Discretely tailored multi-zone bondline for fail-safe structural repair
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B32B-007/02
B32B-003/26
B32B-003/02
G11B-011/05
B29C-073/00
B32B-043/00
출원번호
US-0903489
(2010-10-13)
등록번호
US-8617694
(2013-12-31)
발명자
/ 주소
Dan-Jumbo, Eugene A.
Keller, Russell L
Westerman, Everett A.
출원인 / 주소
The Boeing Company
대리인 / 주소
Yee & Associates, P.C.
인용정보
피인용 횟수 :
5인용 특허 :
41
초록▼
A repair patch for reworking an inconsistent area of a composite structure includes a patch body adapted to cover the inconsistent area and having a first patch region, a second patch region outside the first patch region and a first separation zone between the first patch region and the second patc
A repair patch for reworking an inconsistent area of a composite structure includes a patch body adapted to cover the inconsistent area and having a first patch region, a second patch region outside the first patch region and a first separation zone between the first patch region and the second patch region, with the first patch region, the first separation zone and the second patch region having increasing interlaminar fracture toughness from a center to an edge of the patch body; and a layer of adhesive for bonding the patch body to the composite structure.
대표청구항▼
1. A repair patch for reworking an inconsistent area of a composite structure, comprising: a patch body adapted to cover the inconsistent area and having a first patch region, a second patch region outside the first patch region and a first separation zone between the first patch region and the seco
1. A repair patch for reworking an inconsistent area of a composite structure, comprising: a patch body adapted to cover the inconsistent area and having a first patch region, a second patch region outside the first patch region and a first separation zone between the first patch region and the second patch region, with the first patch region, the first separation zone and the second patch region having increasing interlaminar fracture toughness from a center to an edge of the patch body, the first separation zone and the second patch region being substantially concentric rings surrounding the first patch region, the first patch region being centrally located relative to the first separation zone and the second patch region; anda layer of adhesive for bonding the patch body to the composite structure. 2. The repair patch of claim 1 wherein said patch body includes a plurality of fiber reinforced composite laminate plies each having a fiber orientation and a first portion of the plurality of plies in said first patch region possesses characteristics that are different from a second portion of the plurality of plies in said second patch region. 3. The repair patch of claim 2 wherein said characteristics include at least one of a characteristic of the fibers, a thickness of the plurality of plies, the number of the plies in the plurality of plies, a presence of a gap between the plurality of plies, a fiber orientation of the plurality of plies, and a sequence of the fiber orientations of the plurality of plies in the patch region. 4. The repair patch of claim 1 further comprising a third patch region outside the second patch region. 5. The repair patch of claim 4 further comprising a second separation zone between the second patch region and the third patch region. 6. The repair patch of claim 4 wherein the first separation zone has a first interlaminar fracture toughness value of at least about 2.0 in-#/in2. 7. The repair patch of claim 6 wherein the second separation zone has a second interlaminar fracture toughness value of at least about 2.5 in-#/in2. 8. The repair patch of claim 7 further comprising: a third separation zone circumscribing the third patch region, wherein the third separation zone has a third interlaminar fracture toughness value of at least about 3.0 in-#/in2. 9. The repair patch of claim 1 wherein the first patch region, the first separation zone and the second patch region all share at least one common radial axis relative to the concentric rings. 10. A repair patch for reworking an inconsistent area of a composite structure, comprising: a patch body adapted to cover the inconsistent area and having a first patch region, a first separation zone outside the first patch region, a second patch region outside the first separation zone, a second separation zone outside the second patch region, a third patch region outside the second separation zone and a third separation zone outside the third patch region, with the first patch region, the first separation zone, the second patch region, the second separation zone, the third patch region and the third separation zone having increasing interlaminar fracture toughness from a center to an edge of the patch body, and the first separation zone, the second patch region, the second separation zone, the third patch region, and the third separation zone all being substantially concentric rings surrounding the first patch region, the first patch region being centrally located relative to all of the first separation zone, the second patch region, the second separation zone, the third patch region, and the third separation zone; anda layer of adhesive for bonding the patch body to the composite structure. 11. The repair patch of claim 10 wherein the patch body includes a plurality of fiber reinforced composite laminate plies each having a fiber orientation and wherein a first portion of the plurality of plies in the first patch region, a second portion of the plurality of plies in the first separation zone, a third portion of the plurality of plies in the second patch region, a fourth portion of the plurality of plies in the second separation zone, a fifth portion of the plurality of plies in the third patch region, and a sixth portion of the plurality of plies in the third separation zone each possess characteristics that are different from each other. 12. The repair patch of claim 11 wherein said characteristics include at least one of a characteristic of the fibers, a thickness of the plurality of plies, a number of the plurality of plies, a presence of a gap between the plurality of plies, the fiber orientation of the plurality of plies, and a sequence of the fiber orientations of the plurality of plies in the patch region. 13. The repair patch of claim 10 wherein the first separation zone has a first interlaminar fracture toughness value of at least about 2.0 in-#/in2. 14. The repair patch of claim 13 wherein the second separation zone has a second interlaminar fracture toughness value of at least about 2.5 in-#/in2. 15. The repair patch of claim 14 wherein the third separation zone has a third interlaminar fracture toughness value of at least about 3.0 in-#/in2. 16. The repair patch of claim 15 wherein the first patch region has a fourth interlaminar fracture toughness of less than about 2.0 in-#/in2, the second patch region has a fifth interlaminar fracture toughness of about 2.0-2.5 in-#/in2, and the third patch region has a sixth interlaminar fracture toughness of about 2.5-3.0 in-#/in2. 17. The repair patch of claim 10 further comprising an overlay doubler on the patch body. 18. The repair patch of claim 10 wherein the first patch region, the first separation zone, the second patch region, the second separation zone, the third patch region, and the third separation zone all share at least one common radial axis relative to the concentric rings.
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