Test run control device of airplane auxiliary power device

The invention discloses a test run control device of an airplane auxiliary power device, which comprises a supporting table, a piano-type console is arranged on one side of the supporting table, the piano-type console is fixedly connected to one end of the supporting table, an APU is arranged at one...

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Bibliographic Details
Main Author NIE ERBING
Format Patent
LanguageChinese
English
Published 14.06.2024
Subjects
ADVERTISING
APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND,DEAF OR MUTE
CRYPTOGRAPHY
DIAGRAMS
DISPLAY
EDUCATION
EDUCATIONAL OR DEMONSTRATION APPLIANCES
GLOBES
PHYSICS
PLANETARIA
SEALS
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Summary:The invention discloses a test run control device of an airplane auxiliary power device, which comprises a supporting table, a piano-type console is arranged on one side of the supporting table, the piano-type console is fixedly connected to one end of the supporting table, an APU is arranged at one end, far away from the piano-type console, of the supporting table, the APU is fixedly connected to the supporting table, and a cross beam is fixedly connected to the back of the piano-type console. The fuel tank is installed on the piano-type control table, a fuel shutoff electromagnetic valve is arranged on one side of the fuel tank and fixedly connected to the piano-type control table, a low-pressure fuel pump is arranged on one side of the fuel shutoff electromagnetic valve and fixedly connected to the piano-type control table, and a fuel turbine flowmeter is arranged between the low-pressure fuel pump and the APU. The instrument monitoring system is high in integration level, does not need external power supp
Bibliography:Application Number: CN202410406382