Heterogeneous multilayer heat prevention-heat insulation composite material prefabricating body structure and molding process thereof

A composite material and forming process technology, applied in the directions of lamination, layered products, lamination devices, etc., can solve the problem of poor thermal performance stability, affecting the reliability of the thermal protection system of hypersonic aircraft, and the weight of the thermal protection system being too large, etc. question

Active Publication Date: 2019-01-25
CHINA ACADEMY OF MACHINERY SCIENCE & TECHNOLOGY +1
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

However, whether it is a sandwich structure or a multi-level structure, due to the limitation of the preparation process and its own structure, the weight of the thermal protection system is too large and the stability of the thermal protection performance is poor, which in turn affects the reliability of the thermal protection system of the hypersonic vehicle.

Method used

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  • Heterogeneous multilayer heat prevention-heat insulation composite material prefabricating body structure and molding process thereof
  • Heterogeneous multilayer heat prevention-heat insulation composite material prefabricating body structure and molding process thereof
  • Heterogeneous multilayer heat prevention-heat insulation composite material prefabricating body structure and molding process thereof

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Embodiment Construction

[0033] Prepare the positioning plate 5 and the guide rod 4, the diameter of the guide rod is 1.2mm, punch a hole on the positioning plate 5, the hole diameter is 1.2mm, fix the guide rod 4 on the positioning plate 5, as figure 2 shown.

[0034] image 3 It is a top view of the guide rod 4 distribution, the center distance of the guide sleeves in the y direction is 2 mm, the center distance of the first, second, fourth and fifth rows of guide sleeves in the x direction is 2 mm, and the center distance of the third row of guide sleeves in the x direction is 4 mm.

[0035] The heat-proof structure layer 1 is made of 3K SiC fiber with an area density of 1.79g / cm 3 , the center distance of the guide sleeve in the x and y directions is 2mm, and the fibers follow the guide sleeve according to Figure 4 The method of middle 6 is used for cross-winding, and then laid along the horizontal direction of the guide sleeve to prepare a heat-resistant structural layer 1 with a thickness of...

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Abstract

The invention discloses a heterogeneous multilayer heat prevention-heat insulation composite material prefabricating body structure and a molding process thereof, wherein the structure comprises a heat prevention structure layer, a heat insulation transition layer and a bearing structure layer. According to the molding process, a guiding rod is pre-arranged, different combinations of different kinds of fibers are used, the sequences in fiber winding processes are controlled, the center distance of a guiding sleeve is changed, and the guiding sleeve is replaced with fibers, such that the multi-material multilayer prefabricating body with density gradient is prepared; fibers with excellent heat prevention performance are wound and spread along the guiding sleeve to prepare the heat prevention structure layer; fibers with excellent heat insulation performance are wound along the guiding sleeve to prepare the heat insulation transition layer; continuous fibers are wound and spread along the guiding sleeve to prepare the bearing structure layer; and density gradient structure is achieved by controlling the center distance of the guiding sleeve and the fiber spreading and winding combination mode. According to the present invention, the composite material prepared from the prefabricating body structure and the matrix through impregnating can achieve the heat prevention / heat insulation / bearing integrated function.

Description

technical field [0001] The invention relates to a heat-proof / heat-insulation / load-bearing composite material prefabricated body structure and forming process, in particular to a heterogeneous multi-layer heat-insulating composite material prefabricated body structure and forming process, which are used for composite material heat-proof / heat-insulating / Carrying integrated thermal protection field. Background technique [0002] With the characteristics of hypersonic cruise, fast response, and high strategic value, hypersonic aircraft has become an important strategic equipment for major countries to compete for development. During hypersonic flight and hypersonic reentry of hypersonic aircraft in adjacent space, the surface temperature of the aircraft is very high, and the fuselage cabin is subjected to ultra-high dynamic loads. The thermal protection system is located outside the fuselage of the hypersonic vehicle to protect the temperature of the fuselage and internal str...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B32B5/08B32B5/26B32B5/14B32B37/02B32B37/14B32B37/10B32B7/03B32B15/02B32B15/14B32B9/00B32B9/04B32B27/02B32B27/12B32B27/34B64C1/40
CPCB32B5/08B32B5/14B32B5/26B32B15/02B32B15/14B32B37/02B32B37/10B32B37/14B32B2262/0269B32B2262/10B32B2262/106B32B2262/14B32B2307/304B32B2605/18B64C1/40
Inventor 单忠德孙正刘丰张群胡培利
Owner CHINA ACADEMY OF MACHINERY SCIENCE & TECHNOLOGY
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