Engine simulation apparatus

Measuring and testing – Simulating operating condition – Engine specific

Reexamination Certificate

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Details

C073S112010, C073S116030, C073S118030

Reexamination Certificate

active

08082778

ABSTRACT:
The present invention relates to a turbofan propulsion simulator means, in particular for a turbofan of an aircraft or spacecraft, wherein the turbofan propulsion simulator means comprises a modular configuration, wherein the turbofan propulsion simulator means comprises a module, wherein the module is a turbine means to drive the turbofan of the turbofan propulsion simulator means, wherein the turbine means can be coupled with at least two fan means, characterized in that, the at least two fan means to be connected with the turbofan propulsion simulator means comprises almost or essentially the same mass and/or almost or essentially the same barycentre.

REFERENCES:
patent: 4033185 (1977-07-01), McNally et al.
patent: 4034604 (1977-07-01), Decher et al.
patent: 4189939 (1980-02-01), West et al.
patent: 4691561 (1987-09-01), Ganz et al.
patent: 4742709 (1988-05-01), Angel
patent: 6772627 (2004-08-01), Fleming
patent: 6923051 (2005-08-01), Fleming
patent: 7024929 (2006-04-01), Fleming et al.
Kemp, B.C., AIAA 94-2554 “Next Generation Propulsion Simulation Equipment for Use in Wind Tunnels”, 18thAIAA Aerospace Ground Testing Conference, Jun. 20-23, 1994, Colorado Springs, CO.

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