Alignment and positioning system for installing a fuel...

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

Reexamination Certificate

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Details

C060S740000

Reexamination Certificate

active

11087046

ABSTRACT:
A fuel injector for a gas turbine engine is disclosed wherein the engine has an engine case that includes a reception bore for accommodating the fuel injector, and wherein the fuel injector includes a fuel inlet fitting having an annular mounting flange defining opposed upper and lower end surfaces and a cylindrical body portion which depends axially from the lower end surface of the mounting flange, the inlet fitting having integrally formed alignment structure located beneath the lower end surface of the mounting flange for guiding the fuel injector into an installed position within the reception bore of the engine case.

REFERENCES:
patent: 2422214 (1947-06-01), Meyer et al.
patent: 3398529 (1968-08-01), Schmitz et al.
patent: 3458997 (1969-08-01), Clark
patent: 3879940 (1975-04-01), Stenger et al.
patent: 6354085 (2002-03-01), Howell et al.
patent: 0 837 284 (1998-04-01), None
patent: 1 286 111 (2003-02-01), None
EPO Search Report dated Mar. 30, 2006.

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