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Class Information
Number: 244/235
Name: Aeronautics > Aircraft control > Pilot operated > Controller > Rudder bar and pedal
Description: Apparatus comprising foot operated devices for controlling aircraft on land, sea, or in the air.










Patents under this class:

Patent Number Title Of Patent Date Issued
8584990 Method and device for yaw controlling of an aircraft Nov. 19, 2013
8485051 Apparatus and method for testing an aircraft pedal system Jul. 16, 2013
8353484 Cockpit rudder control mechanism for an aircraft Jan. 15, 2013
8197212 Power-assisted control system for a rotorcraft Jun. 12, 2012
7874526 Full authority fly-by-wire pedal system Jan. 25, 2011
7806372 Full authority fly-by-wire pedal system Oct. 5, 2010
7726611 Active rudder pedal mechanism with foreign object strike tolerance and articulating brake Jun. 1, 2010
7690604 Rudder pedal assembly including non-parallel slide rails Apr. 6, 2010
7644893 Full authority fly-by-wire pedal system Jan. 12, 2010
6675076 System, autopilot supplement assembly and method for increasing autopilot control authority Jan. 6, 2004
6526338 Electrical fly-by-wire system for operating an aircraft rudder Feb. 25, 2003
5833173 Aircraft frequency adaptive modal suppression system Nov. 10, 1998
5791596 Process and device for the control of the rudder of an aircraft Aug. 11, 1998
5738310 Rudder bar system with force gradient for a helicopter Apr. 14, 1998
5725184 Brake rudder pedal system for light aircraft Mar. 10, 1998
5056742 Modular rudder pedal and brake control assembly for aircraft Oct. 15, 1991
4848708 Adjustable assembly for aircraft rudder, brake and nose landing gear steering control Jul. 18, 1989
4489904 Actuating mechanism for an auxiliary power source Dec. 25, 1984
4484722 Translating rudder pedal system Nov. 27, 1984
4470570 Control assembly for aircraft Sep. 11, 1984
4206891 Helicopter pedal feel force proportional to side slip Jun. 10, 1980
4192476 Rudder pedal adjustment system Mar. 11, 1980
3931943 Airplane rudder and controls Jan. 13, 1976











 
 
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