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Thermal compensation device of special-shaped spray pipe heat shield

A technology of special-shaped nozzles and heat shields, which is applied in the direction of jet propulsion devices, machines/engines, etc., can solve the problems of not being deep enough, and achieve the effects of enhancing strength, ensuring profile size, and ensuring safe use

Active Publication Date: 2020-12-01
AECC SICHUAN GAS TURBINE RES INST
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  • Abstract
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  • Application Information

AI Technical Summary

Problems solved by technology

[0005] At present, the design of special-shaped nozzles is in its infancy, and the research on the effective thermal compensation connection structure of heat shields for special-shaped nozzles is not yet in-depth. There is an urgent need for a combined thermal compensation connection structure that can adapt to high temperature and high pressure working environments to meet the functional requirements of special-shaped nozzles.

Method used

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  • Thermal compensation device of special-shaped spray pipe heat shield
  • Thermal compensation device of special-shaped spray pipe heat shield
  • Thermal compensation device of special-shaped spray pipe heat shield

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Embodiment Construction

[0024] Embodiments of the present disclosure will be described in detail below in conjunction with the accompanying drawings.

[0025] Embodiments of the present disclosure are described below through specific examples, and those skilled in the art can easily understand other advantages and effects of the present disclosure from the contents disclosed in this specification. Apparently, the described embodiments are only some of the embodiments of the present disclosure, not all of them. The present disclosure can also be implemented or applied through different specific implementation modes, and various modifications or changes can be made to the details in this specification based on different viewpoints and applications without departing from the spirit of the present disclosure. It should be noted that, in the case of no conflict, the following embodiments and features in the embodiments can be combined with each other. Based on the embodiments in the present disclosure, a...

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Abstract

The invention provides a thermal compensation device of a special-shaped spray pipe heat shield, and relates to the technical field of aero-engine spray pipes. The thermal compensation device comprises the special-shaped heat shield, wherein a plurality of L-shaped supports are evenly fixed to the outer side of the special-shaped heat shield at intervals, lifting lugs are assembled on longitudinalsections of the L-shaped supports, and assembly gaps are reserved in the assembly positions between the lifting lugs and the longitudinal sections of the L-shaped supports, so that the lifting lugs are movably connected with the L-shaped supports; and assembling holes for assembling the lifting lugs on the longitudinal sections of the L-shaped supports are circular holes or kidney-shaped holes. By means of the L-shaped supports, the lifting lugs and an arch-shaped frame combined structure assembled on the outer surface of the special-shaped heat shield, radial heat deformation of the special-shaped heat shield after being heated is effectively converted into the axis direction and the circumferential direction, the molded surface sizes of inner and outer ducts are guaranteed, and the pneumatic and invisible performance of a spray pipe is guaranteed.

Description

technical field [0001] The disclosure relates to the technical field of aeroengine nozzles, in particular to a heat compensation device for a special-shaped nozzle heat shield. Background technique [0002] High stealth performance is the trend of future aircraft research and development. The design technology of the low-detectable and large-curvature special-shaped nozzle is a new stealth technology based on this. The low-detectable large-curvature special-shaped nozzle not only has good stealth performance, but also facilitates integration with the rear body. The advantage of design is a research hotspot in recent years. [0003] Compared with the traditional axisymmetric nozzle, the low-detectable large-curvature special-shaped nozzle has a non-axisymmetric cross-section and a curved centerline, which requires the ability to completely block the rearward visible high-temperature components. precedent. At the same time, when the engine air flow is applied to the non-axi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02K1/82
CPCF02K1/822
Inventor 郭建伟廖华琳谢龙罗红飞刘立立朱川母鸿瑞商盼盼
Owner AECC SICHUAN GAS TURBINE RES INST
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