$\require{mediawiki-texvc}$
  • 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

Adaptive compliant wing and rotor system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/48    B64C-003/00   
미국특허분류(USC) 244/123.1; 244/201
출원번호 US-0548053 (2004-03-03)
등록번호 US-7384016 (2008-06-10)
국제출원번호 PCT/US04/006876 (2004-03-03)
§371/§102 date 20050902 (20050902)
국제공개번호 WO04/108525 (2004-12-16)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Rohm & Monsanto, PLC
인용정보 피인용 횟수 : 29  인용 특허 : 28
초록

Variation in the contours of first and second compliant surfaces is produced by a compliant frame having a first resiliently variable frame element (120) having a corresponding first outer surface (122) and a first inner surface (124), and a second resiliently variable frame element (130) having a corresponding second outer surface (132) and a second inner surface (134). The first and second outer surfaces (122, 132) communicate with respective ones of the first and second compliant surfaces. A linkage element (141-144) having a predetermined resilience...

대표
청구항

What is claimed is: 1. An arrangement for producing a variation in the contour of a compliant surface, the arrangement comprising: a compliant frame having, a first resiliently variable frame element having a corresponding first outer surface and a first inner surface, and a second resiliently variable frame element having a corresponding second outer surface and a second inner surface, the first outer surface being arranged in substantially distal opposition to the second outer surface and in communication with the compliant surface, wherein the variat...

이 특허에 인용된 특허 (28)

  1. Young Kendall G. ; Zimmerman Phil S.. Adaptive control surface apparatus. USP2000126164598.
  2. Maclean Brian J. (Daniel WY) Carpenter Bernard F. (Littleton CO) Misra Mohan S. (Golden CO). Adaptive control surface using antagonistic shape memory alloy tendons. USP1997095662294.
  3. Gruenewald Michael,DEX ; Moeser Clemens,DEX ; Steigenberger Josef,DEX ; Mueller Guenther,DEX. Adaptive flow body. USP2001086276641.
  4. Krall Kenneth M. (Arlington TX). Airfoil construction. USP1981104296900.
  5. Bauer Claus,DEX. Airfoil with a landing flap having a flexible trailing edge. USP2000066076775.
  6. Croswell ; Jr. Thomas L. (1703 Hunts End Court Vienna VA 22180). Airplane wing camber control. USP1976013930626.
  7. McAnally Robert W. (Fort Worth TX). Continuous force actuator. USP1982094349169.
  8. Geiger Michael Watson ; Waldrop ; III John Cleveland,ESX ITX 28223. Continuous moldline technology system. USP1998095810291.
  9. Statkus Frank D. (Woodinville WA). Continuous skin, variable camber airfoil edge actuating mechanism. USP1982094351502.
  10. Beauchamp Charles H. (Jamestown RI) Dean Laurence M. (Newport RI) Raffa Anthony V. (Newport RI). Controllable camber fin. USP1994115367970.
  11. Paterson ; John Howard ; Wilson ; Jr. ; Francis Marion. Drag reducer for lift surface of aircraft. USP1978014067518.
  12. Diller Joseph B. ; Miller ; Jr. Nicholas F.. Elastomeric transition for aircraft control surface. USP1998085794893.
  13. Compton Christopher J. (Hatfield GB2). Flow deflector blades. USP1980114235397.
  14. Roselli Auro (319 E. 51st St. New York NY 10022). Inflated wing aircraft. USP1981044261534.
  15. Thompson Harold L. (Okmulgee OK). Land, water and air craft. USP1989094865275.
  16. Muller Dietmar,DEX. Lift body having a variable camber. USP2000116152405.
  17. Martin Willi,DEX ; Siegling Hans-Friedrich,DEX ; Kuhn Marcel,DEX ; Himmel Norbert,DEX. Load carrying structure having variable flexibility. USP2001026182929.
  18. Perez, Juan. Mechanism for at least regionally adjusting the curvature of airfoil wings. USP2003116644599.
  19. Becker, Juergen. Process for designing flight controllers. USP2004116816823.
  20. Fuller Brian L. (1167 Danner St. ; SE. Atlanta GA 30316). Rollable airfoil. USP1984124485991.
  21. Appa Kari. Seamless mission adaptive control surface. USP1999035887828.
  22. Arata Allen A.. Single surface multi axis aircraft control. USP2000056068219.
  23. Livingston David E. (Huntsville AL) Kornell Thomas J. (Federal Way WA). Single-piece, flexible inlet ramp. USP1991075033693.
  24. Mueller Dietmar,DEX ; Schuermann Helmut,DEX. Skin-rib structure. USP2001016173925.
  25. Kota Sridhar. System for varying a surface contour. USP1999105971328.
  26. Palmer Harry W. (P.O. Box 821 Denmark ME 04022). Torsional twist airfoil control means. USP1997105681014.
  27. Rinn Aaron ; Khamly Somphone ; Hornick David ; Obrigkeit Matthew ; Kota Sridhar. Variable camber airfoil. USP2000046045096.
  28. Roglin Robert L. (Duluth GA) Hanagud Sathyanaraya (Atlanta GA). Variable camber control of airfoil. USP1992095150864.

이 특허를 인용한 특허 피인용횟수: 29

  1. Pitt, Dale M.; Eckstein, Nicholas Stephen. Active twisting of an aircraft lifting surface via modulated clamping of substructure. USP2012038128020.
  2. Iannucci, Lorenzo. Aerofoil member. USP2012058186631.
  3. Reany, Jack W.; Sanderson, Terry M.. Aircraft wing with flexible skins. USP2014058714476.
  4. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2014098844294.
  5. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2013018353164.
  6. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2014058726632.
  7. Jain, Ashok K.. Nacelle flow assembly. USP2013128596573.
  8. Hemmelgarn, Christopher Douglas; Pelley, Bryan Michael. Passive adaptive structures. USP2015059033283.
  9. Hemmelgarn, Christopher Douglas; Pelley, Bryan Michael. Passive adaptive structures. USP2013048418967.
  10. Hemmelgarn, Christopher Douglas; Pelley, Bryan Michael; Cable, Kristin Marie; Kirby, Brandon Charles. Passive adaptive structures. USP2014038678324.
  11. Sobolewski, Pawel A.; Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Szulyk, Zenon P.. Rotary piston actuator anti-rotation configurations. USP2017049631645.
  12. Kim, Joseph H.; O Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.. Rotary piston type actuator. USP2016019234535.
  13. Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.. Rotary piston type actuator. USP20180710030679.
  14. Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.. Rotary piston type actuator with a central actuation assembly. USP2017079709078.
  15. Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.. Rotary piston type actuator with a central actuation assembly. USP2017119816537.
  16. Kim, Joseph H; O'Hara, Robert P; Hydari, Shahbaz H; Sobolewski, Pawel A.. Rotary piston type actuator with a central actuation assembly. USP2015109163648.
  17. Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.; Szulyk, Zenon P.. Rotary piston type actuator with hydraulic supply. USP2017039593696.
  18. Sobolewski, Pawel A.; Kim, Joseph H.; Szulyk, Zenon P.. Rotary piston type actuator with modular housing. USP2016109476434.
  19. Sobolewski, Pawel A.; Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.. Rotary piston type actuator with pin retention features. USP2015028955425.
  20. Wigley, Alexander T.. Shape shifting foils. USP2018049944356.
  21. Sar, David R.; Sanderson, Terry M.. Structural member with clamping pressure mechanism. USP2014058727079.
  22. Bussom, Richard; McVeigh, Michael A.; Narducci, Robert P.; Zientek, Thomas A.. System and method for improved rotor tip performance. USP2010077757992.
  23. De Gregorio Hurtado, Yolanda; Balsa Gonzalez, Alberto. Trailing edge of an aircraft aerodynamic surface. USP2015089108721.
  24. Joo, James J. Variable camber adaptive compliant wing system. USP2018029896188.
  25. Joo, James J.. Variable camber adaptive compliant wing system. USP2016019233749.
  26. Jain, Ashok K.; Winter, Michael. Variable contour nacelle assembly for a gas turbine engine. USP2016019228534.
  27. Jain, Ashok K.; Winter, Michael. Variable contraction ratio nacelle assembly for a gas turbine engine. USP2014058727267.
  28. Jain, Ashok K.; Chaudhry, Zaffir A.. Variable shape inlet section for a nacelle assembly of a gas turbine engine. USP2013038402739.
  29. Hancock, Mark. Wind turbine blade with device for changing the aerodynamic surface or shape. USP2014128899923.