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Isolation coupler for structural assembly and method for attenuating load

A technology for structural components and isolators, which is used in aerospace aircraft, aerospace aircraft vibration reduction, shock absorbers, etc., and can solve problems such as functional equipment failure, damage to functional equipment, space and weight restrictions, etc.

Active Publication Date: 2020-06-16
THE BOEING CO
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Mechanical vibration and / or mechanical shock may damage or cause a functional device to malfunction if sufficient shock loads are transmitted to the functional device
Additionally, in the aerospace industry, vehicle space and weight constraints and the need for a high degree of design flexibility with respect to strength and load attenuation requirements can limit the use of existing shock attenuation methods

Method used

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  • Isolation coupler for structural assembly and method for attenuating load
  • Isolation coupler for structural assembly and method for attenuating load
  • Isolation coupler for structural assembly and method for attenuating load

Examples

Experimental program
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Embodiment approach

[0101] Clause 1. An isolating coupling (100) for coupling a functional element (204) to a support structure (202), the isolating coupling (100) comprising:

[0102] a first bracket (102) comprising a plurality of first bracket sides (106), wherein the plurality of first bracket sides (106) form a closed polygonal shape in plan view;

[0103] a plurality of isolators (110) coupled to each of the first bracket sides (106); and

[0104] A second bracket (104) comprising a plurality of second bracket sides (108) coupled to the isolator (110), wherein the number of second bracket sides (108) is equal to the number of first bracket sides (106) and form a closed polygonal shape in plan view; and

[0105] Wherein, the isolator (110) separates each of the first bracket sides (106) from a corresponding one of the second bracket sides (108) to attenuate transmission from the first bracket (102) to the second bracket. The load of the frame (104).

[0106] Clause 2. The isolation couple...

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PUM

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Abstract

An isolation coupler for coupling a functional element to a support structure includes a first bracket. The first bracket includes a plurality of first bracket sides. The plurality of first bracket sides form a closed polygonal shape in plan view. The isolation coupler also includes a plurality of isolators coupled to each of the first bracket sides. The isolation coupler also includes a second bracket. The second bracket includes a plurality of second bracket sides. The second bracket side is coupled to the isolator. The number of the second bracket sides is equal to the number of the first bracket sides, and the second bracket sides form a closed polygonal shape in plan view. An isolator separates each of the first bracket sides from a corresponding one of the second bracket sides to attenuate a load transmitted from the first bracket to the second bracket.

Description

technical field [0001] The present disclosure relates generally to structural assemblies, and more particularly to an isolating coupler for a structural assembly that couples a functional element to a support structure. Background technique [0002] In various industries, it may be desirable or even necessary to attenuate shock and / or vibration transmitted from a supporting structure to a piece of functional equipment. Shock loads are typically high magnitude, short duration forces. Shock loads can have vibrational frequencies ranging from a few Hertz to several kilohertz or more, can be instantaneous or continuous in nature, and can have axial and / or transverse components. For example, in the aerospace industry, there is a need to prevent the substantial mechanical vibrations and / or mechanical shocks generated during the operation of aerospace vehicles (e.g., aircraft, spacecraft, satellites, rockets, etc.) functional equipment. Mechanical vibration and / or mechanical sho...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F16M11/04F16F15/08
CPCF16M11/04F16F15/08B64C1/00B64G1/413B64G1/40F16F1/38F16F2226/045B64G1/64B64G1/1021B64G1/36B64G1/228F16M13/02B64D47/00F16F2224/025F16F2234/02F16F1/3732F16F7/00
Inventor 理查德·W·阿斯顿迈克尔·约翰·朗马克安娜·M·汤姆钦斯卡马修·赫尔曼艾米丽·C·伍兹
Owner THE BOEING CO