초록 ▼

An aircraft in the form of multi-stage missile 1 with a spiral inducing assembly 2 which is capable of inducing the missile to travel in a continuous spiraling motion without the missile rolling. A ramjet 6b is attached to a tube 3 that is able to rotate around the encircled part of the fuselage. Th

An aircraft in the form of multi-stage missile 1 with a spiral inducing assembly 2 which is capable of inducing the missile to travel in a continuous spiraling motion without the missile rolling. A ramjet 6b is attached to a tube 3 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 3 with respect to the rotate-able tube 3, thereby changing their pitch relative to the longitudinal axis of the rotate-able tube 3. Ramjet 6b is rotated to a greater than another ramjet on the right side of the tube 3. The difference in degree of rotation between the ramjets makes the ramjet 6b exert a greater force on the rotate-able tube 3 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 3 to rotate. When rotated, the ramjets would exert a lateral force on the rotate-able tube 3. Thus, as well as forcing the rotate-able tube 3 to rotate, the ramjets would also 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 missile when in flight.

대표청구항 ▼

The claims defining this invention are as follows: 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 produc

The claims defining this invention are as follows: 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 and such that the at least one means for producing thrust is able to be rotated in a pivoting manner to a greater degree than the at least one additional means for producing thrust, relative to the tube. 2. 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 and which at least one means for producing thrust, by producing thrust, is able to exert a force on the tube that is greater than a force that the at least one additional means for producing thrust is able to exert on the tube by producing thrust. 3. 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. 4. The aircraft of claim 2 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. 5. 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. 6. 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. 7. The aircraft of claim 3 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. 8. The aircraft of claim 4 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. 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 a force could be exerted on the tube by the at least one means for producing thrust, and which force is such that the tube could be forced to rotate in one direction relative to the encircled part of the aircraft, 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 another force could be exerted on the tube by the at least one additional means for producing thrust, which another force is such that 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, and which force exerted on the tube by the at least one means for producing thrust is greater than the another force exerted on the tube by the at least one additional means for producing thrust. 18. The aircraft of claim 17 wherein the said aircraft is a missile.