Patents for B64D 31 - Power plant control; Arrangement thereof (859)
11/2002
11/26/2002US6484605 Control cables
11/21/2002US20020171005 Device and process for regulating the power of the engines of a rotary wing multi-engine aircraft
11/20/2002EP1257466A2 Aircraft
11/20/2002EP1257465A2 Remotely piloted aircraft
10/2002
10/31/2002WO2001058756A9 Aircraft
10/24/2002US20020153452 Multi-mode tiltrotor nacelle control system with integrated envelope protection
10/22/2002US6468035 Method and apparatus for controlling airplane engine
10/09/2002CN1092287C Method and apparatus for automatically providing jet engine thrust ratings to avionic systems
09/2002
09/18/2002EP1240417A2 Device and method for adjusting the power of a power pack driving a helicopter rotor
08/2002
08/29/2002US20020117582 Method for the control of aero gas turbine engines
07/2002
07/24/2002EP1224117A1 Aircraft and method for operating an aircraft
07/23/2002CA2131578C Control lever assembly for setting engine thrust in an aircraft
07/11/2002US20020088225 Turbocharger control system and propeller control system by stepper motor
07/11/2002DE10062252A1 Verfahren zur Regelung von Fluggasturbinen The method for controlling aircraft gas turbines
06/2002
06/27/2002WO2002016739A3 Turbocharger control system and propeller control system by stepper motor
06/19/2002EP1215383A1 Control system for aircraft gas turbine engines
05/2002
05/02/2002WO2001058758A3 Remotely piloted aircraft
05/02/2002WO2001058757A3 Communications system using high altitude, long endurance aircraft as relays
04/2002
04/04/2002WO2001089926A3 Power lever tactile cueing system
03/2002
03/13/2002EP1185912A1 Device for controlling an apparatus
03/13/2002EP1185455A1 Device for controlling an engine
03/13/2002EP1185454A1 Device for controlling an engine
02/2002
02/28/2002WO2002016739A2 Turbocharger control system and propeller control system by stepper motor
02/14/2002WO2001048574A3 Device and method for adjusting the power of a power pack driving a helicopter rotor
01/2002
01/22/2002US6340289 Single lever power controller for manned and unmanned aircraft
01/03/2002WO2001058756A3 Aircraft
11/2001
11/29/2001WO2001089926A2 Power lever tactile cueing system
11/22/2001WO2001087706A1 Multi-mode tiltrotor nacelle control system with integrated envelope protection
11/22/2001US20010044680 Fuzzy logic based emergency flight control with thrust vectoring capability
11/13/2001US6314830 Control cables
08/2001
08/16/2001WO2001058758A2 Remotely piloted aircraft
08/16/2001WO2001058757A2 Communications system using high altitude, long endurance aircraft as relays
08/16/2001WO2001058756A2 Aircraft
08/16/2001US20010013261 Control cables
08/16/2001CA2400048A1 Aircraft
08/16/2001CA2400041A1 Aircraft
08/16/2001CA2400022A1 Aircraft
08/07/2001CA2015588C Helicopter, high rotor speed enhancement
07/2001
07/10/2001US6259976 Fuzzy logic based emergency flight control with thrust vectoring
07/05/2001WO2001048574A2 Device and method for adjusting the power of a power pack driving a helicopter rotor
06/2001
06/28/2001DE19961531A1 Propeller unit for glider can be moved from glide position to propulsion position by manual actuator lever
06/06/2001EP1104503A2 Control cables
05/2001
05/30/2001CN1066371C 轴相位控制机构 Axis phase control mechanism
05/03/2001WO2001030652A1 Aircraft and method for operating an aircraft
05/01/2001US6224021 Thrust control apparatus and method for an airplane
02/2001
02/13/2001US6186447 Autothrottle retard rate control system
01/2001
01/24/2001EP1070199A1 Single lever power controller for manned and unmanned aircraft
01/09/2001US6171055 Single lever power controller for manned and unmanned aircraft
12/2000
12/21/2000WO2000077589A1 Device for controlling an apparatus
12/21/2000WO2000076843A1 Device for controlling an engine
12/21/2000WO2000076842A1 Device for controlling an engine
12/14/2000DE19926800A1 Vorrichtung zum Steuern eines Triebwerkes An apparatus for controlling an engine
12/14/2000DE19926784A1 Vorrichtung zum Steuern einer Einrichtung An apparatus for controlling a device
12/14/2000DE19926563A1 Vorrichtung zum Steuern eines Triebwerkes An apparatus for controlling an engine
10/2000
10/03/2000US6126111 Emergency flight control system using one engine and fuel transfer
09/2000
09/26/2000US6122984 Shaft phase control mechanism
08/2000
08/15/2000US6102330 Emergency multiengine aircraft system for lateral control using differential thrust control of wing engines
07/2000
07/11/2000US6088632 Engine control system for an aircraft
06/2000
06/29/2000WO2000009895A3 Control cables
05/2000
05/23/2000CA2116340C Helicopter engine control having yaw input anticipation
05/18/2000WO2000009895A9 Control cables
04/2000
04/27/2000WO1997030813A9 Shaft phase control mechanism
03/2000
03/21/2000US6041273 Emergency control aircraft system using thrust modulation
02/2000
02/24/2000WO2000009895A2 Control cables
01/2000
01/04/2000CA2017151C Helicopter control with multiple schedule rotor speed decay anticipator
12/1999
12/07/1999US5996464 Fail safe valve and multiplexed fluid control systems incorporating the same
11/1999
11/10/1999EP0954401A1 Shaft phase control mechanism
10/1999
10/14/1999WO1999051868A1 Single lever power controller for manned and unmanned aircraft
08/1999
08/04/1999EP0933294A1 Aircraft engine control system
07/1999
07/27/1999US5927655 Device for controlling the thrust of a multi-engine aircraft
06/1999
06/24/1999DE19840711A1 Twin-engine aircraft
05/1999
05/05/1999CN1215682A Leading wingless airplane
04/1999
04/06/1999US5893040 Method and apparatus for automatically providing jet engine thrust ratings to avionic systems
02/1999
02/24/1999CN1209087A Shaft phase control mechanism
02/23/1999US5873546 System and method for conducting one engine inoperative flight procedures training in a dual-engine helicopter
06/1998
06/23/1998CA2113729C Helicopter engine speed enhancement during heavy rotor load and rapid descent rate maneuvering
03/1998
03/11/1998EP0828206A1 Device for controlling the thrust of a multi-engine aircraft
02/1998
02/04/1998CN1172208A Method and apparatus for automatically providing jet engine thrust ratings to avionic systems
11/1997
11/19/1997EP0807897A2 Method and apparatus for automatically providing jet engine thrust ratings to avionic systems
08/1997
08/28/1997WO1997030813A1 Shaft phase control mechanism
04/1997
04/22/1997US5623197 Active control of battery charging profile by generator control unit
03/1997
03/25/1997US5613652 Aircraft auto throttle system
02/1997
02/05/1997EP0667008B1 Partial engine and driveshaft failure detection monitor for a multi-engine aircraft
02/1996
02/06/1996US5488824 Throttle control device controlling two engines of a same aerodyne
11/1995
11/22/1995EP0601099B1 Helicopter engine control having yaw input anticipication
11/02/1995EP0601097B1 Helicopter engine speed enhancement during heavy rotor load and rapid descent rate maneuvering
08/1995
08/16/1995EP0667008A1 Partial engine and driveshaft failure detection monitor for a multi-engine aircraft.
08/09/1995EP0601100B1 Helicopter engine control having lateral cyclic pitch anticipation
06/1995
06/14/1995EP0657350A1 Manual throttle control device for operating both enzymes of an aircraft
04/1995
04/04/1995US5403155 Power management for a turbine powered helicopter
03/1995
03/16/1995DE4331230A1 Steuerhebelgerät für die Einstellung der Schubkraft bei Flugzeugen Control lever device for adjusting the thrust for aircraft
11/1994
11/15/1994US5363652 Air/fuel ratio control device of a turbocharged engine
11/08/1994US5363317 Engine failure monitor for a multi-engine aircraft having partial engine failure and driveshaft failure detection
06/1994
06/15/1994EP0601100A1 Helicopter engine control having lateral cyclic pitch anticipation.
06/15/1994EP0601099A1 Helicopter engine control having yaw input anticipication.
05/1994
05/31/1994US5315817 Control system for preventing crash engagement of a ratchet and pawl clutch during restart of a turbine engine
05/31/1994CA1329907C Control apparatus
05/24/1994US5314147 Helicopter engine speed enhancement during heavy rotor load and rapid descent rate maneuvering
05/11/1994WO1994010619A1 Partial engine and driveshaft failure detection monitor for a multi-engine aircraft
05/11/1994CA2143871A1 Partial engine and driveshaft failure detection monitor for a multi-engine aircraft
1 2 3 4 5 6 7 8 9