Patent ID: 11897602
Assignee: THE BOEING COMPANY
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 12:
13. A support structure to mount a landing gear to a wing spar of an aircraft, the support structure comprising:
a first trunnion support mounted to a rear side of the wing spar, the first trunnion support configured to connect to a forward section of the landing gear; and
a second trunnion support mounted on an opposing front side of the wing spar and connected to the first trunnion support;
a frame mounted to the first trunnion support and extending outward from the first trunnion support in a rear direction away from the wing spar and configured to connect to a rear section of the landing gear, the frame comprising a rib with a first end connected to the first trunnion support and a second end positioned outward away from the wing spar to support the rear section of the landing gear;
wherein the first trunnion support and the second trunnion support are aligned in an overlapping arrangement on the opposing front and rear sides of the wing spar;
wherein the second trunnion support is connected to the frame just through the connection with the first trunnion support.