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Turboshaft engine intake device and operation method

A turboshaft engine and air intake device technology, which is applied in the direction of engine components, turbine/propulsion device air intake, charging system, etc., can solve the problems of circumferential uneven sealing, difficulty, and engineering application difficulty , to achieve the effect of reducing height and improving aerodynamic efficiency

Active Publication Date: 2017-03-22
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Description
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  • Application Information

AI Technical Summary

Problems solved by technology

This idea is ingenious, but it is very difficult to realize. The installation of the worm device adds a lot of complexity to the system structure. At the same time, there are circumferential unevenness and sealing problems, and the current research on memory alloys still does not meet the requirements. level, therefore, the engineering application of this concept is extremely difficult

Method used

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  • Turboshaft engine intake device and operation method
  • Turboshaft engine intake device and operation method
  • Turboshaft engine intake device and operation method

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Embodiment Construction

[0021] see figure 1 As shown, the invention discloses a turboshaft engine air intake device, which includes a center body assembly, a wedge assembly and a casing assembly. The casing assembly is the shell of the integral air intake device, including an outer cylinder 13 surrounding the central body assembly and a double-button lip section 12 located at the front of the outer cylinder 13 . The central body assembly includes a front fairing 1, an annular air chamber 3, a central body front section 4 extending forward from the annular air chamber, a central body rear section 5 extending backward from the annular air chamber, connecting and fixing the outer cylinder 13 and The front support section 2 of the front section 4 of the central body is connected and fixed to the outer cylinder 13 and the rear support section 6 and the pressure monitor 7 of the rear section 5 of the central body. Among them, the annular air chamber 3 adopts an integral structure, with a metal structure a...

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Abstract

The invention discloses a turboshaft engine intake device and an operation method thereof. The turboshaft engine intake device comprises a central body component, a wedge component and a casing component, and is characterized in that a flexible deformable annular air chamber is embedded into the central body component, meanwhile, a wedge capable of moving in the axial direction is designed, and the profiles of the air chamber and the axial position of the wedge can be adjusted according to the working environment and the working state of an engine. When a helicopter works in unclean air environments such as the environment with dust sand, the intake system is enabled to work in a mode with high dust sand separation efficiency through increasing the height of the air chamber and moving the wedge forwards; and when the helicopter is in a cruising state, the intake system is enabled to work in a mode with high aerodynamic efficiency by reducing the height of the air chamber and moving the wedge backwards. The invention effectively solves the problem that a traditional fixed-geometry intake system cannot give consideration to both low-altitude efficient sand draining and high cruising aerodynamic performance.

Description

technical field [0001] The invention relates to the field of aeroengine design, in particular to the air intake system of a turboshaft engine. Background technique [0002] my country is one of the countries with the largest desert area in the world. The desert is an arc-shaped belt stretching across the northwest, north and northeast lands. This arc-shaped desert belt is 600km wide from north to south and 4000km long from east to west. In the desert area, the desert covers an area of ​​1.49 million square kilometers, accounting for 15.5% of the country's land area. Due to the convenient take-off and landing of the helicopter, the requirements for the airport environment are relatively low, and it can hover in the air. It is especially suitable for military and civilian rescue, supply, and fire fighting in the above-mentioned environment. Shaft engine) working efficiency and service life have all brought great harm. The inhaled dust and sand hit the high-speed rotating engi...

Claims

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Application Information

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IPC IPC(8): F02C7/04F02C7/05
CPCF02C7/04F02C7/05
Inventor 谭慧俊凌棫陈昊孙姝黄河峡张悦
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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