Method of removing a fan section of a jet engine

Metal working – Method of mechanical manufacture – Impeller making

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Details

187244, B23P 1500

Patent

active

058708243

ABSTRACT:
A jet aircraft engine transport apparatus utilizes three major subcomponents. The first subcomponent is a shipping stand which enables a jet aircraft engine to be configured for transport in either a truck transport mode or air transport mode. The second subcomponent is a fan dolly which releasably secures the fan section of the jet aircraft engine for transport. The fan dolly serves the dual purpose of enabling removal of the fan section from the jet aircraft engine and providing a means of transport so that the fan section may be transported on the fan dolly or loaded onto a fan shipping frame, the third major subcomponent of the transport apparatus of this invention. The fan shipping frame enables transport of the fan section in either an upright or horizontal position, and further provides for a fan storage container for securing the fan blades of the fan section.

REFERENCES:
patent: 2594586 (1952-04-01), Ries
patent: 2613807 (1952-10-01), Higbee
patent: 2670166 (1954-02-01), Applegate
patent: 2674370 (1954-04-01), Iredell, III
patent: 2674371 (1954-04-01), Blackinton
patent: 2928535 (1960-03-01), Simmons et al.
patent: 2982395 (1961-05-01), Rados
patent: 3194525 (1965-07-01), Webb
patent: 3211299 (1965-10-01), Metzrath
patent: 4117927 (1978-10-01), Gothsche
patent: 4451979 (1984-06-01), Schuster
patent: 4660796 (1987-04-01), Garrec
patent: 4699337 (1987-10-01), Lewis
patent: 5383652 (1995-01-01), Van Den Berg
patent: 5575145 (1996-11-01), O'Neill et al.
No. 1: Product information advertisement by applicant Re: Core Engine Module.
No. 2: Product information advertisement by applicant Re: various types of ground support equipment to secure and transport components of a jet aircraft.
No. 3: Product information advertisement by applicant Re: a cradle device for securing components of a jet aircraft engine.
No. 4: Product information advertisement by applicant Re: a cradle device for securing components of a jet aircraft engine.
No. 5: Product information advertisement by applicant Re: Engine Stand.
No. 6: Product information advertisement by applicant Re: Hydraulic Engine Stand.
No. 7: Relevant portions of a product information catalog by Advance Ground Systems Engineering Corporation of Anaheim, California (23 Oct. 1990).

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