The invention discloses a test bed of an aircraft fuel system and relates to the technical field of aircraft fuel systems. The test bed of the aircraft fuel system comprises a bed strut (1), a bed platform (2), a bed scaling ladder (6), connecting parts (8) and supporting racks (9). The bed strut (1) is hinged to the bottom of the bed platform (2) to support the bed platform (2); the bed scaling ladder (6) is used for working personnel to step on the bed platform (2); one end of each supporting rack (9) is hinged to the bottom surface of the bed scaling ladder (6), and the other end of each supporting rack (9) is connected with one end of the bed platform (2). The connecting parts (8) are used for connecting the supporting racks (9) with the bed scaling ladder (6). The test bed has the advantages that the supporting rack, the bed scaling ladder and the bed platform of the test bed of the aircraft fuel system are integrally designed, the structure is light, the occupied area is small, the number of used supporting racks is small, the operation is convenient, and the test bed is suitable for fields with bearing trenches.
Test bed of aircraft fuel system
2015-12-23
Patent
Electronic Resource
English
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Aircraft Fuel System and Component Icing Test
SAE Technical Papers | 2012
Aircraft Fuel System and Component Icing Test
SAE Technical Papers | 2007
AIRCRAFT FUEL SYSTEM AND COMPONENT ICING TEST
SAE Technical Papers | 1979