Folding configuration for air vehicle
IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0475371
(2012-05-18)
|
등록번호 |
US-8899515
(2014-12-02)
|
발명자
/ 주소 |
- Guptaa, Suneal
- Bley, Jeremy
|
출원인 / 주소 |
- Textron Systems Corporation
|
대리인 / 주소 |
|
인용정보 |
피인용 횟수 :
1 인용 특허 :
7 |
초록
▼
An air vehicle, as well as a method for folding an air vehicle for storage, may include a fuselage and a wing connected to the fuselage. The wing may include two ends positioned opposite from each other, and the wing may be substantially perpendicular to the fuselage. At least one of the ends may de
An air vehicle, as well as a method for folding an air vehicle for storage, may include a fuselage and a wing connected to the fuselage. The wing may include two ends positioned opposite from each other, and the wing may be substantially perpendicular to the fuselage. At least one of the ends may define a space therebetween the fuselage and the wing. The space may be sized to receive a potion of the wing when the wing is wrapped around the fuselage.
대표청구항
▼
1. An air vehicle, comprising: a fuselage having a top portion;a wing connected to the fuselage at the top portion, the wing having a top surface, a bottom surface, and two ends positioned opposite each other, wherein the wing is substantially perpendicular to the fuselage; andat least the bottom su
1. An air vehicle, comprising: a fuselage having a top portion;a wing connected to the fuselage at the top portion, the wing having a top surface, a bottom surface, and two ends positioned opposite each other, wherein the wing is substantially perpendicular to the fuselage; andat least the bottom surface of the wing and the top portion of the fuselage defining a space therebetween, wherein the space is sized to receive a portion of the wing when the wing is wrapped around the fuselage. 2. The air vehicle of claim 1, wherein the portion of the wing is adapted to pass entirely through or partially through the space. 3. The air vehicle of claim 1, wherein the wing comprises a first portion having a first end of the two ends, a second portion having a second end of the two ends, and a center portion. 4. The air vehicle of claim 3, wherein the space is defined between the fuselage and the center portion of the wing. 5. The air vehicle of claim 4, wherein the first portion of the wing is adapted to wrap around the fuselage, and the first end is adapted to pass through the space in a wrapped position of the first portion, and the second portion of the wing is adapted to wrap around the first portion in the wrapped position. 6. The air vehicle of claim 1, wherein the space is sized to allow the end of the wing to pass between the fuselage and wing for storage, and to allow the end of the wing to rapidly release for use. 7. The air vehicle of claim 1, wherein the space is sized to allow the wing to pass between the fuselage and wing multiple times for storage. 8. An air vehicle, comprising: a fuselage having a top portion;a wing connected to the fuselage at the top portion, the wing having a top surface, a bottom surface, and two ends positioned opposite each other, wherein the wing extends out from the fuselage on both sides of the fuselage; andat least the bottom surface of the wing and the top portion of the fuselage defining a space that is sized and positioned to receive a portion of the wing when the wing is wrapped around the fuselage. 9. The apparatus of claim 8, wherein the wing comprises a first portion having a first end of the two ends, a second portion having a second end of the two ends, and a center portion. 10. The apparatus of claim 9, wherein the space is defined between the top portion the fuselage and the center portion of the wing.
이 특허에 인용된 특허 (7)
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Reany, Jack W.; Sanderson, Terry M., Aircraft wing with flexible skins.
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Ifju,Peter; Lee,Kyu Ho; Albertani,Roberto; Mitryk,Shawn J.; Boria,Frank J.; Abdulrahim,Mujahid, Bendable wing for micro air vehicle.
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Hellman, Ulf, Guided artillery missile with extremely long range.
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Fuller Brian L. (1167 Danner St. ; SE. Atlanta GA 30316), Rollable airfoil.
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Klestadt Ralph H. (Sherman Oaks CA), Rotationally mounted flexible band wing.
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Lapidot, Ehud, Unmanned aircraft having a pivotably movable double wing unit.
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Greenhalgch Samuel (Doylestown PA), Wing-extendible gliding store.
이 특허를 인용한 특허 (1)
-
Cesaroni, Anthony Joseph, Surface skimming munition.
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