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Round pipe sandwich heat-preventing component

A technology of structural parts and round tubes, which is applied in the field of aerospace engineering, can solve problems such as difficult industrial use, difficult to withstand temperature, limited physical properties, etc., to solve poor impact resistance, reduce maintenance costs, and support the system. Effect

Inactive Publication Date: 2011-04-20
BEIHANG UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

There is also a lot of research in China, but it is concentrated between 400°C and 600°C, and most of the metal heat-resistant materials are made of aluminum alloy, which is limited by its own physical properties and it is difficult to withstand higher temperatures. Thermal materials or honeycomb sandwich panels are difficult to put into industrial use due to the limitation of technological level
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  • Round pipe sandwich heat-preventing component
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  • Round pipe sandwich heat-preventing component

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Embodiment Construction

[0017] Such as figure 1 As shown, the present invention consists of an upper high-temperature nickel-based deformed alloy honeycomb panel 1, a lower layer of nickel-based alloy honeycomb panel 2, and a round tube group 3 sandwiched between the high-temperature nickel-based deformed alloy honeycomb panel 1 and the nickel-based alloy honeycomb panel 2 constitute. High-temperature nickel-based deformed alloy 1 refers to a high-temperature nickel-based deformed alloy of 850°C or higher. The round tube group 3 is a stainless steel round tube group, which can be a Φ8mm 1Cr18NI9 stainless steel tube, and the round tubes in the round tube group 3 are welded together by argon arc welding. The two ends of the round tube group 3 are respectively connected to the process tube 11. One end 9 of the process tube 11 is sealed and welded, and the other end 8 is connected to 4 taps for feeding coolant. Water cooling can be used to simulate the coolant. The diameter of the circular tube group ...

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Abstract

The invention relates to a round pipe sandwich heat preventing component which comprises an upper high temperature nickel base wrought alloy honeycomb panel, a lower nickel base alloy honeycomb plate and a round pipe set arranged between the high temperature nickel base wrought alloy honeycomb panel and the nickel base alloy honeycomb plate, wherein round pipes in the round pipe set are welded together; the high temperature nickel-base wrought alloy honeycomb panel and the nickel base alloy honeycomb plate are provided with multiple layers of reflecting screens; the upper high temperature nickel base wrought alloy honeycomb panel and the lower nickel base alloy honeycomb plate are connected with the round pipe set through point contact, namely, in a mode of line connection; one end of theround pipe set is sealed, while the other end is connected with a four-way joint; and high-temperature nickel base wrought alloy can bear temperature higher than or equal to 850 DEG C. The invention has the advantages of high-efficiency heat insulation and shock resistance.

Description

technical field [0001] The invention relates to a heat-resistant structural part of a high-speed aircraft body, in particular to a heat-resistant structural part using a circular tube sandwich, and belongs to the technical field of aerospace engineering. Background technique [0002] When a high-speed aircraft flies in the atmosphere at high speed, due to the aerodynamic heating effect at high Mach numbers, the surface structure of the aircraft needs to bear mechanical loads and also bear relatively strong thermal loads. For the large-area fuselage of the aircraft, heat-resistant structures such as metal and insulation are generally used to form a heat-resistant system to achieve heat insulation and protect the performance of the internal normal-temperature structure from being affected. The traditional heat-proof structure generally consists of a multi-layer structure composed of high-temperature metal metal honeycomb panels, non-ash fiber insulation layers, etc. In recent...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B32B3/20B32B15/01B64C1/40B32B3/12
Inventor 梁伟杨嘉陵吴大方
Owner BEIHANG UNIV