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High-precision detection device for aero-engine blade film holes and detection method thereof

An aero-engine and engine blade technology, which is applied in the field of aero-engines, can solve problems such as difficult processing, and achieve the effects of high detection reliability, improved work efficiency, and easy transfer and preservation.

Pending Publication Date: 2021-11-19
宜兴市鑫煜科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, because the air film holes of the blade are distributed on the curved surface of the blade body, they are three-dimensional curved surface holes in space, and the hole diameter is small. Not only is the processing process difficult, but how to achieve accurate detection has always been a technical problem in the industry.

Method used

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  • High-precision detection device for aero-engine blade film holes and detection method thereof
  • High-precision detection device for aero-engine blade film holes and detection method thereof
  • High-precision detection device for aero-engine blade film holes and detection method thereof

Examples

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Effect test

Embodiment 1

[0033] Embodiment 1: as figure 1 , 2 A high-precision detection device for an air film hole of an aero-engine blade is shown, including a detection platform 1, a blade fixing component 2, a switching component 3, a thermal imaging detection component 4 and a controller; the detection platform 1 is provided with a blade cooling component 5 ;

[0034] Such as figure 1 , 4 , 5, the blade fixing assembly 2 includes a moving seat 20, a clamping seat 21 and a fastening motor 22, the moving seat 20 is fixedly arranged on the detection platform 1, and the side wall of the moving seat 20 is provided with an air inlet port 200; There are two seats 21, two clamping seats 21 are arranged side by side up and down on the upper end of the moving seat 20, and the clamping seat 21 at the top of the moving seat 20 is engaged with the moving seat 20 by sliding, and the fastening motor 22 is fixedly arranged on the The top of the moving seat 20, the output shaft of the fastening motor 22 is p...

Embodiment 2

[0046] Embodiment 2: as figure 1 , 2 A high-precision detection device for the air film hole of an aero-engine blade is shown, including a detection platform 1, a blade fixing component 2, a switching component 3, a thermal imaging detection component 4 and a controller; Moving groove 10, detection platform 1 tail end is provided with moving motor 11, and the output shaft of moving motor 11 is provided with first leading screw 110, and first leading screw 110 runs through moving groove 10 horizontally, and with the inner wall rotation card of moving groove 10 connected; the detection platform 1 is provided with a blade cooling assembly 5, and the upper end of the detection platform 1 is slidingly clamped with a transparent protective cover 6, and the transparent protective cover 6 is located outside the thermal imaging detection assembly 4; by setting the transparent protective cover 6, on the one hand, it can During the detection process, the blades are kept warm to improve ...

Embodiment 3

[0059] Embodiment 3: as figure 1 , 2 A high-precision detection device for the air film hole of an aero-engine blade is shown, including a detection platform 1, a blade fixing component 2, a switching component 3, a thermal imaging detection component 4 and a controller; Moving groove 10, detection platform 1 tail end is provided with moving motor 11, and the output shaft of moving motor 11 is provided with first leading screw 110, and first leading screw 110 runs through moving groove 10 horizontally, and with the inner wall rotation card of moving groove 10 connected; the detection platform 1 is provided with a blade cooling assembly 5; the upper end of the detection platform 1 is slidingly clamped with a transparent protective cover 6, and the transparent protective cover 6 is located outside the thermal imaging detection assembly 4; by setting the transparent protective cover 6, on the one hand, it can During the detection process, the blades are kept warm to improve the ...

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Abstract

The invention discloses a high-precision detection device for aero-engine blade film holes and a method thereof. The device comprises a detection platform, a blade fixing assembly, a switching assembly, a thermal imaging detection assembly and a controller. The blade fixing assembly, the switching assembly and the thermal imaging detection assembly are all arranged on the detection platform, the blade fixing assembly is used for clamping and fixing engine blades, the switching assembly is located at the front end of the blade fixing assembly and used for conveying the engine blades to the blade fixing assembly, the thermal imaging detection assembly is located on the outer side of the blade fixing assembly and used for detecting the quality of the air film hole in the engine blade, and the controller is electrically connected with each electric device; the device is reasonable in structural design, can perform multi-angle thermal imaging detection on the quality of the engine blade air film hole, has relatively high detection efficiency and accuracy, and is suitable for large-scale popularization.

Description

technical field [0001] The invention relates to the technical field of aero-engines, in particular to a high-precision detection device and a detection method for an air film hole in an aero-engine blade. Background technique [0002] As the sole source of aircraft flight power, the aeroengine is the core unit of the aircraft. Aeroengines are based on aerodynamics, starting from fan guide vanes, to low-pressure static, rotor blades, high-pressure static, rotor blades, high-pressure guide turbines and turbine blades, low-pressure turbine guides and turbine blades, etc., relying on a large number of different geometric shapes, sizes and functions. The blades enable the engine to continuously generate high-pressure gas, and the high-temperature and high-pressure gas is carried by the high-turbine blades to drive the turbine unit to work, and finally converted into aircraft flight power. [0003] Modern advanced aero-engines generally use small-hole film-cooled turbine blades t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M13/00G01J5/00
Inventor 吴烂平高寅风
Owner 宜兴市鑫煜科技有限公司
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