Gas turbine nose cone attachment

Fluid reaction surfaces (i.e. – impellers) – Support mounting – carrier or fairing structure – Spinner or fairwater cap

Patent

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Details

415201, 411175, 411970, B64C 1114

Patent

active

055733786

ABSTRACT:
A nose cone on the fan of a gas turbine engine contains access holes that provide access to cap screws that hold the nose cone on the fan hub. The cap screws extend through an internal flange on the nose cone. A spring clip extends from the flange in a configuration that covers the access hole and holds the cap screw in the flange as the nose cone is installed.

REFERENCES:
patent: 2371801 (1945-03-01), Chester et al.
patent: 2394749 (1946-02-01), Chester
patent: 3799693 (1974-03-01), Hull
patent: 4393650 (1983-07-01), Pool

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