Novel civil aviation engine and important component equipment

Abstract

The invention discloses a novel civil aviation engine and important component equipment. The novel civil aviation engine comprises a fixing base, wherein foot columns are fixedly arranged around the bottom surface of the fixing base, rolling wheels are arranged at the bottom parts of the foot columns, a pushing armrest is fixedly arranged on the left end surface of the fixing base, a lower machinebody is fixedly connected onto the upper end surface of the fixing base, an upper machine body is arranged on the upper side of the lower machine body, an operation part is arranged between the uppermachine body and the lower machine body, a left supporting plate and a right supporting plate are respectively arranged at both the left end and the right end of the operation part, a lower seat block is fixedly connected onto the upper end surface of the lower machine body rotationally, an upper seat block is fixedly connected onto the lower end surface of a limiting plate, a display screen is fixedly arranged on the right side of the front end surface of the upper machine body, a signal light is fixedly connected to the right side of the upper end surface of the upper machine body, and an electronic ruler is fixedly connected to the left side of a landing block. In the operation, the electronic ruler can measure different gap values of one revolution of a workpiece, and after being processed by a system, specific values are displayed, and when the gap values are too large, the display screen controls the signal light to work.

Description

technical field

[0001] The invention relates to the field of aviation, in particular to a novel civil aeroengine and important component equipment. Background technique

[0002] Aviation engine refers to the engine that provides the power required for the flight of the aircraft. It is mainly used to generate pull or thrust to make the aircraft move forward. A large number of output shafts are used in aero-engines and other important components, and the output shaft is equipped with a ring gear. Under the existing technical conditions, the assembly of the output shaft and the ring gear relies on manual work, which is time-consuming and laborious. The spacing is difficult to control and the precision is low. Contents of the invention

[0003] The object of the present invention is to provide a novel civil aeroengine and important component equipment to solve the problems raised in the above-mentioned background technology.

[0004] In order to achieve the above object, the...

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