• 热门标签

当前位置: 主页 > 航空资料 > 国外资料 >

时间:2010-08-15 20:39来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

the situation. The case, instructor’s manual, and synopsis, were anonymously peer reviewed and accepted by the
North American Case Research Association (NACRA) for its annual meeting, October 27-29, 2005, North Falmouth,
MA. All rights are reserved to the author and NACRA. © 2005 by Isaac Cohen. Contact person: Isaac Cohen,
Department of Organization and Management, COB, San Jose State University, One Washington Square, San Jose,
Ca 95192, 408-924-3567, cohen_i@cob.sjsu.edu
PILOT AUTHORITY AND AIRCRAFT
PROTECTIONS
Air Line Pilots Association
Airworthiness Performance Evaluation and Certification Committee
Captain Ron Rogers, Chairman
March 1, 1999
CONTENTS
PILOT AUTHORITY AND AIRCRAFT PROTECTIONS --------------------------------------- 1
1.0 INTRODUCTION--------------------------------------------------------------------------------- 4
2.0 ARGUMENT --------------------------------------------------------------------------------------- 4
3.0 ON-GROUND SENSING------------------------------------------------------------------------ 4
3.1 Recommendation---------------------------------------------------------------------------------------------------------------- 5
4.0 STALL PROTECTION--------------------------------------------------------------------------- 5
4.1 Recommendation---------------------------------------------------------------------------------------------------------------- 6
5.0 ENGINE CONTROLS---------------------------------------------------------------------------- 6
5.1 Effects Of Additional Thrust On Climb Performance------------------------------------------------------------------ 9
5.2 The Effects Of Additional Thrust Capability On Cfit Recovery Capability------------------------------------10
5.3 The Effect Of Additional Thrust On Recovery From Windshear--------------------------------------------------11
5.3.1 The Effects of Additional Thrust in Windshear Recovery for the Airbus A-320 (Takeoff) ------------12
5.3.2 The Effects of Additional Thrust in Windshear Recovery for the Boeing B-777 (Takeoff)------------12
5.3.3 The Effects of Additional Thrust in Windshear Recovery for the Boeing B-777 (Approach)---------13
5.4 Conclusion----------------------------------------------------------------------------------------------------------------------13
6.0 FLIGHT ENVELOPE PROTECTIONS -------------------------------------------------------13
6.1 Design Error ---------------------------------------------------------------------------------------------------------------------14
6.2 Flight Envelope Protection Design Philosophies ---------------------------------------------------------------------14
6.2.1 Conventional Flight Envelope Protections-------------------------------------------------------------------------14
6.2.2 Hard Flight Envelope Protections ------------------------------------------------------------------------------------14
6.2.3 Soft Flight Envelope Protections -------------------------------------------------------------------------------------14
6.2.4 Flight Envelope Protection Overrides -------------------------------------------------------------------------------15
6.2.5 Flight Envelope Authority----------------------------------------------------------------------------------------------15
6.3 Controlled Flight Into Terrain (CFIT)-----------------------------------------------------------------------------------16
6.3.1 Flight Test------------------------------------------------------------------------------------------------------------------17
6.3.2 CFIT Maneuver------------------------------------------------------------------------------------------------------------17
6.4 Aircraft Flight Control Design----------------------------------------------------------------------------------------------17
6.4.1 Aircraft With Conventional Flight Controls-----------------------------------------------------------------------17
6.4.2 FBW Aircraft With ÒHardÓ Protection Features------------------------------------------------------------------18
6.4.3 FBW Aircraft With ÒSoftÓ Protection Features-------------------------------------------------------------------19
6.4.4 CFIT Recovery Conclusions/Recommendations-----------------------------------------------------------------19
6.4.5 Conclusions-----------------------------------------------------------------------------------------------------------------20
6.4.6 Recommendations---------------------------------------------------------------------------------------------------------20
6.5 High Speed Upset Recovery------------------------------------------------------------------------------------------------21
6.5.1 Aircraft With Conventional Flight Controls-----------------------------------------------------------------------21
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:航空资料16(12)