Hinge device of a nacelle cowling of an aircraft engine on a...

Details Hinge device of a nacelle cowling of an aircraft engine on a... Hinge device of a nacelle cowling of an aircraft engine on a...

2011-06-14

2011-06-14

Michener, Joshua J (Department: 3644)

Aeronautics and astronautics

Aircraft structure

Details

C244S054000

Reexamination Certificate

active

07959107

ABSTRACT:
A hinge device of a nacelle cowling of an aircraft engine on a supporting structure is disclosed. The hinge device includes two fittings and a link rod connected thereto and mounted on the fitting by an end connection. The link rod is further mounted on the fitting by an intermediate connection including a pivot pin slidably housed in a hole, and the end connection includes a guide pin slidably housed in a guide ramp. The connections are designed so as to create, upon rotation of the link rod about the pin, a relative movement of the axis in the ramp, simultaneously causing a relative movement of the pin in the hole.

REFERENCES:
patent: 4585189 (1986-04-01), Buxton
patent: 5203525 (1993-04-01), Remlaoui
patent: 5275357 (1994-01-01), Seelen et al.
patent: 6401299 (2002-06-01), Schwarz
patent: 7147185 (2006-12-01), Beaufort
patent: 1 245 769 (2002-10-01), None
patent: 2 715 185 (1995-07-01), None

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