|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/034.R; 244/039; 244/003.1; 244/003.24|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 5 인용 특허 : 19|
An aircraft 1 with a spiral inducing assembly 2 which is capable of inducing the aircraft to travel in a continuous spiralling motion without the aircraft rolling. Two fins 6 and 17 are attached to a tube 3 that is able to rotate around the encircled part of the fuselage. The fins 6, 17 are able to rotate in a pivoting manner on the rotatable tube 3 with respect to the rotatable tube 3, thereby changing their pitch relative to the longitudinal axis of the rotatable tube 3. Fin 6 is larger than fin 17. The difference in sizes between the fins makes the ...
The claims defining this invention are as follows: 1. An aircraft comprising a spiral inducing assembly, which said spiral inducing assembly is capable of forcing the aircraft to travel in a spiralling motion during flight or the aircraft and which spiral inducing assembly comprises a tube, which tube encircles part of the aircraft and is able to rotate relative to the encircled part of the aircraft, with a plurality of fins connected to the tube, which fins are connected to the tube such that the fins can be rotated in a pivoting mariner relative to th...