97精品天天人人揉人人玩,AV在线播放WWW啦啦啦,亚洲va欧美va国产综合,人人曰人人做人人,成人黄色电影网址,欧美久久久久久中文字幕,欧美亚洲另类A片区,亚洲资源AV无码日韩AV无码

航空翻譯_飛行翻譯_民航翻譯_藍(lán)天飛行翻譯公司

當(dāng)前位置: 主頁 > 直升機(jī) > 直升機(jī)資料 >

直升機(jī)飛行手冊(cè) Helicopter Flying Handbook

時(shí)間:2014-11-09 12:30來源:FAA 作者:直升機(jī)翻譯 點(diǎn)擊:

To view this page ensure that Adobe Flash Player version 9.0.124 or greater is installed.


Blade loading. The load imposed on rotor blades, determined by dividing the total weight of the helicopter by the combined area of all the rotor blades.
Blade root. The part of the blade that attaches to the blade grip.
Blade span. The length of a blade from its tip to its root.
Blade stall. The condition of the rotor blade when it is operating at an angle of attack greater than the maximum angle of lift.
Blade tip. The furthermost part of the blade from the hub of the rotor.
Blade track. The relationship of the blade tips in the plane of rotation. Blades that are in track will move through the same plane of rotation.
Blade tracking. The mechanical procedure used to bring the blades of the rotor into a satisfactory relationship with each other under dynamic conditions so that all blades rotate on a common plane.
Blade twist. The variation in the angle of incidence of a blade between the root and the tip.
Blowback. The tendency of the rotor disk to tilt aft in transition to forward flight as a result of unequal airflow.
Calibrated airspeed (CAS). Indicated airspeed of an aircraft, corrected for installation and instrumentation errors.
Center of gravity. The theoretical point where the entire weight of the helicopter is considered to be concentrated.
Center of pressure. The point where the resultant of all the aerodynamic forces acting on an airfoil intersects the chord.
Centrifugal force. The apparent force that an object moving along a circular path exerts on the body constraining the object and that acts outwardly away from the center of rotation.
Centripetal force. The force that attracts a body toward its axis of rotation. It is opposite centrifugal force.
Chip detector. A warning device that alerts you to any abnormal wear in a transmission or engine. It consists of a magnetic plug located within the transmission. The magnet attracts any metal particles that have come loose from the bearings or other transmission parts. Most chip detectors have warning lights located on the instrument panel that illuminate when metal particles are picked up.
Chord. An imaginary straight line between the leading and trailing edges of an airfoil section.
Chordwise axis. For semirigid rotors, a term used to describe the flapping or teetering axis of the rotor.
Coaxial rotor. A rotor system utilizing two rotors turning in opposite directions on the same centerline. This system is used to eliminated the need for a tail rotor.
Collective pitch control. The control for changing the pitch of all the rotor blades in the main rotor system equally and simultaneously and, consequently, the amount of lift or thrust being generated.
Coning. See blade coning.
Coriolis effect. The tendency of a rotor blade to increase or decrease its velocity in its plane of rotation when the center of mass moves closer to or farther from the axis of rotation.
Cyclic feathering. The mechanical change of the angle of incidence, or pitch, of individual rotor blades, independent of other blades in the system.
Cyclic pitch control. The control for changing the pitch of each rotor blade individually as it rotates through one cycle to govern the tilt of the rotor disk and, consequently, the direction and velocity of horizontal movement.
Delta hinge. A flapping hinge with an axis skewed so that the flapping motion introduces a component of feathering that would result in a restoring force in the flap-wise direction.
Density altitude. Pressure altitude corrected for nonstandard temperature variations.
Deviation. A compass error caused by magnetic disturbances from the electrical and metal components in the aircraft. The correction for this error is displayed on a compass correction card placed near the magnetic compass of the aircraft.
Direct control. The ability to maneuver a helicopter by tilting the rotor disk and changing the pitch of the rotor blades.
Direct shaft turbine. A single-shaft turbine engine in which the compressor and power section are mounted on a common driveshaft.
直升機(jī)翻譯 www.pankajksingh.com
本文鏈接地址:直升機(jī)飛行手冊(cè) Helicopter Flying Handbook