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Trailing edge flap

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50    B64C-003/54   
미국특허분류(USC) 244/215; 244/218; 244/213
출원번호 US-0939211 (2010-11-04)
등록번호 US-8714493 (2014-05-06)
우선권정보 GB-0920968.5 (2009-11-27)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Lowe Hauptman & Ham, LLP
인용정보 피인용 횟수 : 16  인용 특허 : 18
초록
▼

A single slotted trailing edge flap arrangement for an aircraft wing, comprising a main flap element and an auxiliary flap element sealed to and supported by the main flap element for movement between a retracted and an extended position relative to the main flap element so as to vary the planform area of the flap. The auxiliary flap element remains sealed to the main flap element when in its extended position, and movement of the auxiliary flap element relative to the main flap element is solely translational. The auxiliary flap element may be translati...

대표
청구항
▼

1. A single slotted trailing edge flap arrangement for an aircraft wing, comprising: a main flap element and a first actuator for moving the main flap element relative to the wing,an auxiliary flap element sealed to and supported by the main flap element for movement between a retracted position and an extended position relative to the main flap element so as to vary the planform area of the flap, and a second actuator for moving the auxiliary flap element between the extended position and the retracted position independently of the movement of the main ...

이 특허에 인용된 특허 (18)

  1. Lam Lawrence Y. ; Lam Michael. Aileron for fixed wing aircraft. USP2000066079672.
  2. Weiland Richard H. (Seattle WA) Franklin William L. (Bothell WA). Aircraft trailing edge flap apparatus. USP1987104702442.
  3. Reckzeh, Daniel; Dyke, Adrian R.. Aircraft wing, method for operating an aircraft wing, and use of a pivotable trailing edge on a main wing of an aircraft, for adjusting the shape and width of an air gap. USP2009047520471.
  4. Atchison Donald L. (Gilbert AZ) Hines Marshall U. (Scottsdale AZ) Ball Larry K. (Chandler AZ). Control surface structures for fluid-borne vehicles and method for rotationally moving such structures. USP1992075127605.
  5. Sankrithi Mithra M. K. V. (417 Bellevue Way SE. #400 Bellevue WA 98004). Flexible flap for an airfoil. USP1984074460138.
  6. Libby, John. High lift longitudinal axis control system. USP2010027661630.
  7. Libby,John. High lift longitudinal axis control system. USP2008057367532.
  8. Arena Aldo (Smithtown NY). Integrated power hinge actuator. USP1992035098043.
  9. Arena Aldo (Smithtown NY). Linear flap drive system. USP1997075651513.
  10. Milliere,J챕r척me. Method and spoiler system for ensuring the aerodynamic continuity of the upper surface of an aircraft. USP2006016981676.
  11. Perez Sanchez, Juan. Pivoted flap mechanism for adjusting an aerodynamic pivoted flap associated with a wing. USP2009107600718.
  12. Lewis Delbert S. (Bellevue WA) Norton David A. (Bellevue WA) Person Robert P. (Mercer Island WA) Schairer George S. (Bellevue WA) Wimpress John K. (Seattle WA). STOL aircraft. USP1976083977630.
  13. Berry Patrick,SEX. Segmented flap with variable camber for aircraft wing. USP2000096123297.
  14. Arena Aldo (Smithtown NY). Segmented variable sweep wing aircraft. USP1994055312070.
  15. Kaniut Herbert (Orrerweg 33/35 5000 Cologne 71 DT). Shifting horizontal tail with helical motions. USP1977054025007.
  16. Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L.. Systems and methods for controlling aircraft flaps and spoilers. USP2011027891611.
  17. Heynatz Johann T. (Immenstaad DEX). Trailing edge flap operation in wings. USP1989014796840.
  18. Dean Roy Delmar (BOTH OFSeattle WA) Weiland Richard Herschel (BOTH OFSeattle WA). Variable pivot trailing edge flap. USP1977094049219.

이 특허를 인용한 특허 피인용횟수: 16

  1. Moser, Matthew A.; Finn, Michael R.. Adaptive trailing edge actuator system and method. USP20180710017243.
  2. Habibvand, Alex; Cowles, Jr., John H.; Murphy, Richard. Bearing installed on an aircraft structure. USP2017029561845.
  3. Habibvand, Alex. Cage for hourglass roller bearings. USP2018029890814.
  4. Habibvand, Alex. Composite annular seal assembly for bearings in aircraft. USP2016019227720.
  5. Habibvand, Alex; Gyuricsko, Frederick S.; Phoenix, Jay; Fredericksen, Arnold E.; Cowles, Jr., John H.. Corrosion resistant bearing material. USP20180710012265.
  6. Cowles, Jr., John H.; Habibvand, Alex; Murphy, Richard. Roller profile for hourglass roller bearings in aircraft. USP20180910077808.
  7. Sobolewski, Pawel A.; Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Szulyk, Zenon P.. Rotary piston actuator anti-rotation configurations. USP2017049631645.
  8. Kim, Joseph H.; O Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.. Rotary piston type actuator. USP2016019234535.
  9. Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.. Rotary piston type actuator. USP20180710030679.
  10. Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.. Rotary piston type actuator with a central actuation assembly. USP2017079709078.
  11. Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.. Rotary piston type actuator with a central actuation assembly. USP2017119816537.
  12. Kim, Joseph H; O'Hara, Robert P; Hydari, Shahbaz H; Sobolewski, Pawel A.. Rotary piston type actuator with a central actuation assembly. USP2015109163648.
  13. Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.; Szulyk, Zenon P.. Rotary piston type actuator with hydraulic supply. USP2017039593696.
  14. Sobolewski, Pawel A.; Kim, Joseph H.; Szulyk, Zenon P.. Rotary piston type actuator with modular housing. USP2016109476434.
  15. Sobolewski, Pawel A.; Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.. Rotary piston type actuator with pin retention features. USP2015028955425.
  16. Murphy, Richard; Johnston, Dean P.. Seal for self aligning roller bearing. USP20180910082179.

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