Engine testing mounting adaptor

Measuring and testing – Test stand – For engine

Patent

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Details

248554, 269 46, 269909, G01L 110

Patent

active

053967917

ABSTRACT:
A flexible adaptor mounts an aircraft gas turbine engine to a test stand. The adaptor includes an upper frame configured for mounting on the test stand, and a lower frame spaced from the upper frame and configured for supporting the engine. A spring flexibly joins the lower frame to the upper frame to simulate the flexibility of an aircraft wing which supports the engine during operation.

REFERENCES:
patent: 3834221 (1974-09-01), Swis et al.
patent: 4174627 (1979-11-01), Swis et al.
patent: 4511112 (1985-04-01), Ruehle
patent: 4660796 (1987-04-01), Garrec
patent: 4848717 (1989-07-01), Bevill
patent: 4875374 (1989-10-01), Pinson
patent: 4932628 (1990-06-01), Pacheco
patent: 5085396 (1992-02-01), Mansson

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