Patents for B64C 13 - Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers (4,795) |
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05/03/1994 | US5307630 System pressure compensated variable displacement hydraulic motor |
04/26/1994 | CA1328911C Synthetic speed stability flight control system |
04/19/1994 | CA2018814C Digital electronics assembly for a tube-launched missile |
04/13/1994 | EP0592280A1 Method and apparatus for the analysis of a message emitted by interactive means to a man-machine dialog system |
04/13/1994 | EP0591890A1 Hand control system |
04/12/1994 | CA1328495C Arrangement for controlling the position of an aircraft control surface |
04/07/1994 | CA2107712A1 Method and device for analyzing messages forwarded to a man-machine dialogue system by interaction means |
04/06/1994 | EP0590294A1 Centering unit for an aircraft control surface |
04/05/1994 | US5301112 Transient free synchronizer for autopilot systems |
04/05/1994 | US5299666 Resettable pilot operated torque limiter |
03/29/1994 | CA1328132C Arrangement for controlling the performance of bob-up/bob-down maneuvers by a helicopter |
03/23/1994 | EP0479921B1 Flight craft with fluid systems which incorporate butterfly valves, and butterfly valve methods and apparatus |
03/01/1994 | US5291113 Servo coupled hand controllers |
02/23/1994 | EP0584010A1 Method of actuation of the control surfaces of an aircraft to make up for a lateral deviation of the flight path at low speed |
02/17/1994 | WO1994003854A1 Failsafe digital bus to analog protocol converter system |
02/17/1994 | CA2120347A1 Failsafe digital bus to analog protocol converter system |
02/03/1994 | DE4319540A1 Fermentative prodn. of sophorolipid compsn. |
01/19/1994 | EP0419644B1 Self-adaptive control process for piloting a physical system |
01/11/1994 | US5277020 Hydraulically actuated aircraft engine control system |
12/29/1993 | EP0576194A1 Multipiece gimbal |
12/23/1993 | CA2098227A1 Multipiece gimbal |
12/21/1993 | US5271143 Method of making a multipiece gimbal |
12/08/1993 | EP0573106A1 Multiaxis redundant fly-by-wire primary flight control system |
11/25/1993 | WO1993023797A1 Helicopter integrated fire and flight control having constraint limiting control |
11/25/1993 | WO1993023715A1 Helicopter integrated fire and flight control having azimuth and pitch control |
11/25/1993 | CA2118025A1 Helicopter integrated fire and flight control having constraint limiting control |
11/25/1993 | CA2118024A1 Helicopter integrated fire and flight control having azimuth and pitch control |
11/24/1993 | EP0570690A2 Control unit for aircraft cockpits |
11/11/1993 | WO1993022195A1 Fault-tolerant linear electromechanical actuator |
11/11/1993 | WO1993022194A2 Airplane mechanical control system |
11/09/1993 | CA2068305A1 Aircraft control locking apparatus |
11/03/1993 | EP0527135A4 Method and apparatus for structural actuation and sensing in a desired direction |
10/26/1993 | US5255882 Setting device with a nut controllable by a spindle |
10/20/1993 | EP0566452A1 Single-rotor helicopter with mixed counter-torque system and method to counter the torque induced by this single rotor |
10/05/1993 | US5249761 Setting device for a control surface |
09/29/1993 | EP0561988A1 Motor having integral detent. |
08/31/1993 | US5240207 Generic drone control system |
08/24/1993 | US5238207 Aircraft rudder boost system |
08/24/1993 | US5238203 High speed turn coordination for rotary wing aircraft |
08/11/1993 | EP0555122A1 Linear actuator, in particular for an aircraft landing gear leg |
08/04/1993 | CA2088569A1 Linear actuator, especially for operation of a landing gear strut |
08/03/1993 | US5233542 Method and circuit configuration for forming an evaluation signal from a plurality of redundant measurement signals |
08/03/1993 | US5233252 Motor having integral detent |
07/07/1993 | EP0550341A1 Hydraulic fluid supply for the control device of an aircraft engine |
07/06/1993 | US5224826 Piezoelectric helicopter blade flap actuator |
07/06/1993 | US5224667 System enabling the flutter behavior of an aircraft to be improved |
06/29/1993 | US5223776 Six-degree virtual pivot controller |
06/29/1993 | CA1319664C Segmentized flap system |
06/22/1993 | US5220861 Actuator with neutral position return |
06/01/1993 | US5216422 Control mechanism for use with an operator-actuated control member |
06/01/1993 | US5214972 Fault-tolerant linear electromechanical actuator |
05/25/1993 | US5213283 Low speed turn coordination for rotary wing aircraft |
05/18/1993 | CA1317796C Two motor redundant drive mechanism |
05/12/1993 | EP0460003B1 Drive device with variable torque-limiting system |
04/27/1993 | CA1317008C Aircraft precision approach control system |
04/14/1993 | EP0404772B1 Non-jamming rotary mechanical actuator |
04/06/1993 | US5199538 Drive device with variable torque-limiting system |
03/23/1993 | US5195700 Helicopter flight control system |
03/18/1993 | WO1993005463A1 Improved model following control system |
03/18/1993 | WO1993005462A1 Low speed model following velocity command system for rotary wing aircraft |
03/18/1993 | WO1993005461A1 High speed turn coordination for rotary wing aircraft |
03/18/1993 | WO1993005460A1 Low speed turn coordination for rotary wing aircraft |
03/18/1993 | WO1993005458A1 High speed yaw control system for rotary wing aircraft |
03/16/1993 | US5195039 Hover position hold system for rotary winged aircraft |
03/02/1993 | US5190503 Geared rotary actuator with internal stop mechanism |
03/02/1993 | US5190243 Device for the adjustment of the maneuver forces of movable members of an aircraft |
02/17/1993 | EP0527135A1 Method and apparatus for structural actuation and sensing in a desired direction |
02/16/1993 | US5186420 Articulated fin/wing control system |
02/16/1993 | US5186416 System for reducing the forces applied to the wings and particularly to the root of the wings of an aircraft in flight |
02/16/1993 | US5186415 Aircraft having means for controlling the ground effect flying altitude by sensing air pressure on the surface of the wing |
02/03/1993 | EP0525689A1 Translational hand controller |
02/02/1993 | US5184054 Friction actuator |
02/02/1993 | US5182961 Three degree of freedom translational axis hand controller mechanism |
01/26/1993 | US5182505 Aircraft control surface position transducer |
01/26/1993 | US5181380 Hydrostatic operating mode hydraulic actuator preferably for backup operation, and flight control system comprising it |
01/13/1993 | EP0522623A2 Mechanically-linked side stick controllers with isolated pitch and roll control movement |
01/12/1993 | US5178307 High speed yaw control system for rotary wing aircraft |
01/12/1993 | US5178030 Non-recirculating rotary ball actuator |
01/07/1993 | EP0521760A1 Device to adjust the operating effort of aircraft control members |
01/04/1993 | CA2072767A1 Device for adjusting the effort exerted to operate mobile equipment in an aircraft |
12/16/1992 | EP0518345A1 Hydraulic control system for aircraft |
12/01/1992 | CA1311034C Approach to hover control system for helicopters |
11/24/1992 | CA1310723C Associated afc and aed system |
11/05/1992 | DE4113504A1 Use of shape-memory alloys - by means of wire-wound torsion element |
10/29/1992 | DE4209946A1 Driving gear for control surfaces of model aircraft - transmits motion from single DC motor in fuselage through two=part gearing acting directly or indirectly |
10/20/1992 | US5156363 Helicopter collective stick of the displacement type occupying a minimum space envelope yet whose grip generates an arc of large radius |
09/23/1992 | EP0505071A2 A fin command mixing method |
09/22/1992 | US5149023 Mechanically-linked side stick controllers with isolated pitch and roll control movement |
09/16/1992 | EP0503801A2 Hand-operated controller |
09/15/1992 | CA1307573C Optimal flight guidance for aircraft in windshear |
09/10/1992 | DE4107133A1 Flight curve regulator for fighter aircraft - calculates aircraft rotation rate during flight curve using mach number |
09/08/1992 | US5144851 Jam tolerant linear actuator |
09/08/1992 | US5144801 Electro-hydraulic actuator system |
08/25/1992 | US5141177 Model following control system |
08/25/1992 | US5141092 Low spring rate mechanical stop |
08/25/1992 | US5141084 Brake stop |
08/11/1992 | US5137234 Sidestick controllers |
08/05/1992 | EP0497660A1 System for improving the flutter behaviour of an aircraft |
08/04/1992 | US5135186 Flutter control system for aircraft wings |
07/28/1992 | US5133698 Power driven actuator system |