Turbine engine disk spacers

Details Turbine engine disk spacers Turbine engine disk spacers

2006-04-21

2008-01-29

Look, Edward K. (Department: 3745)

Metal working

Method of mechanical manufacture

Impeller making

C029S401100, C415S199500

Reexamination Certificate

active

07322101

ABSTRACT:
A gas turbine engine rotor stack may be engineered or reengineered to include one or more longitudinally outwardly concave spacers. The spacers may provide a longitudinal compression force that increases with rotational speed.

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patent: 595643 (1947-12-01), None
European Search Report for EP Patent Application No. 05252294.3.

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