Patent ID: 11866157
Assignee: AIRBUS OPERATIONS LIMITED
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 13:
14. The A landing gear support comprising:
a gear rib including an upper flange configured to support an upper wing skin, a lower flange configured to support a lower wing skin, a forward flange configured to attached to a wing spar,
a first support portion including:
a first mount having a first surface abutting the web of the gear rib and a second surface opposite to the first surface, and
first pintle supports integral with and forming a single piece component with the first mount, the first pintle supports extend outward from the first surface of the first mount, and the first pintle supports each include a first aperture configured to receive a first pintle to rotatably support a landing gear assembly attached to the first pintle,

a second support portion including:
a second mount having a first surface abutting the web of the gear rib and a second surface opposite to the first surface, and
a second pintle support integral with and forming a single piece component with the second mount, the second pintle support extends outward from the first surface of the second mount, and the second pintle support includes a second aperture configured to receive a second pintle to rotatably support the landing gear assembly attached to the second pintle,
wherein the first mount and the first pintle support are removably attached to the web of the gear rib separately from the second mount and the second pintle support.