CPC G01M 15/14 (2013.01) [B64D 31/00 (2013.01); B64F 5/60 (2017.01); G01M 15/02 (2013.01)] | 16 Claims |
1. A system for operating an aircraft engine, the system comprising:
a main fuel conduit;
a first end of a main fuel conduit configured to connect into an engine fuel delivery system existing on a first aircraft;
a second end of the main fuel conduit configured to connect into an engine fuel intake on an aircraft engine being tested, the aircraft engine being tested not being associated with the first aircraft;
the main fuel conduit being elongated to interconnect the engine fuel delivery system on the first aircraft and the aircraft engine being tested;
a motive fuel conduit, the motive fuel conduit configured on a first end to be coupled into a motive fuel output included in the engine fuel delivery system on the first aircraft, the motive fuel conduit configured on a second end to be coupled to an aircraft motive fuel intake on the engine being tested; and
the main and motive fuel conduits being configured to extend between the engine on the first aircraft and the aircraft engine being tested.
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