«TAILERON» 관련 영어 책
다음 도서 목록 항목에서
taileron 의 용법을 확인하세요.
taileron 에 관련된 책과 해당 책의 짧은 발췌문을 통해 영어 서적에서 단어가 사용되는 맥락을 제공합니다.
1
PANAVIA TORNADO: FLIGHT MANUAL 2
The pitch and roll output signals of the CSAS are routed to the taileron actuators.
The electrical signal is converted into a mechanical movement, which operates
the taileron power actuator servo valve. Roll output signals are also fed to the ...
2
Mikoyan Mig-29 Fulcrum Pilot's Flight Operating Manual (in ...
To protect the operation of the taileron. the speedbrakes are electrically
deactivated ii main or boost hydraulic pressure decreases. ft the boost hydraufic
pressure drops below 100 ltpifcrn2 (10 MPa). the speedbrakes are retracted
automatically ...
North Atlan Treaty Organization (Nato), 2007
3
Aircraft Systems: Mechanical, Electrical and Avionics ...
Thecombined pitch/roll output to the taileron actuators is consolidated from three
lanes to four within the pitch computersothe feed to the taileron actuatorsis
quadruplex.The quadruplex taileron actuator is provided byFaireyHydraulics ...
Ian Moir, Allan Seabridge, 2011
4
Jet Fighters: Inside & Out
1 Starboard taileron construction 2 Honeycomb trailing-edge panels 3
Compound sweep taileron leading edge 4 Taileron pivot fixing 5 Afterburner
ducting, extended 14 in (36 cm) 6 Thrust-reverser bucket door actuator 7
Afterburner nozzle ...
5
Proceedings of the Sixteenth International Modal Analysis ...
Modal Analysis The fundamental antisymmetric nomal modes are described
contribution of the fundamental taileron and fin modes (empanage flutter) the
flutter mode II at approximately 19 Hz which represents mainly the second
taileron ...
Alfred L. Wicks, Society of Photo-optical Instrumentation Engineers, Society for Experimental Mechanics (U.S.), 1998
6
Aviation Safety and Pilot Control:: Understanding and ...
The taileron became rate saturated. Compensating for a slow roll motion, the pilot
command for differential tail was not fed through to the taileron due to internal
CSAS [Command Stability Augmentation System] priorities giving the pitch axis ...
Committee on the Effects of Aircraft-Pilot Coupling on Flight Safety, National Research Council, Commission on Engineering and Technical Systems, 1997
7
Health Monitoring of Aerospace Structures: Smart Sensor ...
(b) (c) (d) Figure 2.9 TORNADO airframe components used for cost analysis: (a)
main landing gear fitting; (b) cover; (c) tail section skin; (d) taileron (Brand and
Boller) Cover 1 Cover 2 Fitting Tail Taileron MLG section fitting skin Figure 2.10 ...
Wieslaw Staszewski, C. Boller, G. R. Tomlinson, 2004
8
Aircraft Engineering Principles
Another common control grouping is the taileron, which has been designed to
provide the combined control functions of the tailplane and ailerons. With a
taileron, the two sides of the slab tail will act collectively to provide tailplane
control in ...
Lloyd Dingle, Michael H Tooley, 2013
9
Robust flight control: a design challenge
The actuator representations for each aerodynamic control surface are described
in sections 27.2.4 to 27.2.4 below. Taileron actuator The taileron consists out of a
starboard taileron and a port taileron, which can be controlled independently.
Jean-François Magni, Samir Bennani, Jan Terlouw, 1997
10
Encyclopedia of aircraft
... Tail navigation light 94 Rudder 95 Starboard taileron surface 96 Thrust-
reverser bucket- doors, open 97 Starboard fully-variable exhaust nozzle 98 Rear
spine end fairing 99 Port fully-variable exhaust nozzle 100 Thrust-reverser bucket
- door ...
Michael John Haddrick Taylor, John William Ransom Taylor, 1978
