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Double Wall Big Elbow

A double-wall and large-bend technology, which is applied in combustion methods, lighting and heating equipment, and continuous combustion chambers, can solve problems such as cracks in parts, affecting engine life and safety, and poor design of the two-layer wall connection structure to achieve cooling Excellent effect and good maintenance effect

Active Publication Date: 2022-07-01
AECC HUNAN AVIATION POWERPLANT RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0010] The invention provides a double-wall large elbow to solve the problem that the existing double-wall large elbow is often caused by poor design of the connection structure of the two-layer wall, so that the internal stress of the part cannot be released, resulting in local cracks, and then Technical issues affecting engine life and safety

Method used

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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 as defined and covered below.

[0037] refer to figure 2 , the preferred embodiment of the present invention provides a double-walled large elbow, which is applied to the return combustion chamber of an aero-engine. The inlet ends of the inner wall assembly 10 and the outer wall assembly 20 are connected to form a supporting structure 30 for supporting against the diffuser 40 in the axial direction, and then passing through the diffuser 40 to the inlet end of the double-walled large elbow It is axially limited, and at the same time, the inlet end of the double-walled large elbow has free thermal expansion in the radial direction. The supporting structure 30 is also used to support the flame tube outlet 50, so that the flame tube outlet 50 is sealedly connected with the double-walled ...

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Abstract

The invention discloses a double-walled large elbow. The double-walled large elbow comprises an inner wall component and an outer wall component which are arranged inside and outside in sequence. The inlet ends of the inner wall assembly and the outer wall assembly are connected to form a supporting structure, which is used to support the diffuser in the axial direction, and then the inlet end of the double-walled large elbow is axially limited by the diffuser. , and at the same time make the inlet end of the double-walled large elbow have free thermal expansion along the radial direction. The supporting structure is also used to support the outlet of the flame tube, so that the outlet of the flame tube is sealed and connected with the double-walled large elbow, and at the same time, the outlet of the flame tube has free thermal expansion along the axial direction. The outlet ends of the outer wall assembly and the inner wall assembly are connected to form an open overlapping structure, so that the inner wall assembly has free thermal expansion in the axial and radial directions, and the extension portion of the outlet end of the outer wall assembly forms a fixed structure. The fixing structure is also used to support the guide so that the guide has free thermal expansion in the axial direction.

Description

technical field [0001] The invention relates to the technical field of aero-engine return combustion chambers, in particular, to a double-walled large elbow. Background technique [0002] Small and medium gas turbine engines rotate at very high speeds. In order to avoid rotor dynamics problems, the compressor and turbine must be compactly arranged to shorten the wheelbase. In order to organize efficient combustion in a limited space, annular return combustion chambers are used in small and medium gas turbine engines. is widely used. Compared with the direct-flow combustion chamber, there are more exhaust elbows at the outlet of the flame tube of the reflux combustion chamber. The inner and outer profiles of the exhaust elbows are respectively large elbows and small elbows. Therefore, it can be said that the large elbow is the return flow. Unique structure on the combustion chamber. The high-temperature and high-pressure gas flows from the outlet of the flame tube into the ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F23R3/42
CPCF23R3/42
Inventor 王启道康尧江立军陈江陈彬
Owner AECC HUNAN AVIATION POWERPLANT RES INST
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