US 12,214,861 B2
Aircraft rudder pedal frame
Eric Granier, Saint-Cloud (FR); and Vincent Mateus, Saint-Cloud (FR)
Assigned to DASSAULT AVIATION, Paris (FR)
Filed by DASSAULT AVIATION, Paris (FR)
Filed on Mar. 6, 2023, as Appl. No. 18/118,125.
Claims priority of application No. 22 01930 (FR), filed on Mar. 7, 2022.
Prior Publication US 2023/0278697 A1, Sep. 7, 2023
Int. Cl. B64C 13/04 (2006.01); B64C 13/06 (2006.01); B64C 13/12 (2006.01); B64C 13/50 (2006.01)
CPC B64C 13/044 (2018.01) [B64C 13/06 (2013.01); B64C 13/12 (2013.01); B64C 13/50 (2013.01)] 20 Claims
OG exemplary drawing
 
1. A frame for a rudder pedal comprising:
a base;
a support framework; and
connection interfaces, each connection interface being configured to connect another part of the rudder pedal to the frame,
the support framework connecting each connection interface to the base, the support framework comprising framework elements arranged in a lattice, at least one of the framework elements extending from each connection interface,
wherein the connection interfaces comprise at least four pedal interfaces divided into two distinct pairs of pedal interfaces, each pair corresponding to connection interfaces of a pedal articulated support structure of the rudder pedal, the two pairs being arranged on either side of a longitudinal median plane of the frame, each pair comprising a distal pedal interface and a proximal pedal interface.