Apparatus and method for mounting a cascade support ring to...

Aeronautics and astronautics – Retarding and restraining devices – Friction brakes

Reexamination Certificate

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C060S226200, C239S265190

Reexamination Certificate

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06915984

ABSTRACT:
A thrust reverser for a jet engine of a mobile platform. The thrust reverser includes a hinge beam defining a first track and a latch beam defining a second track. The thrust reverser also includes at least one cascade support ring having an upper end portion and a lower end portion. A first fitting is disposed at the upper end portion of the cascade support ring. The first fitting includes an engagement portion slidably positioned within the first track. A second fitting is disposed at the lower end portion of the cascade support ring. The second fitting includes an engagement portion slidably positioned within the second track.

REFERENCES:
patent: 5778659 (1998-07-01), Duesler et al.
patent: 6584763 (2003-07-01), Lymons et al.
patent: 6592074 (2003-07-01), Dehu et al.
U.S. Appl. No. 10/758,887, filed Jan. 16, 2004, McAuley.

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