Double shear joint for bonding in structural applications
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B32B-037/00
B32B-038/04
출원번호
US-0728720
(2010-03-22)
등록번호
US-8088242
(2012-01-03)
발명자
/ 주소
Frisch, Douglas A.
Piehl, Marc J.
Grose, Douglas L.
Sweetin, Joseph L.
Chapman, Michael R.
출원인 / 주소
The Boeing Company
대리인 / 주소
Caven & Aghevli LLC
인용정보
피인용 횟수 :
1인용 특허 :
19
초록▼
A bonded composite joint may include a base having a foot configured to couple to a member. The base may include a flange extending outward from the foot. The joint further may include a panel having a core positioned between opposing skins, where the skins have inner walls proximate the core and th
A bonded composite joint may include a base having a foot configured to couple to a member. The base may include a flange extending outward from the foot. The joint further may include a panel having a core positioned between opposing skins, where the skins have inner walls proximate the core and the skins extend outward beyond the core on at least one end of the panel to define a recess between the skins. The recess between the skins may receive the flange. A bonding agent may be used to couple the flange to the inner walls of the panel.
대표청구항▼
1. A method for joining a structure to a base, comprising: removing a segment of a core configured between skins to create a recess on the structure;positioning the recess of the structure proximate the base, the base including a flange projecting away from the base, the flange configured to insert
1. A method for joining a structure to a base, comprising: removing a segment of a core configured between skins to create a recess on the structure;positioning the recess of the structure proximate the base, the base including a flange projecting away from the base, the flange configured to insert into the recess;applying a bonding agent to a gap by inserting a bonding application apparatus into an aperture located on at least one of the skins, the aperture configured to provide access to the gap that is defined by a volume between the flange and the skins; andcuring the bonding agent to couple the structure and the base. 2. The method of claim 1, wherein removing the segment of the core includes detaching the segment that is removably secured to the core with a semi-permanent adhesive tape. 3. The method of claim 1, wherein removing the segment of the core includes machining the segment to remove the segment from the core. 4. The method of claim 1, further comprising creating the structure by making a shear cut from a stock-sized structure to customize the size of the structure. 5. The method of claim 1, further comprising applying sections of tape between the structure and the base, the sections of tape covering at least a portion of the gap. 6. The method of claim 5, wherein applying the bonding agent to the gap includes inserting a bonding application apparatus between the sections of the tape. 7. The method of claim 1, further comprising applying a sealant to the gap after the application of the bonding agent, the sealant protecting the bonding agent from degradation. 8. A method, comprising: aligning a sandwich panel over a base structure, the sandwich panel having a core disposed between skins, the skins to extend beyond the core on a side of the sandwich panel to create a recess that is complementary to flange projecting from the base structure such that the flange is inserted into the recess during the aligning; andbonding the sandwich panel to the base structure by directing bonding agent into apertures in the skins that provide access to the recess after the sandwich panel is aligned over the flange of the base, the bonding to create a joint. 9. The method of claim 8, further comprising removing a portion of the core of the sandwich panel to form the recess. 10. The method of claim 8, further comprising inserting a spacer adjacent and parallel to the flange to increase a width of the flange, the width to be less than a distance between the skins that defines the recess. 11. The method of claim 8, further comprising inserting a fastener through the skins and the flange of the base to secure the sandwich panel to the base. 12. The method of claim 8, further comprising bonding a reinforcing structure to at least one of the skins proximate the recess to increase a lateral strength of the at least one of the skins. 13. The method of claim 8, further comprising applying a sealant over a bonding agent used to bond the sandwich panel to the base structure, the sealant protecting the bonding agent from degradation. 14. A method of assembling a structural joint, comprising creating a recess in a sandwich panel by removing a segment of a core portion configured between skins of the sandwich panel;positioning the recess of the sandwich panel proximate a base, the base including a flange projecting away from the base, the flange configured to insert into the recess;applying a spacer to a side of the flange to increase a width of the flange, the width of the flange to be less than a distance between the skins that defines the recess; andapplying a bonding agent to a gap defined by a volume between the skins minus a displacement of the flange and the spacer. 15. The method of claim 14, wherein creating the recess includes detaching a segment of the core portion. 16. The method of claim 14, wherein creating the recess includes machining the segment of the core portion to remove the segment. 17. The method of claim 14, wherein the spacer is attached to the flange prior to the positioning. 18. The method of claim 14, further comprising applying a sealant over the bonding agent to prevent degradation of the bonding agent.
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이 특허에 인용된 특허 (19)
Schmidt, Hans-Juergen, Aircraft fuselage shell component with crack propagation resistance.
Grose,Douglas L.; Wanthal,Steven P.; Sweetin,Joseph L.; Mathiesen,Christopher B.; Southmayd,Randy A., Methods of joining structures and joints formed thereby.
Thrash, Patrick J.; Burgess, Roger Alan; Markus, Alan M., Resin infusion mold tool system and vacuum assisted resin transfer molding with subsequent pressure bleed.
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