[특허]Aircraft spiraling mechanism with jet assistance--B

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특허 상세정보

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내보내기 페이스북 공유 트위터 공유 카카오톡 공유

Aircraft spiraling mechanism with jet assistance--B

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F41G-007/00
미국특허분류(USC)	244/003.22; 244/003.1; 244/062; 244/055
출원번호	UP-0601804 (2006-11-20)
등록번호	US-7635104 (2010-01-08)
발명자 / 주소	Kusic, Tom
인용정보	피인용 횟수 : 1 인용 특허 : 21

초록
▼

An aircraft 1 with a spiral inducing assembly 2 which is capable of inducing the aircraft to travel in a continuous spiraling motion without the aircraft rolling. A ramjet 6b is attached to a tube 3a that is able to rotate around the encircled part of the fuselage. The ramjet 6b is able to rotate in a pivoting manner on the rotate-able tube 3a with respect to the rotate-able tube 3a, thereby changing their pitch relative to the longitudinal axis of the rotate-able tube 3a. Ramjet 6b is rotated as is another ramjet on the right side of the tube 3a. The rotate-able tube 3a is rotated by means of an electric motor 3b rotating a wheel 3c. The difference in degree of rotation between the ramjets makes the ramjet 6b exert a greater force on the rotate-able tube 3a than the ramjet on the right side when the ramjets are rotated in the same direction. The imbalance between the rotational forces thus causes the rotate-able tube 3a to rotate. When rotated, the ramjets would exert a lateral force on the rotate-able tube 3a. Thus, the ramjets would push the rotate-able tube sideways. But as the rotate-able tube is pushed sideways, it rotates, and hence the lateral direction of push constantly revolves, causing a spiraling motion of the aircraft when in flight.

대표
청구항
▼

The invention claimed is: 1. An aircraft comprising a tube, which tube encircles part of the aircraft and is able to rotate relative to the encircled part of the aircraft, and which tube comprises a plurality of means for producing thrust, with at least one means for producing thrust connected to the tube such that the at least one means for producing thrust is able to be rotated in a pivoting manner relative to the tube, and with at least one additional means for producing thrust connected to the tube such that the at least one additional means for producing thrust is able to be rotated in a pivoting manner relative to the tube, and which said aircraft comprises a means to rotate the at least one means for producing thrust in a pivoting manner relative to the tube and a means to rotate the at least one additional means for producing thrust in a pivoting manner relative to the tube such that the at least one means for producing thrust can be rotated in a pivoting manner relative to the tube in a same direction as a direction of rotation in a pivoting manner of the at least one additional means for producing thrust relative to the tube. 2. The aircraft of claim 1 wherein the means to rotate the at least one means for producing thrust and the means to rotate the at least one additional means for producing thrust are such that rotation of the at least one means for producing thrust in a pivoting manner relative to the tube can cause rotation of the at least one additional means for producing thrust in a pivoting manner relative to the tube in a same direction as a direction of rotation in a pivoting manner of the at least one means for producing thrust relative to the tube. 3. An aircraft comprising a tube, which tube encircles part of the aircraft and is able to rotate relative to the encircled part of the aircraft, and which tube comprises at least one means for producing thrust, which at least one means for producing thrust is connected to the tube such is that the at least one means for producing thrust is able to be rotated in a pivoting manner relative to the tube, and which aircraft comprises a plurality of sections which can be separated and a means to rotate the at least one means for producing thrust such that separation of the sections is able to cause rotation of the at least one means for producing thrust in a pivoting manner relative to the tube. 4. The aircraft of claim 1 wherein the said same direction is such that rotation of the at least one means for producing thrust in a pivoting manner relative to the tube is substantially in the same direction as a direction of rotation of the at least one additional means for producing thrust in a pivoting manner relative to the tube. 5. The aircraft of claim 2 wherein the said same direction is such that rotation of the at least one means for producing thrust in a pivoting manner relative to the tube is substantially in the same direction as a direction of rotation of the at least one additional means for producing thrust in a pivoting manner relative to the tube. 6. The aircraft of claim 3 wherein the tube comprises at least one additional means for producing thrust and which at least one additional means for producing thrust is connected to the tube such that the at least one additional means for producing thrust is able to be rotated in a pivoting manner relative to the tube, and which aircraft comprises a means to rotate the at least one additional means for producing thrust such that separation of the said sections is able to cause rotation of the at least one additional means for producing thrust in a pivoting manner relative to the tube. 7. The aircraft of claim 6 wherein the means to rotate the at least one means for producing thrust and the means to rotate the at least one additional means for producing thrust are such that separation of the said sections is able to cause rotation of the at least one means for producing thrust in a pivoting manner relative to the tube and rotation of the at least one additional means for producing thrust in a pivoting manner relative to the tube, and such that the at least one means for producing thrust can be caused to rotate in a pivoting manner in a same direction as a direction of rotation in a pivoting manner of the at least one additional means for producing thrust relative to the tube. 8. The aircraft of claim 7 wherein the said same direction is such that rotation of the at least one means for producing thrust is substantially in a same direction relative to the tube as a direction rotation of the at least one additional means for producing thrust. 9. The aircraft of claim 1 wherein the said aircraft is a missile. 10. The aircraft of claim 2 wherein the said aircraft is a missile. 11. The aircraft of claim 3 wherein the said aircraft is a missile. 12. The aircraft of claim 4 wherein the said aircraft is a missile. 13. The aircraft of claim 5 wherein the said aircraft is a missile. 14. The aircraft of claim 6 wherein the said aircraft is a missile. 15. The aircraft of claim 7 wherein the said aircraft is a missile. 16. The aircraft of claim 8 wherein the said aircraft is a missile. 17. An aircraft comprising a tube, which tube encircles part of the aircraft and is able to rotate relative to the encircled part of the aircraft, and which tube comprises at least one means for producing thrust, which said at least one means for producing thrust is able to produce thrust in a direction such that the tube could be forced to rotate in one direction relative to the encircled part of the aircraft as a result of thrust produced by the at least one means for producing thrust, and the tube comprises at least one additional means for producing thrust, which at least one additional means for producing thrust is able to produce thrust in a direction such that as a result of the thrust produced by the at least one additional means for producing thrust the tube could be forced to rotate in a direction that is opposite to the said one direction if no other force acted on the tube. 18. The aircraft of claim 17 wherein the said aircraft is a missile.

이 특허에 인용된 특허 (21)

이 특허를 인용한 특허 피인용횟수: 1

Rosenlund, Gunnar. Propulsion system with movably mounted engines. USP2015069067687.

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Aircraft spiraling mechanism with jet assistance--B

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이 특허에 인용된 특허 (21)

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Aircraft spiraling mechanism with jet assistance--B

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이 특허에 인용된 특허 (21)

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