IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0130813
(2001-10-26)
|
국제출원번호 |
PCT/US01/49795
(2001-10-26)
|
국제공개번호 |
WO02/07759
(2002-10-03)
|
발명자
/ 주소 |
- Heisler, Richard R.
- Ratliff, Cliford L.
|
출원인 / 주소 |
- The Johns Hopkins University
|
대리인 / 주소 |
|
인용정보 |
피인용 횟수 :
9 인용 특허 :
9 |
초록
▼
A wind tunnel model design employs a reinforcing strongback 10, made of a rigid material, for receiving a balance 12. At least one jacket section 14, made of a rapid prototype (RP) material, fits over the strongback 10 and defines at least part of an aerodynamic surface. Other aerodynamic surfaces,
A wind tunnel model design employs a reinforcing strongback 10, made of a rigid material, for receiving a balance 12. At least one jacket section 14, made of a rapid prototype (RP) material, fits over the strongback 10 and defines at least part of an aerodynamic surface. Other aerodynamic surfaces, made of either RP materials or conventional metal materials, may be attached directly to the strongback 10.
대표청구항
▼
1. A wind tunnel model comprising:a strongback, comprising a rigid material and having an exterior axial surface, said strongback designed to be supported by a balance; andat least one jacket section, made of a rapid prototype (RP) material, having an interior axial surface and an exterior surface,
1. A wind tunnel model comprising:a strongback, comprising a rigid material and having an exterior axial surface, said strongback designed to be supported by a balance; andat least one jacket section, made of a rapid prototype (RP) material, having an interior axial surface and an exterior surface, said interior axial surface of said jacket section defining an interior volume, said strongback being at least partially inside said interior volume of said jacket section such that said exterior axial surface of said strongback engages said interior axial surface of said jacket section, said exterior surface of said jacket section defining at least part of an aerodynamic surface. 2. The wind tunnel model of claim 1, further comprising a balance, said balance rigidly connected to said strongback and said strongback rigidly connected to said jacket section, whereby, when said balance is supported by a wind tunnel facility sting, all aerodynamic forces and moments acting on said jacket section are transferred first to said strongback and then to said balance. 3. The wind tunnel model of claim 1 wherein said strongback is made of a material selected from the group consisting of steel, aluminum, metal alloys and wood. 4. The wind tunnel model of claim 1 wherein said jacket section is made of an RP material selected from the group consisting of photopolymers, thermoplastics, cast ceramic powders, and sintered powdered metals. 5. The wind tunnel model of claim 1 wherein said jacket section is made of ABS plastic infused with resin. 6. The wind tunnel model of claim 1 further comprising:a secondary aerodynamic component connected to said jacket section. 7. The wind tunnel model of claim 1 further comprising:a secondary aerodynamic component connected directly to said strongback. 8. The wind tunnel model of claim 6 or claim 7 wherein said secondary aerodynamic component is a wing, fin, canard, nose, engine or inlet. 9. The wind tunnel model of claim 6 or claim 7 wherein said secondary aerodynamic component is made of a material selected from the group consisting of steel, aluminum, titanium, metal alloys, wood, photopolymers, thermoplastics, cast ceramic powders, sintered powdered metals, and combinations thereof. 10. The wind tunnel model of claim 7 wherein said jacket section defines a slot between said external and internal surfaces of said jacket section for receiving said secondary aerodynamic component. 11. The wind tunnel model of claim 1, further comprising a plurality of said jacket sections. 12. The wind tunnel model of claim 11, wherein said jacket sections have interlocking tabs for connecting said jacket sections together. 13. The wind tunnel model of claim 1 wherein said strongback is reusable. 14. The wind tunnel model of claim 1, wherein said strongback has an interior axial surface defining an interior volume for receiving a balance. 15. A wind tunnel model comprising:strongback means for providing a rigid, longitudinal support;jacket section means, made of a rapid prototype (RP) material, for defining an aerodynamic surface, said jacket section means fitting at least partially over said strongback means. 16. The wind tunnel model of claim 15 wherein said jacket section means and strongback means are rigidly connected to a balance, whereby, when said balance is supported by a wind tunnel facility sting, all aerodynamic forces and moments acting on said jacket section means are transferred first to said strongback means and then to said balance. 17. The wind tunnel model of claim 15 wherein said strongback means is made of a material selected from the group consisting of steel, aluminum, metal alloys and wood. 18. The wind tunnel model of claim 15 wherein said jacket section means is made of an RP material selected from the group consisting of photopolymers, thermoplastics, cast ceramic powders, and sintered powdered metals. 19. The wind tunnel model of claim 15 wherein said jacket section means is made of ABS plastic infus ed with resin. 20. The wind tunnel model of claim 15 further comprising:a secondary aerodynamic component connected to said jacket section means. 21. The wind tunnel model of claim 15 further comprising:a secondary aerodynamic component connected directly to said strongback means. 22. The wind tunnel model of claim 20 or claim 21 wherein said secondary aerodynamic component is a wing, fin, canard, nose, engine or inlet. 23. The wind tunnel model of claim 20 or claim 21 wherein said secondary aerodynamic component is made of a material selected from the group consisting of steel, aluminum, titanium, metal alloys, wood, photopolymers, thermoplastics, cast ceramic powders, sintered powdered metals, and combinations thereof. 24. The wind tunnel model of claim 21 wherein said jacket section means defines a slot for receiving said secondary aerodynamic component. 25. The wind tunnel model of claim 15 further comprising a plurality of said jacket section means. 26. The wind tunnel model of claim 25, wherein said jacket section means have interlocking tabs for connecting said jacket section means together. 27. The wind tunnel model of claim 15 wherein said strongback is reusable.
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