Hydraulic test device for detachable housing of combustion chamber case of aeroengine

A technology of aero-engine and hydraulic test, which is applied in engine test, liquid-tightness measurement using liquid/vacuum degree, measuring device, etc. It can solve the problems of rigidity and strength that cannot be known to meet the requirements, and achieve convenient handling and rigidity. Good strength and reduced device weight

Active Publication Date: 2016-04-13
CHENGDU ENGINE GROUP
View PDF6 Cites 8 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, in the prior art, there is no special experimental device for corresponding tests on the detachable shell, and this test has not been carried out, and it is impossible to know whether the rigidity and strength of the detachable shell after processing meet the requirements

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Hydraulic test device for detachable housing of combustion chamber case of aeroengine

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0020] This embodiment is used for the device of the hydraulic test of the casing of the combustor casing of the aero-engine, and its structure is shown in Figure 1. The object of the hydraulic test is the removable casing 4, which is a component part of the casing of the combustor of a certain type of aero-engine. The two-part cylindrical body is assembled by assembly bolts 19, and the cylindrical body is a thin-wall sandwich structure, and a plurality of openings are processed on the wall surface of the cylindrical body. The hydraulic test device consists of a base 1, a base plate 2 fixedly arranged on the base and connected with the lower end of the detachable shell 4 of the component to be tested, an inner cylinder 5 located at the inner lower end of the detachable shell connected with the base plate and the base, and connected with the upper end of the inner cylinder The cover plate 9 is located at the outer cylinder body 6 where the lower end of the inner cylinder body is...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The invention discloses a hydraulic test device for a detachable housing of a combustion chamber case of an aeroengine. The test device comprises a pedestal, a base plate, an inner cylinder, a cover plate, an outer cylinder and a plug, wherein the base plate is arranged on the pedestal and connected with the lower end of the detachable housing of a part to be tested, the inner cylinder is placed at the inner lower end of the detachable housing and connected with the base plate and / or the pedestal, the cover plate is connected with the upper end of the inner cylinder, the outer cylinder is placed at the outer lower end of the inner cylinder and connected with the upper end of the detachable housing, the upper end of the outer cylinder is connected with the cover plate, and the plug is used to plug an opening in the detachable housing. The base plate, the inner cylinder, the cover plate, the outer cylinder and the detachable housing to be tested form a hydraulic annular enclosed space, and a part of the hydraulic annular enclosed space is provided with a hydraulic medium injection pipeline interface assembly, a hydraulic medium discharge pipeline interface assembly and an internal air discharge pipeline interface assembly of the annular enclosed space. The device can be used to detect the intensity, rigidity and welding compactness of the detachable housing, product is prevented from blindness, and guarantee is provided for producing combustion chamber cases, which satisfy using requirements, of the aeroengine.

Description

technical field [0001] The invention relates to the technical field of hydraulic test of a detachable case of an aero-engine combustion chamber, in particular to a device for hydraulic test of a detachable case of an aero-engine combustion chamber. Background technique [0002] The combustor casing is an important part of the aero-engine, and there are strict requirements for the strength, rigidity, sealing of the end face and whether the weld seam has leakage. The combustor casing is composed of a diffuser and a detachable casing, wherein the detachable casing is a thin-walled double-layer cylindrical structure, and the cylinder wall is designed with openings of different diameters. Before the experimental device of the present invention is completed, the enterprise mainly guarantees the strength, rigidity, and tightness of the weld seam of the detachable shell from the design and processing technology, so as to meet the use requirements of the assembled combustion chamber ...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
Patent Type & Authority Applications(China)
IPC IPC(8): G01M15/00G01M5/00G01M3/02
CPCG01M3/025G01M5/00G01M15/00
Inventor 陈静刘建
Owner CHENGDU ENGINE GROUP
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products