US2003051434A1PendingUtilityA1

Composite structure and method for constructing same

Assignee: LOCKHEED CORPPriority: Sep 20, 2001Filed: Sep 20, 2001Published: Mar 20, 2003
Est. expirySep 20, 2021(expired)· nominal 20-yr term from priority
B29C 70/24B29D 99/0014B29C 70/222B29C 70/30
41
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Claims

Abstract

According to one embodiment of the invention, a method of constructing a composite structure includes positioning a plurality of forming elements on a skin panel formed from a composite material in a predetermined configuration, disposing a stiffening panel formed from an uncured composite material outwardly from the forming elements to create a plurality of contact regions between the skin panel and the stiffening panel, and curing the skin panel and the stiffening panel to bond the skin panel and the stiffening panel together at the contact regions.

Claims

exact text as granted — not AI-modified
What is claimed is:  
     
         1 . A method of constructing a composite structure, comprising: 
 positioning a plurality of forming elements on a skin panel formed from a composite material in a predetermined configuration;    disposing a stiffening panel formed from an uncured composite material outwardly from the forming elements to create a plurality of contact regions between the skin panel and the stiffening panel; and    curing the skin panel and the stiffening panel to bond the skin panel and the stiffening panel together at the contact regions.    
     
     
         2 . The method of  claim 1 , further comprising removing the forming elements after curing the skin panel and the stiffening panel.  
     
     
         3 . The method of  claim 1 , further comprising coupling the skin panel and the stiffening panel with a plurality of fasteners.  
     
     
         4 . The method of  claim 3 , wherein coupling the skin panel and the stiffening panel with the fasteners comprises coupling the skin panel and the stiffening panel with a plurality of Z-pins proximate the contact regions.  
     
     
         5 . The method of  claim 1 , wherein the skin panel is formed from a composite material selected from the group consisting of a cured composite material and an uncured composite material.  
     
     
         6 . The method of  claim 1 , wherein disposing the stiffening panel comprises spraying a composite material outwardly from the forming elements.  
     
     
         7 . The method of  claim 1 , wherein disposing the stiffening panel formed from the uncured composite material comprises disposing a stiffening panel formed from an uncured composite material having a plurality of discontinuous fibers.  
     
     
         8 . The method of  claim 1 , wherein positioning the forming elements on the skin panel in the predetermined configuration comprises positioning the forming elements in a corrugated configuration.  
     
     
         9 . The method of  claim 1 , wherein positioning the forming elements on the skin panel in the predetermined configuration comprises positioning the forming elements in a waffle configuration.  
     
     
         10 . A method of constructing a composite structure, comprising: 
 positioning a plurality of forming elements on a skin panel formed from a composite material in a corrugated configuration;    disposing a stiffening panel formed from an uncured composite material having a plurality of discontinuous fibers outwardly from the skin panel and the forming elements;    partial-curing the skin panel and the stiffening panel to create a plurality of first contact regions between the skin panel and the stiffening panel and to create a plurality of second contact regions between the forming elements and the stiffening panel;    coupling the skin panel and the stiffening panel with a plurality of fasteners proximate the first contact regions; and    final curing the skin panel and the stiffening panel to bond the skin panel and the stiffening panel together at the first contact regions.    
     
     
         11 . The method of  claim 10 , further comprising removing the forming elements after final curing the skin panel and the stiffening panel.  
     
     
         12 . The method of  claim 11 , wherein coupling the skin panel and the stiffening panel with the fasteners comprises coupling the skin panel and the stiffening panel with a plurality of Z-pins proximate the first contact regions.  
     
     
         13 . The method of  claim 10 , wherein the skin panel is formed from a composite material selected from the group consisting of a partially-cured composite material and an uncured composite material.  
     
     
         14 . The method of  claim 10 , wherein disposing the stiffening panel comprises spraying a composite material outwardly from the forming elements.  
     
     
         15 . A method of constructing a composite structure, comprising: 
 positioning a plurality of forming elements on a first surface of a skin panel formed from a composite material selected from the group consisting of a cured composite material and an uncured composite material, the forming elements and the first surface of the skin panel creating a predetermined configuration;    forming a stiffening panel from an uncured composite material having a plurality of discontinuous fibers on a tool having a configuration substantially the same as the predetermined configuration;    heating the stiffening panel to a state sufficient enough to enable handling of the stiffening panel while maintaining its configuration;    disposing the stiffening panel outwardly from the skin panel and the forming elements to create a plurality of first contact regions between the skin panel and the stiffening panel and to create a plurality of second contact regions between the forming elements and the stiffening panel; and    curing the skin panel and the stiffening panel to bond the skin panel and the stiffening panel together at the first contact regions.    
     
     
         16 . The method of  claim 15 , further comprising removing the forming elements after curing the skin panel and the stiffening panel.  
     
     
         17 . The method of  claim 15 , wherein coupling the skin panel and the stiffening panel with the fasteners comprises coupling the skin panel and the stiffening panel with a plurality of Z-pins proximate the contact regions.  
     
     
         18 . The method of  claim 15 , wherein the predetermined configuration is a corrugated configuration.  
     
     
         19 . The method of  claim 15 , wherein the predetermined configuration is a waffle configuration.  
     
     
         20 . A composite structure, comprising: 
 a skin panel formed from a composite material;    a plurality of forming elements positioned on the skin panel in a corrugated configuration;    a stiffening panel formed from an uncured composite material having a plurality of discontinuous fibers disposed outwardly from the skin panel and the forming elements;    a plurality of contact regions created by the skin panel and the stiffening panel;    a plurality of fasteners coupling the skin panel and the stiffening panel proximate the contact regions; and    a plurality of bonding regions proximate the contact regions, the bonding regions created by curing the skin panel and the stiffening panel.    
     
     
         21 . The composite structure of  claim 20 , wherein the fasteners are Z-pins.  
     
     
         22 . The composite structure of  claim 20 , wherein the skin panel is formed from a composite material selected from the group consisting of a cured composite material and an uncured composite material.  
     
     
         23 . The composite structure of  claim 20 , wherein the stiffening panel is sprayed on the forming elements and the skin panel.

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