Air turbine starter assembly

192 clutches and power-stop control – Clutches – Automatic

Reexamination Certificate

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Details

C192S113320

Reexamination Certificate

active

07086514

ABSTRACT:
An aircraft engine starter assembly has a starter motor, a notch containing plate rotationally coupled to the starter motor or the aircraft engine, a strut pocket containing plate rotationally coupled to the other of the starter motor or the aircraft engine, arranged facing the notch containing plate and spaced apart therefrom by an inter-plate space, wherein the strut pocket containing plate has a spring loaded strut mounted in at least one pocket thereof, aligned to engage a notch as the two plates rotate with respect to each other about a common centerline, so that the strut engages the notch to start the engine and releases from the notch when the engine is running. A lube oil pump is provided to force oil into the inter-plate space and bearings are provided coupled to the two plates to react the expansion forces created by the pressurized lube oil.

REFERENCES:
patent: 5052518 (1991-10-01), Trommer
patent: 5070978 (1991-12-01), Pires
patent: 5474152 (1995-12-01), Wilkinson et al.
patent: 5699889 (1997-12-01), Gadd
patent: 5806643 (1998-09-01), Fitz
patent: 5964331 (1999-10-01), Reed et al.
patent: 6032774 (2000-03-01), Gadd
patent: 6089112 (2000-07-01), Kelly et al.
patent: 6125979 (2000-10-01), Costin et al.
patent: 6244965 (2001-06-01), Klecker et al.
patent: 6338403 (2002-01-01), Costin et al.

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