Structure for mounting a turboprop under an aircraft wing

Aeronautics and astronautics – Aircraft power plants – Mounting

Reexamination Certificate

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Details

C060S797000

Reexamination Certificate

active

10986870

ABSTRACT:
A structure for mounting a turboprop under an aircraft wing includes a rigid structure and a device for fastening the turboprop on the rigid structure. The rigid structure is composed of a box, and the device for fastening includes at least two lateral connecting rods resisting the engine torque generated by the turboprop, the connecting rods being arranged on each side of the box and each having a forward end connected to a gear box of the turboprop, and an aft end connected to the box.

REFERENCES:
patent: 4037809 (1977-07-01), Legrand
patent: 5065959 (1991-11-01), Bhatia et al.
patent: 5409184 (1995-04-01), Udall et al.
patent: 5806792 (1998-09-01), Brossier et al.
patent: 5871177 (1999-02-01), Demouzon et al.
patent: 6126110 (2000-10-01), Seaquist et al.
patent: 2 291 091 (1976-06-01), None

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