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1 прогрессивное горение
1) Astronautics: progressive burning, progressive combustion, progressive geometry2) Arms production: progressive burning (пороха)Универсальный русско-английский словарь > прогрессивное горение
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2 увеличение поверхности горения
Astronautics: burning surface augmentation, progressive geometryУниверсальный русско-английский словарь > увеличение поверхности горения
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3 крыло
wing
основное назначение крыла — wing consists of center wing,
- создание подъемной сипы, потребной для осуществления полета самолета. крыло может состоять из центраплана, средней части (счк) и отъемной части (очк). в конструкцию крыла входят лонжероны, нервюры, стрингеры, обшивка, элементы 6аков-кессонов и др. к крылу относятся закрылки, элероны, спойлеры, предкрылки. (рис. 8, 9, 10). — inner wing and outer wing structural units which enable atmosphere to lift the aircraft, integral fuel tank structure and components which make up these units such as spars, skin, ribs, stringers, clamshells, scuppers, etc, and structure of flaps, ailerons, spoilers and slats.
-, адаптивное крыло изменяемой формы, профиля. — adaptive wing
-, аэродинамическое чистое — clean wing
- бесконечного размаха — infinite-span /endless-span/ wing
крыло, рассматриваемое для упрощения в теоретической аэродинамике, без учета концевых вихрей и индуктивного лобового сопротивпемия. — in aerodynamic theory, а wing of endless span, thus having no tip vortices nor induced drag, assumed for purpose of simplification.
-, верхнее (биплана) (рис. 2) — upper wing
-, вынесенное вперед (биплана) (рис. 2) — wing with positive stagger
вынос крыла считается положительным, если верхнее крыло выступает вперед над нижним. — the stagger is positive when the upper wing is in advance of the lower.
-, высокораспопоженное — high wing
-,"гладкое" (с невыпущенной или отказавшей механизацией) — lean wing
-, двухлонжеронное — two-spar wing
- изменяемого профиля (адаптивное) — adaptive wing
- кессонной конструкции — torsion box wing
лонжероны кессона образуют отсек топливного бака, — spars of torsion box wing form integral fuel tank.
-, кольцевое (колеоптера) — annular wing
-, левое — left wing
-, летающее (самолет) — tailless airplane
- малого удлинения и сужения — stub wing
-, многолонжеронное — multispar wing
-, моноблочное — stressed-skin wing
-, неподвижное (неподвижная часть крыла при наличии пчк) — fixed wing
-, нижнее (биплана) (рис. 2) — lower wing
-, низкораспопоженное — low wing
- носовое (схемы "утка") — canard
-, однолонжеронное — single spar /monospar/ wing
-, одностоечное (биплана) — single bay wing
- оживальной формы — ogival /ogee/ wing
- (-) парасоль — parasole wing
- переднее (схемы "утка") — canard
- переменной стреловидности — variable sweep wing
-, поворотное — pivoting wing
-, поворотное (подвижная часть крыла, пчк) — pivoting wing
-, правое — right wing
-, прямоугольное — rectangular wing
- с изменяемой геометрией — variable-geometry (vg) wing
- с изменяемой площадью — variable-area wing
- с изменяемым профилем (адаптивное) — adaptive wing
- с изменяемым углом атаки — variable-incidence wing
- с изменяемым углом установки — variable-incidence wing
- с механизацией — wing with high-lift devices
- с наплывами по передней кромке — saw-tooth leading edge (le) wing
- с обратной стреловидностью — sweptforward wing, forward swept wing
- с отрицательным углом поперечного v (рис. 136) — anhedral wing
- с переменной стреловидностью — variable sweep wing
- с положительным углом поперечного v (рис. 136) — dihedral wing
- с расчалками — braced wing
- с углом стреловидности... градусов по передней кромке (рис. 8) — wing with... degrees leading edge (le) sweep
- с углом стреловидности... градусов по четвертям хорд — wing with... degrees sweep at quarter chord (or at 25 % сhord)
- с управляемым пограничным слоем — wing with boundary layer сапtrol
-, свободнонесущее — cantilever wing
крыло, установленное по принципу консольной балки, — а wing built on the principle of а cantilever beam.
-, серповидное — crescent wing
-, складывающееся — folding wing
-, среднераспопоженное — mid wing
-, стреловидное — swept wing
-, сужающееся — tapered wing
- типа "обратная чайка" — inverted-gull wing
- типа "чайка" — gull wing
-, трапецевидное — tapered wing
крыло с уменьшающейся длиной хорды от корня к законцовке. — the tapered wing has a progressive decrease in the chord length from the root to the tip.
-, треугольное — delta wing
-, трехлонжеронное — three-spar wing
заклинение к. (угол установки) — angle of wing setting, wing incidence
нагрузка на к. — wing load
неподвижная часть к. (нчк) — fixed wing (section)
обтекание к. — flow about wing
опускание к. — wing dropping
отъемная часть к. (очк) — outer wing
площадь к. — wing area
площадь к. без подфюзеляжной части — net wing area
площадь с подфюзеляжной частью — gross wing area
поверхность к. (верхняя, нижняя) — wing surface (upper, lower)
подвижная часть к. (пчк) — pivoting wing
размах к. — wing span
разъем к. — wing joint
расположение к. — wing position
средняя часть к. (счк) — inner wing
стыковка к. (к фюзеляжу) — wing attachment (to fuselage)
сужение к. — wing taper
сужение к. (относительное) — wing taper ratio
угол установки к. — angle of wing setting
удлинение к. — aspect ratio (ar)
отстыковать к. от фюзеляжа — detach the wing from the fuselageРусско-английский сборник авиационно-технических терминов > крыло
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4 длительный допустимый ток
(длительный) допустимый ток
Максимальное значение электрического тока, который может протекать длительно по проводнику, устройству или аппарату при определенных условиях без превышения определенного значения их температуры в установившемся режиме
[ ГОСТ Р МЭК 60050-826-2009]
Этот ток обозначают IZ
[ ГОСТ Р 50571. 1-2009 ( МЭК 60364-1: 2005)]EN
(continuous) current-carrying capacity
ampacity (US)
maximum value of electric current which can be carried continuously by a conductor, a device or an apparatus, under specified conditions without its steady-state temperature exceeding a specified value
[IEV number 826-11-13]
ampacity
The current in amperes that a conductor can carry continuously under the conditions of use without exceeding its temperature rating.
[National Electrical Cod]FR
courant (permanent) admissible, m
valeur maximale du courant électrique qui peut parcourir en permanence, un conducteur, un dispositif ou un appareil, sans que sa température de régime permanent, dans des conditions données, soit supérieure à la valeur spécifiée
[IEV number 826-11-13]Ampacity, the term is defined as the maximum amount of current a cable can carry before sustaining immediate or progressive deterioration. Also described as current rating or current-carrying capacity, is the RMS electric current which a device can continuously carry while remaining within its temperature rating. The ampacity of a cable depends on:
- its insulation temperature rating;
- conductor electrical properties for current;
- frequency, in the case of alternating currents;
- ability to dissipate heat, which depends on cable geometry and its surroundings;
- ambient temperature.
Electric wires have some resistance, and electric current flowing through them causes voltage drop and power dissipation, which heats the cable. Copper or aluminum can conduct a large amount of current before melting, but long before the conductors melt, their insulation would be damaged by the heat.
The ampacity for a power cable is thus based on physical and electrical properties of the material & construction of the conductor and of its insulation, ambient temperature, and environmental conditions adjacent to the cable. Having a large overall surface area may dissipate heat well if the environment can absorb the heat.
In a long run of cable, different conditions govern, and installation regulations normally specify that the most severe condition along the run governs the cable's rating. Cables run in wet or oily locations may carry a lower temperature rating than in a dry installation. Derating is necessary for multiple circuits in close proximity. When multiple cables are near, each contributes heat to the others and diminishes the amount of cooling air that can flow past the individual cables. The overall ampacity of the insulated conductors in a bundle of more than 3 must be derated, whether in a raceway or cable. Usually the de-rating factor is tabulated in a nation's wiring regulations.
Depending on the type of insulating material, common maximum allowable temperatures at the surface of the conductor are 60, 75 and 90 degrees Celsius, often with an ambient air temperature of 30°C. In the U.S., 105°C is allowed with ambient of 40°C, for larger power cables, especially those operating at more than 2 kV. Likewise, specific insulations are rated 150, 200 or 250°C.
The allowed current in cables generally needs to be decreased (derated) when the cable is covered with fireproofing material.
For example, the United States National Electric Code, Table 310-16, specifies that up to three 8 AWG copper wires having a common insulating material (THWN) in a raceway, cable, or direct burial has an ampacity of 50 A when the ambient air is 30°C, the conductor surface temperature allowed to be 75°C. A single insulated conductor in air has 70 A rating.
Ampacity rating is normally for continuous current, and short periods of overcurrent occur without harm in most cabling systems. The acceptable magnitude and duration of overcurrent is a more complex topic than ampacity.
When designing an electrical system, one will normally need to know the current rating for the following:- Wires
- Printed Circuit Board traces, where included
- Fuses
- Circuit breakers
- All or nearly all components used
Some devices are limited by power rating, and when this power rating occurs below their current limit, it is not necessary to know the current limit to design a system. A common example of this is lightbulb holders.
[http://en.wikipedia.org/wiki/Ampacity]
Тематики
- электротехника, основные понятия
Синонимы
EN
DE
- Dauerstrombelastbarkeit, f
- Strombelastbarkeit, f
FR
- courant admissible, m
- courant permanent admissible, m
Русско-английский словарь нормативно-технической терминологии > длительный допустимый ток
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