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Compound interstitial

A technology of gap fillers and gap fillers, which can be used in material bonding, program control, instruments, etc., and can solve problems such as difficulty in matching gaps

Active Publication Date: 2021-11-23
THE BOEING CO
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the exact part geometry can vary, making it difficult to fit voids through the use of shims and fillers

Method used

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  • Compound interstitial
  • Compound interstitial
  • Compound interstitial

Examples

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Embodiment Construction

[0033] Reference throughout this specification to "one embodiment," "an embodiment," or similar language means that a particular feature, structure, or characteristic described in connection with the embodiment is included in at least one embodiment of the present disclosure. Appearances of "in one embodiment," "in an embodiment," and similar language throughout this specification may, but do not necessarily, all refer to the same embodiment. Similarly, use of the term "implementation" means an implementation having a particular feature, structure, or characteristic described in connection with one or more embodiments of the present disclosure, however, lacking an indication that the implementation may otherwise be related to One or more embodiments are associated.

[0034]The embodiments described below relate to the formation of a composite shim by placing a shim over the parts at a joint region where two parts may or are designed to be in contact. Composite shims can be ad...

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Abstract

This application relates to composite interstitials, and a method is disclosed herein. The method includes identifying a first orientation on a first part to place a first shim to form a first portion of a composite shim. The method also includes applying a first shim to a first orientation on the first part by using the end effector. The method also includes identifying a second location directly adjacent to the first location on the first part to place a second shim. The method also includes applying a second shim to the first part in a second orientation using the end effector to form a second portion of the composite shim. The method also includes applying a third shim to the second shim at the second orientation to increase the thickness of the second portion of the composite shim.

Description

technical field [0001] The present disclosure relates generally to component joining, and more particularly to joint shimming and filling. Background technique [0002] Today, many complex structures such as aircraft, spacecraft, automobiles, etc. are made by assembling individual parts. Those assembled materials include a considerable number of interconnected components. Interconnected parts of complex structures are joined together at joints. Fasteners and weldments are conventionally used to form complex structural joints. [0003] To enhance joint properties, voids between components are filled or caulked to reduce stresses and other forces experienced by fasteners, weldments, and components of a structure. However, the precise part geometry may vary, making it difficult to fit voids through the use of shims and fillers. Contents of the invention [0004] The subject matter of the present application has been developed in response to the state of the art, and speci...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F16B1/00F16B11/00
CPCF16B1/00F16B11/006F16B2200/99B23P19/04B23P2700/01B23P2700/12B64F5/10B25J9/1687G05B2219/40019G06F30/00G06F30/15Y02T50/40B29C65/48B29C66/01B29L2031/3055B29L2031/3076B29L2031/3097B62D65/02
Inventor A·内斯彼特T·沃尔森
Owner THE BOEING CO
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