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An integrated rocket fairing with bearing and noise reduction and its design method

A design method and technology of fairings, which are applied in aerospace safety/emergency devices, thermal protection devices of aerospace vehicles, etc., can solve problems such as encroaching on the space of fairings, environmental excess of acoustic covering layers, threats to fairing satellites, etc., and achieve enhanced Sound insulation ability, improvement of environmental comfort, and effect of reducing internal noise

Active Publication Date: 2021-10-08
广州中科宇航探索技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, laying an acoustic covering layer (porous sound-absorbing material) inside the fairing is a relatively conventional means to reduce the internal noise environment of the fairing. However, laying the acoustic covering inside the fairing will encroach on the inner space of the fairing, especially Yes, acoustic cladding is more difficult to install when low frequency noise reduction measures such as Helmholtz resonators are required inside the fairing
In addition, during the flight of the rocket, it will be subjected to a harsh vibration environment. If it is not handled properly, the acoustic covering layer will easily produce environmental residues, threatening the satellites inside the fairing.

Method used

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  • An integrated rocket fairing with bearing and noise reduction and its design method
  • An integrated rocket fairing with bearing and noise reduction and its design method
  • An integrated rocket fairing with bearing and noise reduction and its design method

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Embodiment 1

[0039] like figure 1 As shown, the present application provides a load-carrying and noise-reducing integrated rocket fairing, including: a fairing main body 1 and a resonator 2 arranged on the inner surface of the fairing main body 1; the fairing main body 1 includes a cylindrical section and an arc section, The cylinder section and the arc section are connected together, and the inside of the fairing main body 1 is hollow, and the fairing main body 1 includes two layers of panels 3 and a honeycomb sandwich core 4 arranged between the two layers of panels 3; the honeycomb sandwich core 4 has a core , the core is connected by a plurality of honeycomb cells, and the plurality of honeycomb cells are evenly arranged, and the honeycomb cells are filled with porous sound-absorbing materials 5, effectively utilizing the internal space of the honeycomb sandwich core 4, and enhancing the sound insulation of the honeycomb sandwich core 4 performance. The porous sound-absorbing material...

Embodiment 2

[0050] like Figure 4 As shown, the present application provides a design method for carrying a noise reduction integrated rocket fairing, which design method includes the following steps:

[0051] Step S1, designing the main body of the fairing to obtain four basic variables of the main body of the fairing.

[0052] like Figure 5 As shown, the method of designing the fairing main body includes the following steps:

[0053] Step S110, establishing a hypothesis for the fairing main body.

[0054]Assumptions are established for the main body of the fairing: the panel is a single-layer thin plate; the honeycomb sandwich core does not bear normal stress; the coupling effect between antisymmetric and symmetric deformation is ignored;

[0055] Step S120, on the basis of the above assumptions, establish four basic variables of the fairing body design.

[0056] Specifically, the four basic variables are: first, the panel thickness t f ; Second, the honeycomb sandwich height t c...

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Abstract

The present application provides a load-carrying and noise-reducing integrated rocket fairing and its design method, comprising: a fairing main body and a resonator arranged on the inner surface of the fairing main body; the fairing main body includes two layers of panels and is arranged on two A honeycomb sandwich core between the panels; the honeycomb sandwich core has a core, the core is formed by connecting a plurality of honeycomb cells, the plurality of honeycomb cells are evenly arranged, and the honeycomb cells are filled with porous sound-absorbing material. The fairing of the present application can not only realize the mechanical bearing capacity, but also greatly improve the sound insulation, and provide a comfortable acoustic environment for the payload inside the rocket.

Description

technical field [0001] The present application relates to the technical field of noise mitigation of launch vehicle fairings, in particular to a load-carrying noise-reduction integrated rocket fairing and a design method thereof. Background technique [0002] For the launch vehicle fairing, noise is an important source of excitation for its internal vibration environment. As a protective cover for the rocket to transport loads, the fairing mainly plays the role of sound insulation, heat insulation, and pollution prevention. Generally speaking, when designing the fairing , mainly focus on the performance of the fairing itself, such as mechanical bearing, heat protection, and rain resistance. The sound insulation capability of the fairing itself mainly depends on the rigidity of the structure. After the structure is determined, the sound insulation of the fairing is determined immediately. Domestic launch vehicles often There are also no additional active and passive noise red...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/52B64G1/58
CPCB64G1/52B64G1/58
Inventor 王英诚布向伟史晓宁赖谋荣岳之光杨毅强
Owner 广州中科宇航探索技术有限公司
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