[미국특허]
Method of making precision geometry advanced composite honeycomb material for spacecraft applications and honeycomb material made thereby
원문보기
IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0769171
(2001-01-23)
|
발명자
/ 주소 |
- Lewis, Richard A.
- Yocky, Richard C.
- Rivera, Michael
|
출원인 / 주소 |
- Northrop Grumman Corporation
|
인용정보 |
피인용 횟수 :
2 인용 특허 :
4 |
초록
▼
A method of making precision geometry honeycomb material formed of a composite material and exhibiting dimensional uniformity, is disclosed. Composite material is molded in the cavity of a single-sided female mold to form a first web with a plurality of honeycomb cell portions of the desired cell sh
A method of making precision geometry honeycomb material formed of a composite material and exhibiting dimensional uniformity, is disclosed. Composite material is molded in the cavity of a single-sided female mold to form a first web with a plurality of honeycomb cell portions of the desired cell shape in the web. The details of the cavity mold configuration are captured to form the honeycomb cell portions in the composite material during molding the web by applying pressure to the composite material in the mold with an elastomeric pressure intensifier. The composite material of the web is stabilized as by curing. First and second molded webs are precisely aligned in a fixture and joined together at facing cell nodes thereof by bonding yielding a honeycomb material with superior geometric platform.
대표청구항
▼
A method of making precision geometry honeycomb material formed of a composite material and exhibiting dimensional uniformity, is disclosed. Composite material is molded in the cavity of a single-sided female mold to form a first web with a plurality of honeycomb cell portions of the desired cell sh
A method of making precision geometry honeycomb material formed of a composite material and exhibiting dimensional uniformity, is disclosed. Composite material is molded in the cavity of a single-sided female mold to form a first web with a plurality of honeycomb cell portions of the desired cell shape in the web. The details of the cavity mold configuration are captured to form the honeycomb cell portions in the composite material during molding the web by applying pressure to the composite material in the mold with an elastomeric pressure intensifier. The composite material of the web is stabilized as by curing. First and second molded webs are precisely aligned in a fixture and joined together at facing cell nodes thereof by bonding yielding a honeycomb material with superior geometric platform. directing a fabric along a predetermined path of travel while directing one longitudinal edge portion of the fabric into and through a folding guide and folding the longitudinal edge portion upon itself into overlying fabric layers to define a longitudinal hem along the longitudinal edge of the fabric; applying molten curable hot melt adhesive at a temperature of about 200° F. to about 250° F. between the overlying fabric layers along a simulated sewing path, said curable hot melt adhesive having an initial softening point prior to curing and an irreversibly increased softening point relative to said initial softening point after curing; applying pressure to said longitudinal hem to cause molten adhesive to penetrate into the fibrous structure of the fabric layers and to adhere the fabric layers to one another; and subjecting the adhesive to conditions sufficient for curing the adhesive. 15. The process of claim 14, further comprising reheating the curable hot melt adhesive and realigning the overlying fabric layers prior to said subjecting step. 16. The process of claim 14, wherein said adhesive applying step comprises extruding the adhesive. 17. The process of claim 16, wherein said adhesive applying step comprises extruding a continuous bead of adhesive along the simulated sewing path. 18. The process of claim 14, wherein the curable hot melt adhesive is a moisture curable hot melt adhesive. 19. The process of claim 18, wherein the curable hot melt adhesive is a moisture curable polyurethane hot melt adhesive. 20. The process of claim 18, wherein said subjecting step comprises exposing the adhesive to atmospheric moisture. 21. The process of claim 18, wherein said subjecting step comprises increasing the atmospheric moisture in a region proximate the curable adhesive. 22. The process of claim 21, wherein said atmospheric moisture increasing step comprises introducing steam or mist to a region proximate the curable hot melt adhesive. 23. A process for forming a selvage, comprising: applying molten curable hot melt adhesive at a temperature of about 200° F. to about 250° F. to an edge portion of a surface of a textile substrate along a simulated sewing path, said curable hot melt adhesive having an initial softening point prior to curing and an irreversibly increased softening point relative to said initial softening point after curing; and subjecting the adhesive to conditions sufficient for curing the adhesive. 24. The process of claim 23, further comprising applying pressure to the substrate to cause adhesive to penetrate into the fibrous structure of the textile substrate after said adhesive applying step. 25. The process of claim 23, wherein the curable hot melt adhesive is a moisture curable hot melt adhesive. 26. The process of claim 25, wherein the curable hot melt adhesive is a moisture curable polyurethane hot melt adhesive. 27. The process of claim 25, wherein said subjecting step comprises exposing the adhesive to atmospheric moisture. 28. The process of claim 25, wherein said subjecting step comprises increasing the atmospheric moisture in a region proximate the curable hot melt adhesive. 29. The process of claim 28, wherein said atmospheric moisture increasing step comprises introducing steam or mist to a region proximate the curable hot melt adhesive. 30. A process for making textile articles, comprising: directing first and second textile substrates into opposing face-to-face relationship; applying molten curable hot melt adhesive at a temperature of about 200° F. to about 250° F. between the overlying substrates along a simulated sewing path so that adhesive is disposed between the substrates, said curable hot melt adhesive having an initial softening point prior to curing and an irreversibly increased softening point relative to said initial softening point after curing; applying pressure to the textile substrates to cause adhesive to penetrate into the fibrous structure of the textil e substrate; and subjecting the adhesive to conditions sufficient for curing the adhesive. 31. A process for making textile articles, comprising: applying molten curable hot melt adhesive at a temperature of about 200° F. to about 250° F. along a simulated sowing path on a surface of a textile substrate, said curable hot melt adhesive having an initial softening point prior to curing and an irreversibly increased softening point relative to said initial softening point after curing; contacting the molten adhesive with an opposing textile substrate surface so that adhesive is disposed between textile substrate surfaces; applying pressure to the textile article to cause adhesive to penetrate into the fibrous structure of the textile substrate; and subjecting the adhesive to conditions sufficient for curing the adhesive. 32. A process for making textile articles, comprising: applying molten curable hot melt adhesive at a temperature of about 200° F. to about 250° F. along a simulated sewing path on a surface of a textile substrate, said curable hot melt adhesive having an initial softening point prior to curing and an irreversibly increased softening point relative to said initial softening point after curing; thermally quenching the molten curable hot melt adhesive to its initial non-tacky, solid phase; configuring the textile substrate prior to substantial cure of said adhesive so that the non-tacky adhesive is disposed between opposed surfaces of the textile substrate; heating said curable hot melt adhesive mid applying pressure to the textile substrate surface to cause adhesive to penetrate into the fibrous structure of the opposed surfaces of the substrate; and subjecting the adhesive to conditions sufficient for curing the adhesive. 33. The process of claim 32, wherein said configuring step comprises positioning the substrate to form a textile article comprising multiple points of juxtaposed contacting surfaces with non-tacky adhesive disposed therebetween. 34. A process for providing decorative patterns to textile articles, comprising: applying a pattern of molten curable hot melt adhesive at a temperature of about 200° F. to about 250° F., said curable hot melt adhesive having an initial softening point prior to curing and an irreversibly increased softening point relative to said initial softening point after curing on a surface of a textile substrate along a simulated sewing path; and subjecting the adhesive to conditions sufficient for curing the adhesive. 35. The process of claim 34, further comprising contacting at least a portion of the curable hot melt adhesive with another substrate prior to applying the adhesive. 36. The process of claim 35, wherein said another substrate is selected from the group consisting of ribbons, beads, and braiding. 37. A process for providing a decorative edge affect to textile articles, comprising: applying a shaped deposit of curable hot melt adhesive at a temperature of about 200° F. to about 250° F. to an edge of a textile substrate, said curable hot melt adhesive having an initial softening point prior to curing and an irreversibly increased softening point relative to said initial softening point after curing; and subjecting the adhesive to conditions sufficient for curing the adhesive.
-
Rhodes Marvin D. (Yorktown VA) Mikulas ; Jr. Martin M. (Williamsburg VA), Composite sandwich lattice structure.
-
Marshall Andrew C. ; Fellman Michael L., Composite structure.
-
Lusignea Richard W. (Brighton MA) Stanco Joseph J. (Clinton NY) Kashalikar Uday (Natick MA), Film-based composite structures for ultralightweight SDI systems.
-
Harshberger ; Jr. Robert L. ; Olsen Keith A. ; Potter John E. ; McLaughlin Martin J. ; Grossman Stephen P., Isostatic pressure resin transfer molding.
-
Akishev,Niaz Irekovich; Zakirov,Ildus Muhametgaleevich; Nikitin,Alexandr Vladimirovich, Foldable mandrel for production of a single curvature folded core for a sandwich panel.
-
Gil Gonzalez, Leopoldo, Honeycomb frame.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.