Ground testing installation for an aircraft jet engine having a

Measuring and testing – Test stand – For engine

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G01M 1500

Patent

active

052302415

ABSTRACT:
A ground testing installation for an aircraft jet engine having a nozzle that is steerable relative to the longitudinal axis of said engine, the installation comprising:

REFERENCES:
patent: 2804455 (1958-12-01), Hirschorn
patent: 2886121 (1959-05-01), Welbourn
patent: 3205705 (1965-09-01), Talley
patent: 3525418 (1970-08-01), Smith et al.
patent: 4168763 (1979-09-01), White et al.
patent: 4987970 (1991-01-01), Boet
Lemmerman et al., "Aircraft Run-Up Silencing Design", Noise Control, vol. 2, No. 1, Jan. 1956, pp. 10-14, 65.

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