• 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Aircraft spiralling mechanism-B

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/08    B64C-009/00   
미국특허분류(USC) 244/034.R; 244/039; 244/003.1; 244/003.24
출원번호 US-0759090 (2004-01-20)
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...

이 특허에 인용된 특허 (19)

  1. Stahlkopf Friedrich R. R. (Bchen DEX). Device for regulating the pressure and feed volume of a diaphragm pump. USP1986014564340.
  2. Wisshaupt Daniel (Orlans la source FRX). Device for roll attitude control of a fin-stabilized projectile. USP1991095048772.
  3. Gregory Malejko ; John C. Grau. Fin-stabilized projectile with improved aerodynamic performance. USP2002096443391.
  4. Peckham Derek H. (Farnham GBX). Guided missiles. USP1992085139215.
  5. MacDonald ; Gilmour C.. Helical path munitions delivery. USP1978054086841.
  6. Niemeier Byron M. (Claremont CA). Mechanical roll rate stabilizer for a rolling missile. USP1977064029270.
  7. Kranz Walter (Taufkirchen DEX). Missile having rotor ring. USP1990104964593.
  8. Silich Bert A. (Oswego IL). N-dimensional fighter aircraft. USP1993015176338.
  9. 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.
  10. Peller Helmut (Dsseldorf DEX) Schilling Hartmut (Kaarst DEX) Becker Hanjoerg (Dsseldorf DEX) Glotz Gerhard (Dsseldorf DEX). Projectile with rotatable stabilizing device. USP1990024903917.
  11. De Luca Nicholas J. (721 E. Cordova St. #1 Pasadena CA 91101). Recreational and sport rocket construction. USP1993125271579.
  12. Klestadt Ralph H. (Sherman Oaks CA). Rotationally mounted flexible band wing. USP1995055417393.
  13. Stoy David R. (Woodland Hills CA). Separately banking maneuvering aerodynamic control surfaces, system and method. USP1994065322243.
  14. Bar, Klaus; Bohl, Jurgen; Kautzsch, Karl. Spin-stabilized projectile with a braking device. USP2003016511016.
  15. Kusic, Tom. Spiralling missile--A. USP2003116644587.
  16. Kusic, Tom. Spiralling missile--B. USP2003116648433.
  17. Deakin Richard S. (Haslemere GBX). Stabilization systems. USP1993025186413.
  18. Walker Robert A. (17130 Roscoe Blvd. Los Angeles CA 91325). Two-axis rudder trim for aircraft. USP1983024373689.
  19. Ullrich Hans-Gunter,DEX. Vane control system for a guided missile. USP1999115975461.