Support system for auxiliary power unit

Details Support system for auxiliary power unit Support system for auxiliary power unit

2011-03-22

2011-03-22

Michener, Joshua J (Department: 3644)

Aeronautics and astronautics

Aircraft power plants

Auxiliary

C244S054000

Reexamination Certificate

active

07909286

ABSTRACT:
Support system suitable for sustaining an auxiliary power unit of an aircraft to a fixed structure (2) belonging to a compartment of the auxiliary power unit (6) of the aircraft. The support system is made in a high mechanical strength material and with high resistance to ignition, and comprises three fittings (3, 4, 5) two of which are frusto-conical and one with a substantially cylindrical. Fittings (3, 4, 5) being able to be hollow and being able to comprise an array of lateral ribs. Each one of them presenting a first end (7) comprising means of attachment of the support system (8) to the fixed structure (2) and a second end (9) comprising means of securing of the support system (8) which are joined to the auxiliary power unit (1) in the periphery of the extension of said auxiliary power unit (1).

REFERENCES:
patent: 3151464 (1964-10-01), Sato et al.
patent: 3204897 (1965-09-01), Lawrence
patent: 6247668 (2001-06-01), Reysa et al.
patent: 6581874 (2003-06-01), Lemire et al.
patent: 2006/0032974 (2006-02-01), Williams
patent: 2006/0144050 (2006-07-01), Williams
patent: 2006/0273221 (2006-12-01), Olsen et al.

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