US2023415920A1PendingUtilityA1

Systems and methods for joining a first structure and a second structure with a choreographed adhesive de-aeration process

Assignee: BOEING COPriority: Dec 17, 2020Filed: Sep 8, 2023Published: Dec 28, 2023
Est. expiryDec 17, 2040(~14.4 yrs left)· nominal 20-yr term from priority
B64F 5/10B29C 65/544B29C 65/4835B29L 2031/3085B29C 66/721B29L 2031/3082B29C 66/1122B29C 66/81455B29C 66/342B29C 66/00145B29C 65/18B29C 65/5057B29C 65/5021B29C 65/7841B29C 66/532B29C 66/61B29C 66/12441B29C 66/12461B29C 65/7826B29C 65/10B29C 65/36
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Claims

Abstract

An example method of joining a first structure and a second structure is described that includes placing an adhesive within a bond cavity for bonding a first structure to a second structure, securing a vacuum bag to the first structure and the second structure so as to surround a portion of the first structure and the second structure, evacuating the bond cavity via a vacuum port to deaerate the adhesive within the bond cavity, after deaerating the adhesive, moving the first structure and the second structure relative to one another such that deaerated adhesive is disposed between the first structure and the second structure, and curing, via one or more heaters, the deaerated adhesive disposed between the first structure and the second structure to bond the first structure to the second structure.

Claims

exact text as granted — not AI-modified
What is claimed is: 
     
         1 . A system for joining a first structure and a second structure, the system comprising:
 one or more fixtures forming a bond cavity between a first structure and a second structure via positioning of the first structure relative to the second structure and to cause movement of the first structure and the second structure relative to one another;   a vacuum bag to secure the first structure and the second structure by surrounding a portion of the first structure and the second structure;   a vacuum port coupled to the vacuum bag for evacuating the bond cavity to deaerate an adhesive within the bond cavity such that deaerated adhesive is disposed between the first structure and the second structure; and   one or more heaters for curing the deaerated adhesive disposed between the first structure and the second structure to bond the first structure to the second structure.   
     
     
         2 . The system of  claim 1 , further comprising:
 a collapsible standoff positioned between the first structure and the second structure to control a position of the first structure relative to the second structure, wherein the collapsible standoff collapses at a predetermined temperature.   
     
     
         3 . The system of  claim 1 , further comprising:
 a collapsible standoff positioned in the adhesive within the bond cavity.   
     
     
         4 . The system of  claim 1 , wherein the adhesive is placed within the bond cavity on each bonding surface of the first structure and the second structure for bonding the first structure to the second structure. 
     
     
         5 . The system of  claim 1 , further comprising:
 a spacer inserted into a bottom area of the bond cavity to control bondline thickness.   
     
     
         6 . The system of  claim 1 , further comprising:
 a collapsible standoff inserted into a bottom area of the bond cavity to control a distance of distribution of the adhesive into the bond cavity based on temperature, wherein the collapsible standoff collapses at a predetermined temperature.   
     
     
         7 . The system of  claim 6 , wherein a thickness of a bondline between the first structure and the second structure is controlled via a residual thickness of a collapsed collapsible standoff. 
     
     
         8 . The system of  claim 1 , further comprising:
 a semi-permeable breather material placed at one or more exits of the bond cavity.   
     
     
         9 . The system of  claim 1 , wherein the vacuum port continuously evacuates the bond cavity while the one or more fixtures cause movement of the first structure and the second structure to one another. 
     
     
         10 . The system of  claim 1 , further comprising:
 a collapsible standoff placed in a hole of a surface of the second structure, wherein the surface of the second structure is configured to move toward the first structure,   wherein the adhesive is placed in the hole of the surface of the second structure, and   wherein the one or more fixtures cause movement of the first structure and the second structure relative to one another to force the first structure against the collapsible standoff to contact the collapsible standoff and force the adhesive to flow between the first structure and the second structure.   
     
     
         11 . The system of  claim 10 , wherein the one or more heaters cure the deaerated adhesive and cause the collapsible standoff to collapse due to heating and thermal softening at a predetermined temperature. 
     
     
         12 . The system of  claim 11 , wherein the vacuum port continuously evacuates the bond cavity while the one or more heaters cure the deaerated adhesive. 
     
     
         13 . The system of  claim 1 , further comprising:
 a collapsible standoff placed between the first structure and the second structure to control a position of the first structure relative to the second structure, wherein the collapsible standoff collapses at a predetermined temperature due to thermal softening;   the one or more heaters apply heat to achieve a first temperature to cause the collapsible standoff to collapse resulting in the first structure and the second structure moving toward each other due to vacuum pressure.   
     
     
         14 . The system of  claim 13 , wherein the one or more heaters apply heat to achieve a second temperature higher than the first temperature to cure the deaerated adhesive and bond the first structure to the second structure. 
     
     
         15 . The system of  claim 1 , wherein the first structure comprises a component of a wing of an aircraft and the second structure comprises a wing skin of the wing of the aircraft. 
     
     
         16 . A system for joining a first structure and a second structure, the system comprising:
 one or more fixtures forming a bond cavity between a first structure and a second structure via positioning of the first structure relative to the second structure and to cause movement of the first structure and the second structure relative to one another;   a collapsible standoff positioned between the first structure and the second structure to control a position of the first structure relative to the second structure;   a vacuum bag to secure the first structure and the second structure by surrounding a portion of the first structure and the second structure;   a vacuum port coupled to the vacuum bag for evacuating the bond cavity to deaerate an adhesive within the bond cavity such that deaerated adhesive is disposed between the first structure and the second structure; and   one or more heaters for curing the deaerated adhesive disposed between the first structure and the second structure to bond the first structure to the second structure.   
     
     
         17 . The system of  claim 16 , wherein the collapsible standoff comprises include a thermoplastic material. 
     
     
         18 . The system of  claim 16 , wherein the collapsible standoff comprises a spiral or spring-like configuration. 
     
     
         19 . The system of  claim 16 , wherein the collapsible standoff comprises a hollow column configuration. 
     
     
         20 . The system of  claim 16 , wherein the collapsible standoff collapses in a one-dimensional manner while providing alignment and spacing between the first structure and the second structure.

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