Provision of sealing in a jet engine for bleeding air to the...

Power plants – Combustion products used as motive fluid – For nominal other than power plant output feature

Reexamination Certificate

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C060S751000

Reexamination Certificate

active

07409831

ABSTRACT:
A jet engine that provides for the sealing of bleeding air to the cabin, the air passing through a cavity delimited, on the one hand, by the external shell of the compressor and an annular structure connected to the shell, and, on the other hand, by the external casing of the diffuser grating and a strut connected to the external casing and to an external engine casing shell, this external casing shell being fastened to the annular structure by bolting. A tube is provided between the orifice in the strut and the outlet vent, a first end of which tube is mounted in the outlet vent by a connection which is free to rotate and prevented from translational movement, and a second end of which tube is mounted in the orifice by a connection which is free to rotate and free to move translationally.

REFERENCES:
patent: 4554789 (1985-11-01), Napoli et al.
patent: 4870826 (1989-10-01), Daguet et al.
patent: 6783324 (2004-08-01), Muny
patent: 6843059 (2005-01-01), Burrus et al.
patent: 7040098 (2006-05-01), Lepretre et al.
patent: 2005/0056025 (2005-03-01), Lepretre et al.
patent: 0 162 340 (1985-11-01), None
patent: 1 247 944 (2002-10-01), None

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