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특허 상세정보

Aircraft spiraling mechanism with jet assistance—D

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F41G-007/00   
미국특허분류(USC) 244/003.22; 244/003.21; 244/062; 244/055
출원번호 UP-0723216 (2007-03-19)
등록번호 US-7642491 (2010-02-11)
발명자 / 주소
인용정보 피인용 횟수 : 3  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 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 smaller than another ramjet on the right side of the tube 3. The differen...

대표
청구항

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 said tube comprises a means to cause rotation of the tube 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...

이 특허에 인용된 특허 (21)

  1. Kusic, Tom. Aircraft spiralling mechanism. USP2004036708923.
  2. Kusic,Tom. Aircraft spiralling mechanism--c. USP2006087093791.
  3. Wisshaupt Daniel (Orlans la source FRX). Device for roll attitude control of a fin-stabilized projectile. USP1991095048772.
  4. Gregory Malejko ; John C. Grau. Fin-stabilized projectile with improved aerodynamic performance. USP2002096443391.
  5. Peckham Derek H. (Farnham GBX). Guided missiles. USP1992085139215.
  6. Bains William R. (Lake Elsinore CA). Guided projectile flight control fin system. USP1986014565340.
  7. MacDonald ; Gilmour C.. Helical path munitions delivery. USP1978054086841.
  8. Niemeier Byron M. (Claremont CA). Mechanical roll rate stabilizer for a rolling missile. USP1977064029270.
  9. Kranz Walter (Taufkirchen DEX). Missile having rotor ring. USP1990104964593.
  10. Silich Bert A. (Oswego IL). N-dimensional fighter aircraft. USP1993015176338.
  11. Poisson-Quinton Philippe (Paris FRX) Bevert Amedee P. (Nice FRX) Le Thuy Hung (Le Plessis-Robinson FRX). Process and an installation for the control of the efficiency of the aerodynamic surfaces of an aircraft. USP1981084281810.
  12. Peller Helmut (Dsseldorf DEX) Schilling Hartmut (Kaarst DEX) Becker Hanjoerg (Dsseldorf DEX) Glotz Gerhard (Dsseldorf DEX). Projectile with rotatable stabilizing device. USP1990024903917.
  13. De Luca Nicholas J. (721 E. Cordova St. #1 Pasadena CA 91101). Recreational and sport rocket construction. USP1993125271579.
  14. Klestadt Ralph H. (Sherman Oaks CA). Rotationally mounted flexible band wing. USP1995055417393.
  15. Stoy David R. (Woodland Hills CA). Separately banking maneuvering aerodynamic control surfaces, system and method. USP1994065322243.
  16. Bar, Klaus; Bohl, Jurgen; Kautzsch, Karl. Spin-stabilized projectile with a braking device. USP2003016511016.
  17. Kusic, Tom. Spiralling missile--A. USP2003116644587.
  18. Kusic, Tom. Spiralling missile--B. USP2003116648433.
  19. Deakin Richard S. (Haslemere GBX). Stabilization systems. USP1993025186413.
  20. Walker Robert A. (17130 Roscoe Blvd. Los Angeles CA 91325). Two-axis rudder trim for aircraft. USP1983024373689.
  21. Ullrich Hans-Gunter,DEX. Vane control system for a guided missile. USP1999115975461.