Assembly for handling an aircraft engine
A technology of aircraft engine and assembly device, applied in the direction of lifting device, ground device, aircraft parts, etc., can solve the problems of no use of connecting device, no other characteristics, no complete tilt of the unit body, etc.
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[0015] In this embodiment of the invention, the aircraft engine unit 1 is referred to as the "core", or high pressure body. This is a large intermediate unit that includes the compressor and high-pressure turbine as well as the combustion chamber. From Figure 1 to Figure 3 It can be seen that it is assembled on a bracket 2 comprising a frame 3 , rollers 4 mounted on the frame 3 and a reinforcing structure 5 raised from the frame 3 and supporting the unit body 1 . The bracket 2 is lifted from the ground by a lifting device 6 and supported, said lifting device 6 comprising a frame 7 and in particular an upper platform 8 on the frame 7 on which the frame 3 of the bracket 2 is mounted, And there are braces 10 mechanisms 9 connected in between, these braces are located between the platform 8 and the ground, when the connection angle of the braces 10 is changed by the jack 11, the platform is raised. Another part of the device is the tool 12, which is similar in shape to the cove...
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