JP6845746B2 - 航空機のヨー制御 - Google Patents

航空機のヨー制御 Download PDF

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Publication number
JP6845746B2
JP6845746B2 JP2017105216A JP2017105216A JP6845746B2 JP 6845746 B2 JP6845746 B2 JP 6845746B2 JP 2017105216 A JP2017105216 A JP 2017105216A JP 2017105216 A JP2017105216 A JP 2017105216A JP 6845746 B2 JP6845746 B2 JP 6845746B2
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JP
Japan
Prior art keywords
deflector
shaft
swept wing
control device
yaw control
Prior art date
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Application number
JP2017105216A
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English (en)
Japanese (ja)
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JP2017226408A (ja
JP2017226408A5 (enExample
Inventor
マール ドーセット ケネス
マール ドーセット ケネス
カール ストーリー ロバート
カール ストーリー ロバート
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Lockheed Martin Corp
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Lockheed Martin Corp
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Publication date
Application filed by Lockheed Martin Corp filed Critical Lockheed Martin Corp
Publication of JP2017226408A publication Critical patent/JP2017226408A/ja
Publication of JP2017226408A5 publication Critical patent/JP2017226408A5/ja
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Publication of JP6845746B2 publication Critical patent/JP6845746B2/ja
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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/34—Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/08—Stabilising surfaces mounted on, or supported by, wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/30—Transmitting means without power amplification or where power amplification is irrelevant mechanical using cable, chain, or rod mechanisms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/12—Adjustable control surfaces or members, e.g. rudders surfaces of different type or function being simultaneously adjusted
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B64C9/323—Air braking surfaces associated with wings
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Braking Arrangements (AREA)
  • Tires In General (AREA)
JP2017105216A 2016-05-27 2017-05-29 航空機のヨー制御 Active JP6845746B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/166,369 US10486793B2 (en) 2016-05-27 2016-05-27 Yaw control in an aircraft
US15/166,369 2016-05-27

Publications (3)

Publication Number Publication Date
JP2017226408A JP2017226408A (ja) 2017-12-28
JP2017226408A5 JP2017226408A5 (enExample) 2020-07-02
JP6845746B2 true JP6845746B2 (ja) 2021-03-24

Family

ID=58772464

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2017105216A Active JP6845746B2 (ja) 2016-05-27 2017-05-29 航空機のヨー制御

Country Status (3)

Country Link
US (1) US10486793B2 (enExample)
EP (1) EP3248866B1 (enExample)
JP (1) JP6845746B2 (enExample)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10967957B2 (en) * 2016-12-20 2021-04-06 The Boeing Company Methods and apparatus to extend a leading-edge vortex of a highly-swept aircraft wing
CN110697024B (zh) * 2019-10-14 2022-07-15 中国航空工业集团公司西安飞机设计研究所 一种飞机尾翼结构
JP7616930B2 (ja) * 2021-03-29 2025-01-17 株式会社Subaru 単発プロペラ機におけるジェット機操縦特性模擬システム及び単発プロペラ機

Family Cites Families (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1280195A (en) 1917-07-20 1918-10-01 Warren S Eaton Aeroplane-stabilizer.
US1545808A (en) 1923-02-28 1925-07-14 Ajello Gaetan Safety device for aircraft
US1724456A (en) 1928-04-24 1929-08-13 Louis H Crook Aerodynamic control of airplane wings
US2003223A (en) * 1933-06-17 1935-05-28 William K Rose Airplane
DE708447C (de) 1936-01-31 1941-07-21 Forschungsanstalt Fuer Segelfl Sturzflugbremse
DE737178C (de) 1936-02-19 1943-07-08 Forschungsanstalt Fuer Segelfl Sturzflugbremse
DE726413C (de) 1936-05-13 1942-10-13 Forschungsanstalt Fuer Segelfl Sturzflugbremse
DE718322C (de) 1936-07-26 1942-03-09 Forschungsanstalt Fuer Segelfl Sturzflugbremse
US2373089A (en) 1940-11-02 1945-04-10 Boeing Aircraft Co Stall delaying and indicating mechanism
US2373088A (en) 1940-11-02 1945-04-10 Boeing Aircraft Co Stall indicator
US2433649A (en) * 1944-03-14 1947-12-30 Cloyd P Clevenger Aircraft control surfaces for yaw control
US2557829A (en) 1947-11-07 1951-06-19 Thomas B Lavelle Aircraft control means
US2723091A (en) 1951-02-01 1955-11-08 Roe A V & Co Ltd Air or dive brakes for aircraft
US2852211A (en) 1956-09-21 1958-09-16 Xenakis George Airplane wing with aerodynamically actuated spoiler
US2987277A (en) 1958-10-14 1961-06-06 North American Aviation Inc Aircraft control system
GB919793A (en) 1961-11-14 1963-02-27 Sergio Caciagli Improvements relating to aircraft wings
US3107882A (en) 1962-08-10 1963-10-22 Electric Auto Lite Co Yaw control system for vtol tilt wing aircraft
US3721406A (en) 1970-12-14 1973-03-20 Boeing Co Aircraft wing airflow control system
US3774869A (en) * 1972-03-07 1973-11-27 K Harmon Combined throttle spoiler actuator for aircraft
US4132375A (en) 1976-01-21 1979-01-02 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Vortex-lift roll-control device
US4391424A (en) 1976-08-30 1983-07-05 Ball Brothers Method and structure for airfoil thrust and lift control
US4566657A (en) * 1979-05-21 1986-01-28 Grow Harlow B Span loaded flying wing control
US4466586A (en) 1980-03-10 1984-08-21 The Boeing Company Directional control device for aircraft
US4739957A (en) 1986-05-08 1988-04-26 Advanced Aerodynamic Concepts, Inc. Strake fence flap
GB2237254A (en) 1989-10-25 1991-05-01 Richard Harry Barnard Secondary lifting surfaces using separated flow
ES2137092B1 (es) 1996-11-14 2000-08-16 Munoz Saiz Manuel Flap automatico.
US6491261B1 (en) 2000-04-17 2002-12-10 The United States Of America As Represented By The Secretary Of The Air Force Wing mounted aircraft yaw control device
US7503527B1 (en) 2004-01-22 2009-03-17 Fairchild Mark D Flight control method and apparatus to produce induced yaw
FR2902077B1 (fr) * 2006-06-13 2009-04-24 Airbus France Sas Dispositif de surfaces portantes mobiles pour voilure d'aeronef
KR101287624B1 (ko) 2013-02-25 2013-07-23 주식회사 네스앤텍 착륙이 용이한 무인비행체
US9845147B2 (en) 2013-05-01 2017-12-19 Northrop Grumman Systems Corporation Recessed lift spoiler assembly for airfoils

Also Published As

Publication number Publication date
US10486793B2 (en) 2019-11-26
JP2017226408A (ja) 2017-12-28
EP3248866B1 (en) 2022-08-24
US20170341731A1 (en) 2017-11-30
EP3248866A1 (en) 2017-11-29

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