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Control surface for an aircraft 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-009/00
  • B64C-003/58
출원번호 US-0517838 (2000-03-02)
발명자 / 주소
  • Caton John Harold
  • Hobey Michael James
  • Groeneveld John David
  • Jacobs Jack Howard
  • Wille Robert Henry
  • Brase
  • Jr. Lawrence Otto
출원인 / 주소
  • The Boeing Company
인용정보 피인용 횟수 : 26  인용 특허 : 36

초록

A control surface (152) for an aircraft has a reinforced elastomer surface (154) on a surface of the aircraft and has a perimeter (156) attached to the aircraft. An actuation mechanism (160) moves the reinforced elastomer surface (154) from a first position, substantially conforming to a moldline of

대표청구항

[What is claimed is:] [1.]a reinforced elastomer member forming a portion of the surface of the component of the aircraft and having a perimeter attached to the component of the aircraft, the reinforced elastomer member having an elastomer skin containing a plurality of reinforcing members;a spine m

이 특허에 인용된 특허 (36)

  1. Geiger Michael Watson ; Gruensfelder Cynthia Ann ; Jacobs Jack Howard, Active reinforced elastomer system.
  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.
  3. Zell Peter T. (San Jose CA), Aerodynamic surface distension system for high angle of attack forebody vortex control.
  4. Krall Kenneth M. (Arlington TX), Airfoil construction.
  5. O'Neil Patrick J., Airfoil lift management device.
  6. Gruensfelder Cynthia Ann ; Geiger Micael Watson ; Jacobs Jack Howard ; Wille Robert Henry, Apparatus for eliminating gaps in an aircraft.
  7. Nedderman ; Jr. William H., Articulated fin.
  8. Burbridge Thomas Edward ; Tomko Harvey John ; Wille Robert Henry, Blade seal for an aircraft.
  9. Hertzberg Paul E. (San Diego CA), Composites made of fiber reinforced resin elements joined by adhesive.
  10. Geiger Michael Watson ; Waldrop ; III John Cleveland,ESX ITX 28223, Continuous moldline technology system.
  11. Nedderman ; Jr William H. (Middletown RI), Control surface for underwater vehicle.
  12. Beauchamp Charles H. (Jamestown RI) Dean Laurence M. (Newport RI) Raffa Anthony V. (Newport RI), Controllable camber fin.
  13. Diller Joseph B. ; Miller ; Jr. Nicholas F., Elastomeric transition for aircraft control surface.
  14. Geiger Michael Watson, Environmental coating for an elastomer panel.
  15. Gruensfelder Cynthia Ann ; Wille Robert Henry, Expandable aircraft bay and method.
  16. Ellis James R. ; Diller Joseph B., Expandable aircraft section.
  17. Geders Paul Francis ; Groeneveld John David ; Wille Robert Henry, Expandable fuel cell.
  18. Jacobs Jack H. (St. Louis MO) Thomas Matthew M. (Madison IL) Grosskrueger Duane D. (Highlands Ranch CO) Carpenter Bernie F. (Littleton CO) Perry Alan R. (Morrison CO), Fabrication method for composite structure adapted for controlled structural deformation.
  19. Cameron Dean Emory, Fairing for an expandable bay.
  20. Loewy Robert G. (Loudonville NY) Miao Wen-Liu (Trumbull CT), Feedback-stabilized aerodynamically overbalanced lifting/control surface for aircraft.
  21. Narramore Jimmy C. (Bedford TX), Flaperon system for tilt rotor wings.
  22. Yamakawa Eiichi (Kakamigahara JPX) Kobiki Noboru (Kakamigahara JPX) Shima Eiji (Kakamigahara JPX), Helicopter rotor equipped with flaps.
  23. Michel Philip L. (Newtown CT), Helicopter rotor with blade trailing edge tabs responsive to control system loading.
  24. Wille Robert Henry, Hinge line skin system for an aircraft.
  25. Covey James H. (Snohomish WA), Method for plating one side of a woven fabric sheet.
  26. Jacobsen Stephen C. (Salt Lake City UT), Movement actuator/sensor systems.
  27. Lazarus Kenneth B. (Boston MA) Crawley Edward F. (Cambridge MA), Multivariable adaptive surface control.
  28. Meyerhoefer Carl E., Optical fiber strain relief system.
  29. Beier Theodor Harry ; Haake John Martin ; Wille Robert Henry ; Jacobs Jack Howard, Reinforced elastomer panel with embedded strain and pressure sensors.
  30. Sommer William Arthur ; Wille Robert Henry, Retractable sensor system for an aircraft.
  31. DeLaurier James D. (60 Cherry Hills Rd. Concord ; Ontario OH CAX L4K 1M4) Harris Jeremy M. (476 Park Overlook Worthington OH 43085), Spanwise graded twist panel.
  32. Wille Robert Henry, Tail for an aircraft.
  33. Brown Stephen T. (Bellevue WA) Statkus Frank D. (Woodinville WA), Variable camber aircraft wing tip.
  34. Brown Stephen T. (Bellevue WA), Variable camber flap end seal.
  35. Cole James B. (Mercer Island WA), Variable camber leading edge assembly for an airfoil.
  36. Albach Walter C. (Dallas TX) Fewel Kenneth J. (Nacogdoches TX), Variable control aircraft control surface.

이 특허를 인용한 특허 (26)

  1. Elzey,Dana M.; Wadley,Haydn N. G., Active energy absorbing cellular metals and method of manufacturing and using the same.
  2. Mabe, James H.; Calkins, Frederick T.; Bushnell, Glenn S.; Bieniawski, Stefan R., Aircraft systems with shape memory alloy (SMA) actuators, and associated methods.
  3. Dunne, James P.; Pitt, Dale M.; Kilian, Kevin J.; White, Edward V., Apparatus for variation of a wall skin.
  4. Geders, Paul F., Continuous moldline technology (CMT) elastomeric control surface.
  5. John Harold Caton ; Michael James Hobey ; John David Groeneveld ; Jack Howard Jacobs ; Robert Henry Wille ; Lawrence Otto. Brase, Jr., Control surface for an aircraft.
  6. Khorrami, Mehdi R.; Lockard, David P.; Moore, James B.; Su, Ji; Turner, Travis L.; Lin, John C.; Taminger, Karen M.; Kahng, Seun K.; Verden, Scott A., Elastically deformable side-edge link for trailing-edge flap aeroacoustic noise reduction.
  7. Arata, Allen A., Elastomeric transition.
  8. Kopanski, Kris; Cowles, Devon; Bruno, David E.; Miner, Frederick J.; Hein, Benjamin Reed, Flexbeam hinge for helicopter blade active trailing edge flap.
  9. Eveker, James V.; Young, Roger K., Hinge cover integration into door seal edges.
  10. Eveker, James V.; Young, Roger K., Hinge cover integration into door seal edges.
  11. Eveker, James V.; Young, Roger K., Hinge cover integration into door seal edges.
  12. Kholwadwala,Deepesh K.; Johnston,Gabriel A.; Rohrer,Brandon R.; Galambos,Paul C.; Okandan,Murat, MEMS fluidic actuator.
  13. Kane, Daniel J., Memory shape bushings and bearings.
  14. Wadley, Haydn N. G.; Queheillalt, Douglas T.; Haj-Hariri, Hossein; Evans, Anthony G.; Peterson, George P.; Kurtz, Robert; Long, G. Douglas; Murty, Yellapu V., Method and apparatus for jet blast deflection.
  15. Loyet, Jessica; Pitt, Dale M., Mitigation of surface discontinuities between flight control surfaces and an airframe of an aircraft.
  16. Etling, Keith A., Morphing control surface transition.
  17. Elzey, Dana M.; Wadley, Haydn N. G., Reversible shape memory multifunctional structural designs and method of using and making the same.
  18. Wilson, James; West, Colin John; Sutton, David Alistair; Hadley, Paul, Seal.
  19. Martin Hernandez, Agustín Mariano, Sealing system for the gap existing between the fuselage and the elevator of the orientable horizontal stabiliser of an aircraft, extended with an aerodynamic fairing for sealing of the opening existing between the fuselage and the orientable horizontal stabiliser.
  20. Wood,Jeffrey H, Shape changing structure.
  21. Jasklowski, Christopher T., Shape memory alloy actuation system for variable area fan nozzle.
  22. Mabe, James H.; Calkins, Frederick T.; Bushnell, Glenn S.; Bieniawski, Stefan R., Shape memory alloy actuator.
  23. Madsen, Casey Lyn, Shape memory alloy rods for actuation of continuous surfaces.
  24. Da Rocha-Schmidt, Luiz, Shape-variable gap covering between control surfaces and adjacent structural components on aircrafts.
  25. Nguyen, Nhan T., Variable camber continuous aerodynamic control surfaces and methods for active wing shaping control.
  26. Dyckrup, Werner, Wing for an aircraft.
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