load+decrease/xx

load decrease Lastabsenkung f, Lastabwurf m

1. уменьшение нагрузки

decrease in load STAT Belastungsreduzierung f

1. n намаление, намаляване, снижаване, спадане 2. v намалявам (се), снижавам (се)

1. автоматическая частотная разгрузка
2. автоматическая разгрузка

1. load decrease

1. voltage recovery time

1. время восстановления напряжения

Lastabsenkung f load decrease

1. load-shedding protection

abandon the takeoff abeam the left pilot position abeam the right pilot position abort the flight abort the takeoff above the glide slope absorb the shock energy accelerate the rotor accelerate to the speed adhere to the flight plan adhere to the track adjust the cable adjust the compass adjust the engine adjust the heading advice to follow the controller's advance affect the regularity affect the safety align the aircraft align the aircraft with the center line align the aircraft with the runway alter the heading amplify the signal apparent drift of the gyro apply the brake approach the beam approve the limitations approve the tariff area of coverage of the forecasts arrest the development of the stall arrive over the aerodrome assess the damage assess the distance assess the suitability assume the control attain the power attain the speed at the end of at the end of segment (полета) at the end of stroke (поршня) at the ground level at the start of cycle at the start of segment (полета) avoid the obstacle backward movement of the stick balance the aircraft balance the control surface balance the propeller bear on the accident before the turbine below the glide slope below the landing minima bend the cotterpin ends be off the track be on the level on the hour block the brake boundary of the area brake the propeller break the journey bring the aircraft back bring the aircraft out by altering the heading cage the gyroscope calibrate the compass calibrate the indicator calibrate the system calibrate the tank cancel the drift cancel the flight cancel the forecast cancel the signal capture the beam carry out a circuit of the aerodrome carry out the flight center the autopilot center the wiper change the frequency change the pitch change the track check the reading chop the power circle the aerodrome clean the aircraft clean up the crack clearance of the aircraft clearance over the threshold clear for the left-hand turn clear the aircraft clear the obstacle clear the point clear the runway climb on the course close the buckets close the circuit close the flight come clear of the ground commence the flight commence the landing procedure compare the readings compensate the compass compensate the error compile the accident report complete the circuit complete the flight complete the flight plan complete the turn compute the visual range conditions beyond the experience conditions on the route considering the obstacles construct the procedure containerize the cargo continue operating on the fuel reserve continue the flight continue the takeoff contribute towards the safety control the aircraft control the pitch convert the frequency convey the information correct the trouble correspond with the operating minima counteract the rotor torque coverage of the chart cover the route crosscheck the readings cross the airway data on the performance decelerate in the flight decelerate the aircraft to decrease the deviation decrease the pitch decrease the speed de-energize the bus define the failure deflate the tire deflect the control surface (напр. элерон) delay the turn delimit the runway delimit the taxiway delineate the runway delineate the taxiway deliver the baggage deliver the clearance denote the obstacle denoting the obstacle depart from the rules departure from the standards depress the pedal detach the load detach the wing determinate the cause determine amount of the error determine the delay determine the extent of damage determine the friction determine the sign of deviation detract from the safety development of the stall deviate from the flight plan deviate from the glide slope deviate from the heading deviation from the course deviation from the level flight discharge the cargo disclose the fares discontinue the takeoff disengage the autopilot displace the center-of-gravity disregard the indicator disseminate the forecast drain the tank draw the conclusion drift off the course drift off the heading drop the nose duck below the glide path ease the aircraft on effect adversely the strength (напр. фюзеляжа) elevation of the strip eliminate the cause of eliminate the hazard eliminate the ice formation eliminate the source of danger (для воздушного движения) enable the aircraft to endanger the aircraft endange the safety endorse the license energize the bus enforce rules of the air engage the autopilot ensure the adequate provisions enter the aircraft enter the aircraft stand enter the airway enter the final approach track enter the spin enter the tariff into force enter the traffic circuit enter the turn entry into the aerodrome zone entry into the flare erection of the gyro establish the characteristics establish the flight conditions establish the procedure exceeding the stalling angle exceed the stop execute the manoeuvre execute the turn expedite the clearance express the altitude extend the agreement extend the landing gear extend the legs extreme aft the center-of-gravity extreme forward the center-of-gravity eye height over the threshold fail into the spin fail to follow the procedure fail to observe the limitations fail to provide the manuals fall into the spin feather the propeller file the flight plan first freedom of the air flight inbound the station flight outbound the station flight over the high seas flight under the rules fly above the weather fly at the altitude fly into the sun fly into the wind fly on the autopilot fly on the course fly on the heading fly the aircraft 2. пилотировать воздушное судно fly the beam fly the circle fly the glide-slope beam fly the great circle fly the heading fly the rhumb line fly under the autopilot fly under the supervision of focus the light follow the beam follow the glide slope follow up the aircraft forfeit the reservation freedom of the air fuel the tank fulfil the conditions gain the air supremacy gain the altitude gain the glide path gain the power gain the speed gather the speed get into the aerodrome get on the course get the height give the way go out of the spin govern the application govern the flight govern the operation grade of the pilot licence guard the frequency handle the baggage handle the flight controls have the runway in sight head the aircraft into wind hold on the heading hold over the aids hold over the beacon hold the aircraft on the heading hold the brake hold the heading on the compass hold the position hold the speed accurately hover at the height of hovering in the ground effect identify the aerodrome from the air identify the aircraft identify the center line impair the operation impair the safety impose the limitations in computing the fuel in conformity with the specifications increase a camber of the profile increase the pitch increase the speed indicate the location from the air inherent in the aircraft initiate the turn install in the aircraft install on the aircraft intercept the beam intercept the glide slope International Relations Department of the Ministry of Civil Aviation interpretation of the signal in the case of delay in the event of a mishap in the event of malfunction introduction of the corrections issue the certificate jeopardize the flight judge the safety keep clear of the aircraft keep out of the way keep tab on the fleet keep the aircraft on keep the altitude keep the ball centered keep the pace keep to the minima kick off the drift kill the landing speed landing off the aerodrome land into the wind land the aircraft latch the pitch stop (лопасти воздушного винта) latch the propeller flight stop lateral the center-of-gravity lay the route lead in the aircraft lead out the aircraft leave the airspace leave the altitude leave the plane leave the runway level the aircraft out lie beyond the range line up the aircraft load the gear load the generator load the structure lock the landing gear lock the landing gear down lock the landing gear up lock the legs longitudinal the center-of-gravity lose the altitude lose the speed loss the control lower the landing gear lower the legs lower the nose wheel maintain the aircraft at readiness to maintain the altitude maintain the course maintain the flight level maintain the flight procedure maintain the flight watch maintain the flying speed maintain the heading maintain the parameter make a complaint against the company make the aircraft airborne make the course change make the reservation manipulate the flight controls mark the obstacle mean scale of the chart meet the airworthiness standards meet the conditions meet the specifications misjudge the distance modify the flight plan monitor the flight monitor the frequency moor the aircraft mount on the frame move off from the rest move the blades to higher move the pedal forward name-code of the route neglect the indicator note the instrument readings note the time observe the conditions observe the instruments observe the readings obtain the correct path obtain the flying speed obtain the forecast offer the capacity off-load the pump on the base leg on the beam on the cross-wind leg on the down-wind leg on the eastbound leg on the final leg on the left base leg on the speed on the upwind leg open the buckets open the circuit open the door inward outward operate from the aerodrome operate under the conditions overcome the obstacle overcome the spring force overflying the runway overpower the autopilot overrun the runway overshoot capture of the glide slope over the territory over the top over the wing park in the baggage participation in the investigation passing over the runway pass the signal past the turbine perform the service bulletin pick up the signal pick up the speed pilot on the controls pitch the nose downward place the aircraft place the flaps in plane of symmetry of the aeroplane plot the aircraft potential hazard to the safe power the bus present the minimum hazard preserve the clearance pressurize the bearing produce the signal profitability over the route prolongation of the rating properly identify the aircraft protect the circuit prove the system pull out of the spin pull the aircraft out of pull the control column back pull the control stick back pull up the helicopter puncture the tire push the aircraft back push the aircraft down push the control column push the control stick put into the spin put on the course put the aircraft into production put the aircraft on the course put the aircraft over raise the landing gear reach the altitude reach the flight level reach the glide path reach the speed reach the stalling angle read the drift angle read the instruments receive the signal record the readings recover from the spin recover from the turn recovery from the manoeuvre recovery from the stall recovery from the turn rectify the compass reduce the hazard reestablish the track regain the glide path regain the speed regain the track register the aircraft release the aircraft release the landing gear release the landing gear lock release the load release the uplock relocate the plane's trim remedy the defect remedy the trouble remove the aircraft remove the crack remove the tangle render the certificate renew the license renew the rating replan the flight report reaching the altitude report reaching the flight level report the heading reset the gyroscope restart the engine in flight restore the system restrict the operations resume the flight resume the journey retain the lever retract the landing gear return the aircraft to service reverse the propeller roll in the aircraft roll into the turn roll left on the heading roll on the aircraft roll on the course roll out of the turn roll out on the heading roll out the aircraft roll right on the heading rotate the aircraft rotate the bogie rules of the air run fluid through the system run off the runway run out the landing gear schedule the performances seat the brush second freedom of the air secure the mishap site select the course select the flight route select the frequency select the heading select the mode select the track angle separate the aircraft serve out the service life set at the desired angle set the course set the flaps at set the heading set the propeller pitch set the throttle lever set up the speed shift the center-of-gravity shop out the skin simulate the instruments responses slacken the cable slave the gyroscope smooth on the heading smooth out the crack smooth out the dent smooth the signal space the aircraft spin the gyro rotor state instituting the investigation (авиационного происшествия) state submitting the report (об авиационном происшествии) steady airflow about the wing steer the aircraft stop the crack propagation stop the leakage submit the flight plan substitute the aircraft supervision approved by the State supply the signal swing the compass swing the door open switch to the autopilot switch to the proper tank takeoff into the wind take off power to the shaft take over the control take the bearing take the energy from take the readings take the taxiway take up the backlash take up the position tap air from the compressor terminate the agreement terminate the control terminate the flight test in the wind tunnel test the system the aircraft under command the route to be flown the route to be followed the runway is clear the runway is not clear the search is terminated through on the same flight throughout the service life tighten the turn time in the air time the valves titl of the gyro to define the airspace transfer the control transit to the climb speed trim the aircraft turn into the wind turn off the system turn on the system turn the proper tank on unarm the system uncage the gyroscope unfeather the propeller unlatch the landing gear unlatch the pitch stop (лопасти воздушного винта) unstall the aircraft unstick the aircraft uplift the freight violate the law wander off the course warn the aircraft wind the generator with decrease in the altitude withdraw from the agreement with increase in the altitude within the frame of within the range withstand the load work on the aircraft write down the readings

coefficient (coeff.), factor
безразмерное число, в основном отношение к-п. величин, характеризующих заданные условия. — а number indicating the amount of some change under certain specified сoпditions, often expressed as a ratio.
- безопасности — factor of safety
число, равное отношению расчетной нагрузки к эксплуатационной. расчетная нагрузка - произведение эксплуатационной нагрузки на коэффициент безопасности. — а number indicating the ratio between the ultimate load and limit load (maximum load expected in service). ultimate load is limit load multiplied by factor of safety.
- восстановления давления — pressure recovery factor
- двухконтурности (дтрд) — bypass ratio
- загрузки пассажирами, безубыточный — passenger break-even load factor
- запаса длины впп — field length factor
- запаса длины летной полосы — field length factor
- запаса длины летной полосы в направлении взлета — takeoff field length factor
- запаса длины летной полосы в направлении посадки — landing field length factor
- запаса длины летной полосы при всех работающих двигателей — field length factor for all-engines-operating сase
- запаса длины летной полосы при одном отказавшем двигателе — field length factor for one-engine-inoperative ease
- запаса прочности — reserve factor
отношение фактической прочности конструкции к минимально-потребной в данных условиях. — а ratio of the actual strength of the structure to the minimum required to specific condition.
- заполнения (в вычислительном уст-ве) — duty factor in computer, the ratio of active time to total time.
- заполнения (воздушного) винта — propeller solidity ratio
отношение суммарной площади всех лопастей винта к сметаемой ими площади. — the ratio of the total projected blade area to the area of the projected outline of the propeller disc.
- заполнения несущего винта (вертолета) — rotor solidity ratio solidity of rotor is a ratio of the total blade area to the disc area.
- лобового сопротивления (сх) — drag coefficient (cd)
коэффициент, характеризующий лобовое сопротивление рассматриваемого аэродинамического профиля. — а coefficient representing the drag on а given airfoil.
- маневренной перегрузки — maneuvering load factor
- момента крена — rolling-moment coefficient
- момента рыскания — yawing-moment coefficient
- момента тангажа — pitching-moment coefficient
- мощности — power factor
- мощности (воздушного винта) — activity factor
- мощности лопасти (возд. винта) — blade activity factor
безразмерная функция поверхности лопасти, характеризующая способность лопасти использовать прикладываемую мощность. — а non-dimensional function of the blade surface used to express capacity of a blade for absorbing power.
- несущей поверхности (покрытия аэродрома), калифорнийский — californian bearing ratio (с.в.r.)
-, относительный (воздушного винта) — figure of merit
- перегрузки (n) — load factor (n)
число, показывающее, во сколько раз нагрузки, действующие на самолет (или его отдельные части), превышает нагрузки в равномерном горизонтальном полете или нагрузки от веса при стоянке. — the ratio to the weight of an aircraft of а specified exterпаl load. such load may arise from aerodynamic forces, gravity, ground or water reaction, or from combinations of these forces.
- перегрузки, максимальный эксплуатационный — limit load factor
- перегрузки, (полетный) — flight load factor
отношение составляющей аэродинамической нагрузки (действующей перпендикулярно продольной оси ла) к весу ла. — the ratio of the aerodynamic force component (acting normal to the assumed longitudiпа1 axis of the airplane) to the weight of the airplane.
- перегрузки (полетной), отрицательный — negative load factor
- перегрузки (полетной), положительный — positive load factor
в данном случае аэродинамичеекая сила воздействует на ла снизу вверх. — in positive load factor the aerodynamic force acts upward with respect to the airplane.
- перегрузки при маневре — maneuvering load factor
- перегрузки при маневре, максимальный эксплуатационный — limit maneuvering load factor
- перегрузки, расчетный — ultimate load factor
- передачи (коэффициент передаточного числа в системе управления ла) — gain
- подъемной силы (су) безразмерная величина, определяемая по формуле. — lift coefficient (cl) а coefficient representing the lift of а given airfoil or other body. the lift coefficient is obtained ьу dividing the lift by the free-stream dynamic pressure and by the representative area under consideration.
- полезного действия (кпд) — efficiency (n)

the ratio of the useful output of the quantity to its total input.
- полезного действия, общий — overall efficiency
- полезного действия,тепловой — thermal efficiency
-, поправочный — correction factor
например, для учета влияния погодных (сезонных) условий (температура наружного воздуха, атмосферные осадки, обледенение) на характеристики тормозного участка впп в пределах установленных эксплуатационных ограничений. — the correction factors must account for the particular surface characteristics of the stopway and the variations in these characteristics with seasonal weather conditions (such as temperature, rain, snow, and ice) within the established operational limits.
- предельной перегрузки — ultimate load factor
- преобразования (в преобразователе) — conversion efficiency ratio of dc output power to ас input power.
- профильного сопротивления — profile drag coefficient
- прочности грунта, калифорнийский — californian bearing ratio (c.b.r.)
(к. несущей способности покрытия аэродрома, впп) — c.b.r. is used to measure subsoil strength of the runways and airfields.
- связи (эл.) — coupling coefficient
- сжимаемости — coefficient of compressibility
относительное уменьшение объема газа при повышении давления в изотермическом процессе. — the relative decrease of the volume of а gaseous system with increasing pressure in an isothermal process.
- совершенства (воздушного винта) — figure of merit
- сопротивления (лобовой, сx) — drag coefficient (cd)
- сопротивления (сx) груза на внешней подвеске (вертолета) — drag coefficient (cd) representing а drag caused by an externally-slung load
- стоячей волны — standing wave ratio (swr)
- схождения карты — chart convergence factor (ccf)
- сцепления (между шиной колеса и поверхностью впп) — coefficient of friction
-, сцепления (между шиной и впп при торможении) — braking coefficient of friction
- трансформации (в трансформаторе) — transformation ratio compensation windings are used to correct for variations in the resolvers transformation ratio.
- трения — coefficient of friction
- трения торможения — braking coefficient of friction
коэффициент трения между шиной и поверхностью взлетно-посадочной полосы при торможении самолета. — braking coefficient of friction between the aircraft wheel tires and runway (surface).
- трения торможения, осредненный приведенный — (mean) corrected braking coefficient of friction
- тяги (воздушного винта) — thrust coefficient (ст)
- усиления (эл.) — amplification factor

the ratio of output magnitude to input magnitude.
- усиления антенны — antenna gain
- усиления (передаточное число в системе управления) — gain
- усиления, самонастраивающийся (системы управления) — adaptive gain
- утечки — leakage factor
- шарнирного момента — hinge moment factor
- шарнирного момента от порыва ветра на земле, предельный — limit hinge moment factor (к) for ground gusts
в отношении элеронов и рулей высоты, коэффициент имеет положительный знак, если момент, воздействующий на поверхность управления, вызывает ее опускание. — for ailerons and elevators, а positive value of к indicates а moment tending to depress the surface, and а negative value of к - to raise the surface.
- шума — noise factor
для данной полосы частот, отношение суммарной величины помех на выходе к величине помехи на входе. — for а given bandwidth, the ratio оf total noise at the output, to the noise at the input.
- эксплуатационной маневренной перегрузки (максимальный), или эксплуатационной перегрузки при маневрировании (отрицательный или попожительный) — (negative, positive) limit maneuvering load factor rotorcraft must be designed for positive limit maneuvering load factor of 3.5 and negafive limit maneuvering load factor of 1.0.