US 11,897,602 B2
Support structure for an aircraft landing gear
Muhammad Mustajab Malik, Mukilteo, WA (US); and Waeil M. Ashmawi, Bellevue, WA (US)
Assigned to THE BOEING COMPANY, Arlington, VA (US)
Filed by The Boeing Company, Chicago, IL (US)
Filed on Mar. 8, 2022, as Appl. No. 17/689,169.
Claims priority of provisional application 63/162,225, filed on Mar. 17, 2021.
Prior Publication US 2022/0297824 A1, Sep. 22, 2022
Int. Cl. B64C 25/04 (2006.01); B64C 3/18 (2006.01)
CPC B64C 25/04 (2013.01) [B64C 3/185 (2013.01); B64C 3/187 (2013.01)] 20 Claims
OG exemplary drawing
 
1. A support structure to mount a landing gear to a wing spar of an aircraft, the support structure comprising:
a trunnion support assembly comprising a first trunnion support and a second trunnion support that are connected together with the first trunnion support positioned on a first side of the wing spar and a second trunnion support positioned on an opposing second side of the wing spar, each of the first trunnion support and the second trunnion support comprising stiffener plates that form perimeter sides that extend around a central area and a face plate connected to the stiffener plates to fully enclose one side of the central area, the trunnion support assembly configured to support a first section of the landing gear.