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Device for measuring coaxiality of bearing seat of aero-engine combustion chamber casing

An aero-engine, coaxiality measurement technology, applied in mechanical measurement devices, measurement devices, mechanical devices, etc., to achieve the effects of real measurement data, convenient use and simple structure

Active Publication Date: 2015-04-29
AECC AVIATION POWER CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is: to propose a kind of coaxiality measuring device of casing bearing seat of aero-engine combustion chamber, to solve the coaxiality and beating of the diameter dimensions such as casing structural member bearing seat, mounting edge and engine rotor in casing test Quantitative measurement issues, to provide real and reliable data for engine aero-engine design and assembly

Method used

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  • Device for measuring coaxiality of bearing seat of aero-engine combustion chamber casing
  • Device for measuring coaxiality of bearing seat of aero-engine combustion chamber casing
  • Device for measuring coaxiality of bearing seat of aero-engine combustion chamber casing

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Embodiment Construction

[0011] The present invention will be described in further detail below. see Figure 1 to Figure 4 , aero-engine combustor case bearing seat coaxiality measuring device is characterized in that it consists of a positioning sleeve 4, a front needle roller bearing 5, a front stop ring 6, a rear needle roller bearing 7, a back stop ring 8, an end cover 9. End cover screw 10, bracket 11, bracket screw 12 and dial indicator 15; the positioning sleeve 4 is a cylinder, and the inner hole of the positioning sleeve 4 is divided into three sections: left, middle and right, and the left section hole 4a and the inner diameter of the right section hole 4c is greater than the inner diameter of the middle section hole 4b, the front needle roller bearing 5 is installed in the left section hole 4a and maintains a transition fit, the right end surface of the front needle roller bearing 5 and the left section hole 4a and the middle section hole 4b The end face of the step is fitted, the front st...

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Abstract

The invention belongs to an aero-engine measurement technology, and relates to a device for measuring the coaxiality of a bearing seat of an aero-engine combustion chamber casing. The device is characterized by consisting of a locating sleeve (4), a front needle rolling bearing (5), a front baffle ring (6), a rear needle rolling bearing (7), a rear baffle ring (8), an end cover (9), an end cover screw (10), a bracket (11), a bracket screw (12) and a dial indicator (15). The invention provides the device for measuring the coaxiality of the bearing seat of the aero-engine combustion chamber casing, so that the measurement problems of the diameter sizes of the components such as the bearing seat and a mounting side of the casing as well as the coaxiality and the jerk value of an engine rotor in the casing experiment can be solved, and the dynamic balance accuracy of the engine rotor can be guaranteed.

Description

technical field [0001] The invention belongs to the measurement technology of aero-engines, and relates to a coaxiality measurement device for a casing bearing seat of an aero-engine combustion chamber. Background technique [0002] In the test of the aero-engine casing, it is necessary to measure the coaxiality and runout of the engine rotor and the diameter of the bearing seat, mounting edge and other parts of the combustion chamber casing structure, see figure 1 , the right end of engine rotating shaft 1 is positioned at the inside of combustion chamber casing 2, and the right port of combustion chamber casing 2 has bearing block 3. The right end of the engine rotating shaft 1 is a two-stage stepped shaft, the left section of the two-stage stepped shaft is a large-diameter section 1a, the middle section is a middle-diameter section 1b, and the right end is a small-diameter section 1c. The inner cylindrical surface 3a of the central hole of the bearing seat 3 is a detecti...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01B5/252G01B5/08G01B5/00
Inventor 张宁马英刘忠华蒋学军杨立李林生夏毅
Owner AECC AVIATION POWER CO LTD
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