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특허 상세정보

STOL aircraft and wing slat actuating mechanism for same

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50   
미국특허분류(USC) 244/214 ; 244/215 ; 244/218 ; 244/220 ; 244/225 ; 74/104 ; 74/096 ; 74/108 ; 74/110
출원번호 US-0497725 (1995-06-30)
발명자 / 주소
대리인 / 주소
    Leydig, Voit & Mayer, Ltd.
인용정보 피인용 횟수 : 18  인용 특허 : 4
초록

A short take off and landing (STOL) aircraft is optimized for STOL performance and flight at minimum airspeed. The aircraft includes leading edge wing slats that are extended and retracted under the direct manual control of the pilot. The aircraft further includes an aileron/flap mixing mechanism that automatically droops the ailerons when the flaps are lowered. A flap bellcrank, which pivots to lower the flaps, carries a pair of pulleys. Aileron control cables, that actuate an aileron bellcrank to raise and lower an aileron, are threaded around and betw...

대표
청구항

[ I claim:] [1.] A control system for extending wing slats disposed along the leading edge of an aircraft wing, comprising:a slat positioning system havinga guide member disposed adjacent a leading edge of the aircraft wing and comprising an outer tube having an axially extending slot,a support member for supporting the wing slat and engaging said guide member for slidable movement relative to said guide member and comprising an inner tube telescopically received in said outer tube,a slat bellcrank adjacent said guide member and movable around a pivot, s...

이 특허를 인용한 특허 피인용횟수: 18

  1. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F.. Aerospace vehicle flow body systems and associated methods. USP2009037500641.
  2. Keennon, Matthew Todd; Andryukov, Alexander; Klingebiel, Karl Robert; Won, Henry Thome. Air vehicle flight mechanism and control method for non-sinusoidal wing flapping. USP20180910065737.
  3. Jones,Kelly T.. Aircraft control surface drive system and associated methods. USP2009037506842.
  4. Lacy, Douglas S.; Kordel, Jan A.; Dovey, John V.; Balzer, Michael A.; Sakurai, Seiya; Huynh, Neal V.. Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods. USP2010057708231.
  5. Lacy, Douglas S.; Kordel, Jan A.; Dovey, John V.; Balzer, Michael A.; Sakurai, Seiya; Huynh, Neal V.. Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods. USP2013108567726.
  6. Lacy, Douglas S.; Kordel, Jan A.; Dovey, John V.; Balzer, Michael A.; Sakurai, Seiya; Huynh, Neal V.. Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods. USP2011108038103.
  7. Lacy, Douglas S.; Beyer, Kevin W.; Brown, Stephen T.; Dees, Paul W.; Huynh, Neal V.; Kordel, Jan A.; Prow, Clayton A.; Sakurai, Seiya. Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods. USP2010067744040.
  8. Lacy,Douglas S.; Beyer,Kevin W.; Brown,Stephen T.; Dees,Paul W.; Huynh,Neal V.; Kordel,Jan A.; Prow,Clayton A.; Sakurai,Seiya. Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods. USP2009017475854.
  9. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael. Aircraft wing systems for providing differential motion to deployable lift devices. USP2009027494094.
  10. Wagner ; III Fred A.. Extendable/retractable airfoil assembly for fixed wing aircraft. USP2001066241195.
  11. Collins, Andrew J.. Flight control surface actuation system. USP2004086776376.
  12. Wheaton, James M.; Amorosi, Stephen R.. Leading edge flap apparatuses and associated methods. USP2010117828250.
  13. Fox, Stephen J.; Sakurai, Seiya. Link mechanisms for gapped rigid krueger flaps, and associated systems and methods. USP2009087578484.
  14. Manley, David J.; Grip, Robert E.. Shape-changing control surface. USP2013028382045.
  15. 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.
  16. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V.. Trailing edge device catchers and associated systems and methods. USP2010087766282.
  17. Rousseau, David G.. Variable geometry wing using a roll-up device. USP2012018100367.
  18. Speer,Thomas E.. Vehicle control systems and corresponding sizing methods. USP2008097424350.