Pilot control system with adjustable pedals

According to one embodiment, a method of adjusting an aircraft pedal assembly (700) includes providing a pedal linkage (730a, 730b) coupled between a pedal (720a, 720b) and an attachment assembly (710) situated proximate to an aircraft instrument panel. A brake cylinder (740a, 740b) is provided coup...

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Bibliographische Detailangaben
Hauptverfasser:	LINTON, BRADLEY D, YATES, TRAVIS L
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION TECHNICAL SUBJECTS COVERED BY FORMER USPC TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TRANSPORTING
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Beschreibung
Zusammenfassung:	According to one embodiment, a method of adjusting an aircraft pedal assembly (700) includes providing a pedal linkage (730a, 730b) coupled between a pedal (720a, 720b) and an attachment assembly (710) situated proximate to an aircraft instrument panel. A brake cylinder (740a, 740b) is provided coupled between the pedal (720a, 720b) and the attachment assembly (710). The pedal linkage (730a, 730b) is rotated in response to an adjustment input. The pedal linkage (730a, 730b) is maintained approximately parallel to the brake cylinder (740a, 740b) during rotation of the pedal linkage (730a, 730b).