Special test device of ice ingestion of turboprop engine

A test device and engine technology, applied in the direction of engine testing, measuring devices, machine/structural component testing, etc., can solve problems affecting the safety of aircraft operation passengers, damage to engine blades, etc., and achieve ingenious and flexible adjustment methods and simple structure , the effect of large adjustment range

Active Publication Date: 2016-06-15
CHINA AVIATION POWER MACHINE INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] During the flight, the aircraft often encounters sudden hail from the sky. Damage to the shell or other parts of the aircraft will seriously affect the operation of the aircraft and the safety of passengers in the aircraft. Especially when the hail enters the engine, the hail May damage the blades of the engine with serious consequences

Method used

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  • Special test device of ice ingestion of turboprop engine
  • Special test device of ice ingestion of turboprop engine
  • Special test device of ice ingestion of turboprop engine

Examples

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Embodiment Construction

[0036] The embodiments of the present invention will be described in detail below with reference to the accompanying drawings, but the present invention can be implemented in many different ways defined and covered by the claims.

[0037] This embodiment provides a special test device for swallowing ice of a turboprop engine, such as figure 1 As shown, it includes a bracket 1, an ice-throwing guide rail, a mobile adjustment frame, an insulation box 2, an electromagnet 3 and a horizontal support plate 4; the ice-throwing guide rail includes straight rails 5 and curved rails 6 connected to each other; the bracket 1 stands on the ground It is used to support the curved rail 6; the moving adjustment frame includes horizontal moving guide rails and an adjusting frame 8 perpendicular to each other, and the horizontal moving guide rail is fixed on the ground; one end of the straight rail 5 is connected to the curved rail 6, and the other end is fixed to the adjusting frame 8. The adj...

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PUM

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Abstract

The invention provides a special test device of ice ingestion of a turboprop engine. The device comprises a support, an ice feeding track, a moving adjustment support, a heat insulation box, an electromagnet and a horizontal support plate. The moving adjustment support comprises a horizontal moving track and an adjustment support. The angle between the ice feeding track and the adjustment support can be changed by moving the adjustment support along the horizontal moving track, so that the feeding speed and angle of ice blocks can be adjusted. Balance and inclination of the heat insulation box is controlled by connection and disconnection of current inside the electromagnet. Furthermore, a plurality of screw holes are arranged in the adjustment support to adjust the heights of the ice feeding track, the heat insulation box and the electromagnet. A plurality of screw holes are arranged in the support for fine adjustment of the height of the ice feeding track. A straight track of the provided ice feeding track is composed of a plurality of segments, so that the height of the ice feeding track can be adjusted. The device can conduct coarse adjustment and fine adjustment of the included angle between the ice feeding track and the adjustment support either horizontally or vertically. The structure is simple, the production cost is low, the adjustment method is smart and flexible, the adjustment range is wide, and the adaptability is high. The device can quickly and easily control the ice feeding speed and angle.

Description

technical field [0001] The invention relates to the technical field of engines, and more particularly, to a special test device for ice swallowing of a turboprop engine. Background technique [0002] During the flight, the aircraft often encounters sudden hail from the sky. Damage to the shell or other parts of the aircraft will seriously affect the operation of the aircraft and the safety of passengers in the aircraft. Especially when the hail enters the engine, the hail Damage to the blades of the engine may have serious consequences. Therefore, before the aircraft is put into use, a device needs to be studied to carry out the ice swallowing special test on the engine of the aircraft. [0003] The device should be able to store a piece of ice (10-20) min at a certain temperature, and can be remotely controlled to release the ice. The speed and angle of the ice sheet sliding out of the ice throwing device should be controllable. Contents of the invention [0004] The te...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M15/00
CPCG01M15/00
Inventor 邓楚慧贾宗芸邹植伟杨飞熊荆江
Owner CHINA AVIATION POWER MACHINE INST
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