Pneumatic type/mechanical type combined adjustment mach number 0-7 stage combined engine air inlet

A Mach number and mechanical technology, applied in the direction of machines/engines, mechanical equipment, jet propulsion devices, etc., can solve problems such as large effective use of space, low reliability, increased intake weight, etc., to improve flow coefficient and work The effect of simple performance and actuation mode and small space occupation

Active Publication Date: 2017-12-08
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Pneumatic adjustment methods (1) and (2) need to bleed air from the downstream compression surface and the downstream inner channel respectively to adjust the position of the upstream precursor shock wave and ensure the sealing of the precursor shock wave, so it is necessary to add a narrow and long bleed air pipe Road, throttle valve and sealing device, which not only increases the weight of the intake duct, takes up a large effective space, but also has an adverse effect on the starting performance and back pressure resistance of the intake duct; while the method (3) Although the same-level compression surface bleed air is used to avoid the defects of the first two adjustment methods, it can only be adjusted for a specific Mach number and cannot be infinitely adjusted. working performance under
In addition, the above-mentioned single pneumatic adjustment method can only adjust and reconstruct the precursor wave system of the inlet, so it can only adjust the flow coefficient, total pressure recovery, and flow field uniformity of the inlet, and cannot improve Self-starting ability and compression performance of the intake port
[0004] For this reason, it is necessary to develop a new combined engine inlet adjustment scheme, which can not only solve the problem of low reliability of a single mechanical adjustment under high Mach number conditions, but also avoid the above-mentioned problems of traditional pneumatic adjustment. defects, so as to ensure that the combined engine inlet can work effectively in a wide range of Mach numbers and obtain better aerodynamic performance

Method used

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  • Pneumatic type/mechanical type combined adjustment mach number 0-7 stage combined engine air inlet
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  • Pneumatic type/mechanical type combined adjustment mach number 0-7 stage combined engine air inlet

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Embodiment Construction

[0020] see figure 1 , figure 2 and image 3, the invention discloses a pneumatic / mechanical combined adjustment Mach number 0-7 combined engine intake port, including a high-speed passage 1 extending from front to rear, located inside the high-speed passage and extending from front to rear side by side with the high-speed passage The low-speed channel 2, the precursor compression surface 7, the side walls 6 located on both sides of the high-speed channel, the low-speed channel and the precursor compression surface, the base 11 located below the precursor compression surface and extending backward, located between the high-speed channel and the low-speed channel The high-speed / low-speed passage divider 5 between the high-speed passage and the rotating lip cover 4 that is hinged at the front end of the divider divider and extends forward; The engine 27 is connected, the inner wall of the low-speed channel 2 is a mechanical variable geometry component, and the outlet of the lo...

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Abstract

The invention discloses a pneumatic type/mechanical type combined adjustment mach number 0-7 stage combined engine air inlet. The pneumatic type/mechanical type combined adjustment mach number 0-7 stage combined engine air inlet is mainly composed of a high-speed channel, a low-speed channel, a mechanical type variable geometry assembly and a pneumatic type shock wave adjusting assembly. Under the low-speed mode, the mechanical type variable geometry assembly is adopted for adjusting the throat area and the internal shrinkage ratio of the air inlet, and the low mach number starting performance and the high mach number compression performance of the air inlet are guaranteed; and under the high-speed mode, the pneumatic type shock wave adjusting assembly is used for adjusting the precursor shock wave position, the precursor shock wave sealing state is kept, and the discharge coefficient and the working performance of the air inlet are obviously improved within the wide mach number scope. According to the pneumatic type/mechanical type combined adjustment scheme, the compression amount and the precursor shock wave position of the air inlet can be continuously adjusted, it is guaranteed that the combined engine air inlet can effectively work within the wide mach number scope, and the good pneumatic performance is obtained.

Description

technical field [0001] The invention relates to the field of aircraft design, in particular to a combined engine inlet. Background technique [0002] The air-breathing combined engine has many advantages such as wide operating range, high reliability, reusability, horizontal take-off and landing, and high specific impulse, making it an ideal power plant for hypersonic vehicles. As an important part of the air-breathing combined engine propulsion system, the intake duct not only efficiently provides air with a certain pressure, temperature and flow rate to the engine in a wide range of Mach numbers, but also shoulders the responsibility of working mode conversion, outlet flow field, etc. Functions such as uniformity adjustment and isolation of upstream and downstream disturbances. For this reason, the wide Mach number range performance of this type of inlet is one of the key technologies for the development of air-breathing combined engines. [0003] The air-breathing combi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C7/042
CPCF02C7/042
Inventor 孙姝盛发家谭慧俊陈昊黄河峡张悦
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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