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특허 상세정보

Separation activated missile spiraling mechanism—FA

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/01   
미국특허분류(USC) 244/003.24; 244/003.23
출원번호 UP-0654126 (2009-12-11)
등록번호 US-7800033 (2010-10-11)
발명자 / 주소
인용정보 피인용 횟수 : 0  인용 특허 : 23
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 fin 6a is attached to a tube 3 that is able to rotate around the encircled part of the fuselage. The fin 6a is able to rotate in a pivoting manner on the rotate-able tube 3 with respect to the rotate-able tube 3, thereby changing the pitch relative to the longitudinal axis of the rotate-able tube 3. Fin 6a is rotated to a greater than another fin on the right ...

대표
청구항

The invention claimed is: 1. A missile with a tube, which tube encircles part of the missile and is able to rotate relative to the encircled part of the missile, and at least one fin is connected to the tube, which at least one fin is connected to the tube such that the at least one fin is able to be rotated in a pivoting manner relative to the tube, and which missile comprises a plurality of sections and a means to rotate the at least one fin, which sections can be separated, and which means to rotate the at least one fin is such that separation of the...

이 특허에 인용된 특허 (23)

  1. Kusic, Tom. Aircraft spiralling mechanism. USP2004036708923.
  2. Kusic,Tom. Aircraft spiralling mechanism--c. USP2006087093791.
  3. Kusic,Tom. Aircraft spiralling mechanism-B. USP2007017165742.
  4. Kusic, Tom. Airplane spiralling mechanism. USP2004076764044.
  5. Wisshaupt Daniel (Orlans la source FRX). Device for roll attitude control of a fin-stabilized projectile. USP1991095048772.
  6. Gregory Malejko ; John C. Grau. Fin-stabilized projectile with improved aerodynamic performance. USP2002096443391.
  7. Peckham Derek H. (Farnham GBX). Guided missiles. USP1992085139215.
  8. Bains William R. (Lake Elsinore CA). Guided projectile flight control fin system. USP1986014565340.
  9. MacDonald ; Gilmour C.. Helical path munitions delivery. USP1978054086841.
  10. Niemeier Byron M. (Claremont CA). Mechanical roll rate stabilizer for a rolling missile. USP1977064029270.
  11. Kranz Walter (Taufkirchen DEX). Missile having rotor ring. USP1990104964593.
  12. Silich Bert A. (Oswego IL). N-dimensional fighter aircraft. USP1993015176338.
  13. 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.
  14. Peller Helmut (Dsseldorf DEX) Schilling Hartmut (Kaarst DEX) Becker Hanjoerg (Dsseldorf DEX) Glotz Gerhard (Dsseldorf DEX). Projectile with rotatable stabilizing device. USP1990024903917.
  15. De Luca Nicholas J. (721 E. Cordova St. #1 Pasadena CA 91101). Recreational and sport rocket construction. USP1993125271579.
  16. Klestadt Ralph H. (Sherman Oaks CA). Rotationally mounted flexible band wing. USP1995055417393.
  17. Stoy David R. (Woodland Hills CA). Separately banking maneuvering aerodynamic control surfaces, system and method. USP1994065322243.
  18. Bar, Klaus; Bohl, Jurgen; Kautzsch, Karl. Spin-stabilized projectile with a braking device. USP2003016511016.
  19. Kusic, Tom. Spiralling missile--A. USP2003116644587.
  20. Kusic, Tom. Spiralling missile--B. USP2003116648433.
  21. Deakin Richard S. (Haslemere GBX). Stabilization systems. USP1993025186413.
  22. Walker Robert A. (17130 Roscoe Blvd. Los Angeles CA 91325). Two-axis rudder trim for aircraft. USP1983024373689.
  23. Ullrich Hans-Gunter,DEX. Vane control system for a guided missile. USP1999115975461.