic empty weight plus or minus weight of standard item variations.
    - пустого самолета, производственный — manufacturer's empty weight (mew)
    вес конструкции, силовой установки, систем и оборудования, которые являются составной частью конкретного ла. — the weight of the structure, powerplant, furnishings, systems and other items of equipment that are considered an integral part of a particular aircraft configuration.
    - пустого самолета с полным снаряжением — operational empty weight
    - пустого снаряженного самолета — operational empty weight (oew)

    basic empty weight or fleet empty weight plus operational items.
    -, расчетный — design weight
    -, расчетный взлетный — design takeoff weight
    -, расчетный полетный — (maximum) design flight weight
    -, расчетный посадочный — design landing weight
    -, рулежный — taxi weight,
    - самолета (обозначение оси графика изменения веса в полете) — gross /en-route/ weight
    - самолета без топлива — zero fuel weight
    -, сертифицированный — certificate(d) weight
    -, скорректированный — corrected weight
    - служебной нагрузки — weight of standard items
    - снаряжения самолета (с экипажем и бортпроводниками) — weight of (aircraft) operational items
    - снаряженного самолета — operational weight
    - снаряженного самолета, взлетный — operational takeoff weight (otow)
    - снаряженного самолета, посадочный — operational landing weight (olw)
    - (самолета) с полным снаряжением (со снаряжением) — operational weight
    -, стандартный — standard weight
    -, сухой — dry weight
    вес двигателя с установленными агрегатами, без охлаждающей жидкости, масла и топлива — the weight of an engine exclusive of fuel, oil, and liquid coolant.
    - тары — tare weight
    -, транспортировочный — shipping weight
    -, удельный — specific gravity
    - удельный, топлива — fuel specific gravity
    - установленный (для конкретных условий, ограничений) — authorized weight (for takeoff or landing)
    -, чистый — net weight
    -, эксплуатационный (ла) — operational weight
    выигрыш в в. — saving of weight
    избыток в. — excess weight
    по в. — by weight
    %-ный раствор по в. — % by weight solution
    под своим в. — due to own weight
    клапан свободно входит в гильзу под действием своего веса. — the valve drops freely into the sleeve due to its own weight.
    при любом в. — at any weight
    разбивка в. (ла на составляющие: вес конструкции, топлива, снаряжения и т.д.) — weight breakdown
    выигрывать в в. — save weight
    проигрывать в в. — have weight penalty
    уменьшать в. — reduce weight
    химическое фрезерование и сотовые конструкции применяются для уменьшения веса самолета. — chemical milling and honeycomb construction are techniques developed to reduce the aircraft weight.
    увеличивать в. — increase weight

    Русско-английский сборник авиационно-технических терминов > вес

  • 15 нагрузка


    load
    - (нервно-психическая и физическая) — workload
    -, асимметричная — unsymmetrical load
    асимметричная нагрузка на самолет может возникнуть при отказе критического двигателя. — the airplane must be designed for unsymmetrical loads resulting from the failure of the critical engine.
    -, аэродинамическая — aerodynamic load
    -, безопасная — safe load
    -, боковая — side load
    для случая боковой нагрузки предполагается что самолет находится в горизонтальном положении при условии касания земли только колесами основных опор. — for the side load condition, the airplane is assumed to be in the level attitude with only the main wheels contacting the ground.
    -, вертикальная — vertical load
    -, вибрационная — vibration load
    -, воздушная — air load
    -, вызванная отказом двигателя, асимметричная — unsymmetrical load due to engine failure
    - генератора — generator load
    -, гидравлическая — hydraulic load
    -, гироскопическая — gyroscopic load
    -, десантная — air-delivery load
    -, десантная (парашютная) — paradrop load
    -, динамическая — dynamic load
    нагрузка, возникающая при воздействии положительного (ипи отрицательного) ускорения на конструкцию ла. — any load due to acceleration (or deceleration) of an aircraft, and therefore proportional to its mass.
    -, динамическая, при полном вытягивании строп парашюта до наполнения купола — (parachute) deployment shock load the load which occurs when the rigging lines become taut prior to inflation of the canopy.
    -, динамическая, при раскрытии купола парашюта — (parachute) opening shock load

    maximum load developed during rapid inflation of the canopy.
    -, длительная — permanent load
    -, допускаемая прочностью самолета — load not exceeding airplane structural limitations
    -, допустимая — allowable load
    -, знакопеременная — alternate load
    -, индуктивная (эл.) — inductive load
    -, инерционная — inertia load
    -, коммерческая bес пассажиров, груза и багажа. — payload (p/l) weight of passengers, cargo, and baggage.
    - коммерческая, располагаемая — payload available
    -, максимальная коммерческая — maximum payload
    разность между максимальным расчетным весом без топлива и весом пустого снаряженного ла. — maximum design zero fuel weight minus operational empty weight.
    -, максимальная предельная радиальная (на колесо) — maximum radial limit load (rating of each wheel)
    -, максимальная статическая (на колесо) — maximum static load (rating of each wheel)
    -, маневренная — maneuvering load
    -, минимальная расчетная — minimum design load
    при определении минимальных расчетных нагрузок необходимо учитывать влияние возможных усталостных нагрузок и нагрузок от трения и заклинивания. — the minimum design loads must provide а rugged system for service use, including consideration of fatigua, jamming and friction loads.
    -, моментная (напр. поворотного срезного болта водила) — torque load
    - на вал (ротор) — shaft (rotor) load
    - на генератор — generator load
    - на гермокабину (от избыточного давления) — pressurized cabin pressure differential load
    конструкция самолета допжна выдерживать полетные нагрузки в сочетании с нагрузками от избыточного давления в гермокабине. — the airplane structure must be strong enough to withstand the flight loads combined with pressure differential loads.
    - на двигатель — power load on engine

    prevent too sudden and great power load being thrown on the engine.
    - на единицу площади — load per unit area
    - на колесо — wheel load
    - на колонку (или штурвал, ручку) при продольном yправлении — elevator pressure (felt when deflecting control column (wheel or stick)
    - на конструкцию, выраженная в единицах ускорения (статическая и динамическая) — (static and dynamic) loads on structure expressed in g units
    - на крыло, удельная — wing loading
    часть веса самолета, приходящаяся на единицу поверхности крыла и равная частномy от деления полетного веса самолета на площадь крыла. — wing loading is gross weight of aeroplane divided by gross wing area.
    - на лопасть, удельная — blade loading
    - на мотораму — load on engine mount
    - на мотораму, боковая — side load on engine mount
    - на мощность, удельная часть веса самолета, приходящаяся на единицу силы тяги, развиваемой его силовой установкой при нормальном режиме работы. — power loading the gross weight of an aircraft divided by the horsepower of the engine(s).
    - на орган управления (усилие) — control pressure
    - на орган управления, пропорциональная величине отклонения поверхности управнения — control pressure proportional to amount of control surface deflection
    - на орган управления (штурвал, колонку, ручку управления, педали), создаваемая загрузочным механизмом — control pressure created by feel unit /or spring/
    - на орган управления (штурвал, колонку или педали), создаваемая отклоняемой поверхностью управления — control pressure created by control surface
    - на педали при путевом управлении — rudder pressure (felt when deflecting pedals)
    - на площадь, сметаемую несущим винтом — rotor disc loading
    величина подъемной силы (тяги) несущего винта, деленная на площадь ометаемую винтом. — the thrust of the rotor divided by the rotor disc area.
    - на поверхность управления — control surface load, backpressure on control surface
    - на поверхность управления от порыва ветра — control surface gust load
    - на поверхность управления, удельная — control surface loading the mean normal force per unit area carried by an aerofoil.
    - на пол — floor load
    - на пол, удельная — floor loading
    -, направленная к продольной оси самолета, боковая — inward acting side load
    -, направленная от продольной оси самолета, боковая — outward acting side load
    - на размах, удельная — span loading
    полетный вес самолета, деленный на квадрат размаха крыла. — the gross weight of an airplane divided by the square of the span.
    - на растяжение — tensile load /stress, strain/
    - на руль высоты (усилие при отклонении) — backpressure on elevator
    - на руль направления (усилие при отклонении) — backpressure on rudder
    - на сжатие — compression load
    - на систему управления — control system load
    максимальные и минимальные усилия летчика, прикладываемые к органам управления (в условиях полета) и передаваемые в точку крепления проводки управления к рычагу поверхности управления. — the maximum and minimum pilot forces are assumed to act at the appropriate control grips or pads (in a manner simulating flight conditions) and to be reacted at the attachment of the control system to control surface horn.
    - на скручивание — torsional load
    - на срез — shear load
    - на тягу, удельная — thrust loading
    отношение веса реактивного самолета к тяге, развиваемой его двигателем (двигателями), — the weight-thrust ratio of а jet aircraft expressed as gross weight (in kg) divided by thrust (in kg).
    - на шасси при посадке — ground load on the landing gear at touch-down
    - на шину (колеса) — load on tire
    - на штурвал (ручку) при управлении no крену — aileron pressure (felt when deflecting control wheel (or stick)
    - на элерон (усилие при отклонении) — backpressure on aileron
    -, номинальная (эл.) — rated load
    -, нормальная — normal load
    -, нормальная эксплуатационная (в системах управления) — normal operating load control system load that can be obtained in normal operation.
    -, ограниченная весом, коммерческая (платная) — weight limited payload (wlp)
    коммерческая нагрузка, oграниченная одним наиболее перечисленных ниже): — payload as restricted by the most critical of the following:
    1. взлетным весом снаряженного самолета за вычетом веса пустого снаряженного самолета и минимального запаса расходуемого топлива. — 1. operational takeoff weight minus operational empty weight minus minimum usable fuel.
    2. посадочным весом снаряженного самолета за вычетом веса пустого снаряженнаго самолета и анз топлива. — 2. operational landing weight minus operational empty weight minus flight reserve fuel.
    3. ограничениями по использованию отсеков. данная нагрузка не должна превышать макс. коммерческую нагрузку. — 3. compartment and other related limits. (it must not exceed maximum payload).
    -, ограниченная объемом, коммерческая (платная) — space limited payload (slp)
    нагрузка, ограниченная числом мест, объемными и другими пределами кабины, грузовых и багажных отсеков, — payload as restricted by seating,volumetric, and other related limits of the cabin, cargo, and baggage compartments. (it must not exceed maximum payload).
    -, омическая (эл.) — resistive load
    -, осевая — axial load
    -, основная — basic load
    - от встречного порыва (ветpa) — load resulting from encountering head-on gust
    - от заклинивания (подвижных элементов) — jamming load
    - от избыточного давления (в гермокабине) — pressure differential load
    - от порыва (ветра) — gust load
    случай нагружения конструкции самолета, особенного крыла, в результате воздействия на самолет вертикальных и горизонтальных воздушных течений (порывов), — the load condition which is imposed on an airplane, especially the wings, as a result of the airplane's flying into vertical or horizontal air currents.
    - от трения — friction load
    -, параллельная линия шарниров (узлов подвески поверхностей управления). — load parallel to (control surface) hinge line
    -, переменная (по величине) — varying load, load of variable magnitude
    -, пиковая — peak load
    -, платная (коммерческая) — payload (p/l)
    beс пассажиров, груза и багажа. — weight of passengers, cargo, and baggage.
    -, повторная — repeated load
    расчеты и испытания конструкции должны продемонстрировать ее способность выдерживать повторные переменные нагрузки возможные при эксплуатации. — the structure must be shown by analysis, tests, or both, to be able to withstand the repeated load of variable magnitude expected in service.
    -, погонная — load per unit length
    -, полезная — payload (p/l)
    вес пассажиров, груза, багажа — weight of passengers, cargo, and baggage.
    -, полезная — useful load
    разность между взлетным весом снаряженного и весом пустого снаряженного ла. (включает: коммерческую нагрузку, вырабатываемые топливо и др. жидкости, не входящие в состав снаряжения ла). — difference between operational takeoff weight and operational empty weight. (it includes payload, usable fuel, and other usable fluids not included as operational items).
    -, полетная — flight load
    отношение составляющей аэродинамической силы (действующей перпендикулярно продольной оси самолета) к весу самолета. — flight load factors represent the ratio of the aerodynamic force component (acting normal to the assumed longitudinal axis of the airplane) to the weight of the airplane.
    -, полная — full load
    включает вес экипажа, снаряжения, топлива и полезной нагрузки.
    -, постоянная — permanent load
    - предельная, разрушающая (по терминологии икао) — ultimate load
    -, продольная — longitudinal load
    -, равномерная — uniform load
    -, радиальная эксплуатационная (на каждое колесо шасcи) — radial limit load (rating of each wheel)
    -, разрушающая (расчетная) — ultimate load
    нагрузка, в результате которой возникает, или может возникнуть на основании расчетов, разрушение элемента конструкции. — the load which will, or is computed to, cause failure in any structural member.
    -, разрушающая (способная вызывать разрушение) — destructive load
    торможение может привести к появлению разрушающей нагрузки на переднее колесо. — braking can cause destructive loads on nosewheel.
    -, распределенная — distributed load
    -, рассредоточенная — distributed load
    -, расчетная — ultimate load
    расчетная нагрузка опрелеляется как произведение эксплуатационной нагрузки на коэффициент безопасности. — ultimate load is the limit load multiplied by the prescribed factor of safety.
    -, расчетная (по терминологии икао) — proof load
    -, расчетная (по усилиям в системе управления) — design load design loads are accepted in the absence of a rational analysis.
    -, скручивающая — torsional load
    -, служебная — operational items /load/
    включает экипаж, парашюты, кислородное оборудование экипажа, масло для двигателей и невырабатываемое топливо. — includes: crew, parachutes, crew's oxygen equipment, engine oil, unusable fuel.
    -, служебная (стандартная) — standard items
    служебная нагрузка может включать: нерасходуемые топливо и жидкости, масло для двигателей, огнетушители, аварийное кислородное оборудоавние, конструкции в буфете, дополнительное электронное оборудование. — may include, unusable fuel and other fluids, engine oil, toilet fluid, fire extinguishers, emergency oxygen equipment, structure in galley, buffet, supplementary electronic equipment.
    - снаряженного (самолета) — operational load
    -, сосредоточенная — concentrated load
    -, статическая — static load
    постоянно действующая нагрузка, постепенно возрастающая от нуля до своего максимума при нулевом ускорении. — а stationary load or one that is gradually increased from zero to its maximum. it is an unaccelerated basic load.
    -, суммарная — total load
    -, ударная — impact load
    -, уравновешивающая — balancing load
    -, усталостная — fatigue load
    -, фрикционная — friction load
    -, центробежная (на ротор) — centrifugal loading (on rotor)
    -, частичная — partial load
    -, чрезмерная — overload(ing)
    -, эксплуатационная — limit load
    максимальная нагрузка, воздействующая на самолет в эксплуатации, — the strength requirements are specified in terms of limit loads (the maximum loads to be expected in service).
    -, эксплуатационная нормальная (на систему управления) — normal operating load, load obtained in normal operationtained in normal operation
    -, электрическая — (electrical) load
    весовая отдача по полезной н. — useful load-to-takeoff weight ratio
    зависимость платной н. от дальности полета — payload-range curve
    под н. — under load
    при установившемся режиме работы с полной н. — at steady full-load conditions
    распределение н. — load distribution
    точка приложения н. — point of load application
    характеристика н. — load characteristic
    включать (эл.) н. — activate load
    включать (эл.) н. на генератор, (аккумулятор) — apply load to (generator, battery)
    воспринимать н. — take up load
    выдерживать н. — withstand /support/ load
    испытывать h. — be subjected to load
    нести h. — carry load
    передавать н. — transmit load
    подключать (эл.) н. к... — apply load to...
    прикладывать — apply load to...
    работать без н. (об электродвигателе, преобразователе) — run unloaded
    сбрасывать (эл.) н. — deactivate load
    снимать н. (руля высоты) — relieve elevator pressure, adjust elevator trim tab, relieve pressure by adjusting elevator trim control
    создавать (маханическую) н. — impose load on...
    устанавливать за счет платной h. — install (smth) with payload penalty

    Русско-английский сборник авиационно-технических терминов > нагрузка

  • 16 a la larga

    in the long run
    * * *
    * * *
    * * *
    = in the long term, over the long term, in the end, eventually, for the long pull, over a period of time, over the long haul, in the far term, ultimately, by and by
    Ex. For a scheme to be successfull in the long term it is vital that there should be an organisational structure to support the scheme.
    Ex. This project ought to develop over the long term from a system designed to support the exchange of entries in micro-print to a fully automated network for the processing of records.
    Ex. This is time well invested since it saves money in the end and leads to a higher success rate in providing information = Éste es tiempo bien invertido ya que ahorra dinero en última instancia y permite ofrecer una información mucho más pertinente para el usuario.
    Ex. Eventually this work on citation orders came to fruition in the rather unlikely context of a new indexing systems, PRECIS.
    Ex. Thus, the public library in this country for the next few years and for the long pull may be presented with a first-rate opportunity for greater service to its community by defining its service with reference to some qualitative standards.
    Ex. The vibration may cause the chips to work loose over a period of time, and if they have to be pushed back into their sockets, it is very easy to bend or break one of the 'legs'.
    Ex. But over the long haul you'll just find that your data is easier and cheaper to get at if you use XML.
    Ex. In the far term novel techniques are being developed to remove carbon dioxide from fuel gas or flue gas from energy conversion systems.
    Ex. Moreover, these entries must ultimately direct the searcher to his desired specific subject in the classified file.
    Ex. By and by Tom's reading and dreaming about princely life wrought such a strong effect upon him that he began to act the prince unconsciously.
    * * *
    = in the long term, over the long term, in the end, eventually, for the long pull, over a period of time, over the long haul, in the far term, ultimately, by and by

    Ex: For a scheme to be successfull in the long term it is vital that there should be an organisational structure to support the scheme.

    Ex: This project ought to develop over the long term from a system designed to support the exchange of entries in micro-print to a fully automated network for the processing of records.
    Ex: This is time well invested since it saves money in the end and leads to a higher success rate in providing information = Éste es tiempo bien invertido ya que ahorra dinero en última instancia y permite ofrecer una información mucho más pertinente para el usuario.
    Ex: Eventually this work on citation orders came to fruition in the rather unlikely context of a new indexing systems, PRECIS.
    Ex: Thus, the public library in this country for the next few years and for the long pull may be presented with a first-rate opportunity for greater service to its community by defining its service with reference to some qualitative standards.
    Ex: The vibration may cause the chips to work loose over a period of time, and if they have to be pushed back into their sockets, it is very easy to bend or break one of the 'legs'.
    Ex: But over the long haul you'll just find that your data is easier and cheaper to get at if you use XML.
    Ex: In the far term novel techniques are being developed to remove carbon dioxide from fuel gas or flue gas from energy conversion systems.
    Ex: Moreover, these entries must ultimately direct the searcher to his desired specific subject in the classified file.
    Ex: By and by Tom's reading and dreaming about princely life wrought such a
    strong effect upon him that he began to act the prince unconsciously    .

    Spanish-English dictionary > a la larga

  • 17 a largo plazo

    (adj.) = in the long term, over the long term, long-range, in the long run, long-term, over the long run, over the long haul, long-run, in the far term, far-term
    Ex. For a scheme to be successfull in the long term it is vital that there should be an organisational structure to support the scheme.
    Ex. This project ought to develop over the long term from a system designed to support the exchange of entries in micro-print to a fully automated network for the processing of records.
    Ex. In September 1973, the University of Washington initiated implementation of a formal long-range planing process for the total university system.
    Ex. Ostensibly, the maneuver was accomplished to curb patronage abuses and make it easier to dismiss deadwood employees in the long run.
    Ex. The use of agents is necessary but not ideal, because an agent often represents rival concerns, and aims for a quick turnover rather than long-term profitability.
    Ex. Some feel that these sessions can be 'self-defeating over the long run because they are based on a reward-punishment psychology that serves to intensify the pressure on the individual'.
    Ex. But over the long haul you'll just find that your data is easier and cheaper to get at if you use XML.
    Ex. Findings indicate that the short-run success of methadone programs does not automatically translate into long-run abstinence.
    Ex. In the far term novel techniques are being developed to remove carbon dioxide from fuel gas or flue gas from energy conversion systems.
    Ex. These processes can be viewed as near-term and far-term.
    * * *
    (adj.) = in the long term, over the long term, long-range, in the long run, long-term, over the long run, over the long haul, long-run, in the far term, far-term

    Ex: For a scheme to be successfull in the long term it is vital that there should be an organisational structure to support the scheme.

    Ex: This project ought to develop over the long term from a system designed to support the exchange of entries in micro-print to a fully automated network for the processing of records.
    Ex: In September 1973, the University of Washington initiated implementation of a formal long-range planing process for the total university system.
    Ex: Ostensibly, the maneuver was accomplished to curb patronage abuses and make it easier to dismiss deadwood employees in the long run.
    Ex: The use of agents is necessary but not ideal, because an agent often represents rival concerns, and aims for a quick turnover rather than long-term profitability.
    Ex: Some feel that these sessions can be 'self-defeating over the long run because they are based on a reward-punishment psychology that serves to intensify the pressure on the individual'.
    Ex: But over the long haul you'll just find that your data is easier and cheaper to get at if you use XML.
    Ex: Findings indicate that the short-run success of methadone programs does not automatically translate into long-run abstinence.
    Ex: In the far term novel techniques are being developed to remove carbon dioxide from fuel gas or flue gas from energy conversion systems.
    Ex: These processes can be viewed as near-term and far-term.

    Spanish-English dictionary > a largo plazo

  • 18 conversión de la energía

    Ex. In the far term novel techniques are being developed to remove carbon dioxide from fuel gas or flue gas from energy conversion systems.
    * * *

    Ex: In the far term novel techniques are being developed to remove carbon dioxide from fuel gas or flue gas from energy conversion systems.

    Spanish-English dictionary > conversión de la energía

  • 19 conversión energética

    Ex. In the far term novel techniques are being developed to remove carbon dioxide from fuel gas or flue gas from energy conversion systems.
    * * *

    Ex: In the far term novel techniques are being developed to remove carbon dioxide from fuel gas or flue gas from energy conversion systems.

    Spanish-English dictionary > conversión energética

  • 20 emanación tóxica

    (n.) = fume, toxic fume, flue gas, toxic emission
    Ex. The ammonia method of developing poses problems of smell and fumes.
    Ex. Nitrate film ignites readily, burns fiercely, virtually inextinguishably and with highly toxic fumes.
    Ex. In the far term novel techniques are being developed to remove carbon dioxide from fuel gas or flue gas from energy conversion systems.
    Ex. Therefore, there exists an opportunity to reduce toxic emissions by the order of 15 to 20% without substantial economic penalties.
    * * *
    (n.) = fume, toxic fume, flue gas, toxic emission

    Ex: The ammonia method of developing poses problems of smell and fumes.

    Ex: Nitrate film ignites readily, burns fiercely, virtually inextinguishably and with highly toxic fumes.
    Ex: In the far term novel techniques are being developed to remove carbon dioxide from fuel gas or flue gas from energy conversion systems.
    Ex: Therefore, there exists an opportunity to reduce toxic emissions by the order of 15 to 20% without substantial economic penalties.

    Spanish-English dictionary > emanación tóxica

Страницы

См. также в других словарях:

  • fuel injection — fuel injection, adj. the spraying of liquid fuel into the cylinders or combustion chambers of an engine. [1895 1900] * * * In an internal combustion engine, introduction of fuel into the cylinders by a pump rather than by the suction created by… …   Universalium

  • Fuel starvation — and fuel exhaustion (sometimes referred to as fuel depletion) are problems that can affect internal combustion engines fuelled by either diesel, kerosene, petroleum or any other combustible liquid or gas. If no fuel is available for an engine to… …   Wikipedia

  • Fuel saving device — Fuel saving devices are sold on the aftermarket with claims to improve the fuel economy and/or the exhaust emissions of a vehicle. There are numerous different types of device; many purport to optimize ignition, air flow, or fuel flow in some way …   Wikipedia

  • Fuel dumping — of an Airbus A340 600 above the Atlantic Ocean near Nova Scotia …   Wikipedia

  • Fuel Freedom International — is a multi level marketing company based in Altamonte Springs, Florida and co owned by Wendy Lewis and Randy Ray. It sells pills trade marked as MPG CAPS, which are engine conditioners that, it is claimed improve fuel economy, reduce emissions… …   Wikipedia

  • Fuel cell technologies — (FCT) is an Canadian fuel cell standard which is based on the IEC Standard 62282 published by the Canadian standards association.Codes and standards have repeatedly been identified as a major institutional barrier to deploying hydrogen… …   Wikipedia

  • Fuel And Sensor Tactical (FAST) Packs — are a type of Conformal Fuel Tank developed for the F 15. By carrying extra fuel in a form factor that doesn t drastically alter the aerodynamics of the fighter, they offer increased operational time without seriously degrading performance.In the …   Wikipedia

  • Fuel cell gas appliances up to 70 kW — (DVGW VP 119) is a German fuel cell standard published by the Deutsche Vereinigung des Gas und Wasserfaches in 2000. [ [http://www.fuelcellstandards.com/3.2.htm Fuel cell standards] ] copeRules for construction, functional requirements and… …   Wikipedia

  • Fuel cell — For other uses, see Fuel cell (disambiguation). Demonstration model of a direct methanol fuel cell. The actual fuel cell stack is the layered cube shape in the center of the image A fuel cell is a device that converts the chemical energy from a… …   Wikipedia

  • Fuel injection — Fuel rail connected to the injectors that are mounted just above the intake manifold on a four cylinder engine. Fuel injection …   Wikipedia

  • fuel cell — a device that produces a continuous electric current directly from the oxidation of a fuel, as that of hydrogen by oxygen. [1920 25] * * * Device that converts chemical energy of a fuel directly into electricity (see electrochemistry). Fuel cells …   Universalium

Поделиться ссылкой на выделенное

Прямая ссылка:
… Нажмите правой клавишей мыши и выберите «Копировать ссылку»