The application belongs to the technical field of
airplane debugging process, and particularly relates to a process method and a special
test bench for an
airplane canopy cover
air tightness and strength test, comprising an
oil tank, a manual pump, a
reversing valve, a process actuating cylinder and a controller. The
reversing valve is a three-position four-way
reversing valve. Two oil ports on one side of the reversing valve are connected with the manual pump and the
oil tank, and two oil ports on the other side of the reversing valve are connected with the inlet and outlet oil ports of the process actuating cylinder through hydraulic rubber pipes. The
oil tank and the manual pump are connected with each other. The manual pump and the reversing valve are provided with sensors, and the sensors are electrically connected with the controller. The
assembly process of the
canopy cover pneumatic hydraulic
system is successfully moved to the final
assembly stage, and the process cross and repeated disassembly in the
assembly and final assembly stages are completely avoided. The
air tightness and strength test in the assembly stage can be independently and advancedly carried out, and the overall
production cycle of the
airplane is greatly compressed.