Aircraft engine mounting assembly

Power plants – Combustion products used as motive fluid – Having mounting or supporting structure

Reexamination Certificate

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Details

C060S226100, C224S042210

Reexamination Certificate

active

10954277

ABSTRACT:
A mounting assembly (10) for mounting a gas turbine engine on an aircraft. The assembly (10) comprising four equispaced hydraulic piston and cylinder thrust links (16) connecting between the engine fan case (12) and the air intake (14), which intake (14) is mounted to the airframe.

REFERENCES:
patent: 3997134 (1976-12-01), Drakeley
patent: 4022018 (1977-05-01), Tuten et al.
patent: 4361296 (1982-11-01), Hall et al.
patent: 4458863 (1984-07-01), Smith
patent: 5000399 (1991-03-01), Readnour et al.
patent: 5372338 (1994-12-01), Carlin
patent: 6892526 (2005-05-01), Stretton et al.

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