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JPS5398699A - High lift producing apparatus for aircraft - Google Patents

High lift producing apparatus for aircraft

Info

Publication number
JPS5398699A
JPS5398699A JP1288877A JP1288877A JPS5398699A JP S5398699 A JPS5398699 A JP S5398699A JP 1288877 A JP1288877 A JP 1288877A JP 1288877 A JP1288877 A JP 1288877A JP S5398699 A JPS5398699 A JP S5398699A
Authority
JP
Japan
Prior art keywords
producing apparatus
high lift
aircraft
lift producing
notch
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP1288877A
Other languages
Japanese (ja)
Other versions
JPS5810277B2 (en
Inventor
Akira Hashimoto
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.)
Kawasaki Heavy Industries Ltd
Original Assignee
Kawasaki Heavy Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Kawasaki Heavy Industries Ltd filed Critical Kawasaki Heavy Industries Ltd
Priority to JP1288877A priority Critical patent/JPS5810277B2/en
Publication of JPS5398699A publication Critical patent/JPS5398699A/en
Publication of JPS5810277B2 publication Critical patent/JPS5810277B2/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B64C9/24—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • B64C7/02—Nacelles

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)

Abstract

PURPOSE: To provide a front edge high lift producing apparatus for a main wing, with which the stalling characteristic is improved by controlling the air stream passing through a notch formed for a pylon by providing a small wing plate adapted to fill part of the notch.
COPYRIGHT: (C)1978,JPO&Japio
JP1288877A 1977-02-08 1977-02-08 High lift device for aircraft Expired JPS5810277B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1288877A JPS5810277B2 (en) 1977-02-08 1977-02-08 High lift device for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1288877A JPS5810277B2 (en) 1977-02-08 1977-02-08 High lift device for aircraft

Publications (2)

Publication Number Publication Date
JPS5398699A true JPS5398699A (en) 1978-08-29
JPS5810277B2 JPS5810277B2 (en) 1983-02-24

Family

ID=11817929

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1288877A Expired JPS5810277B2 (en) 1977-02-08 1977-02-08 High lift device for aircraft

Country Status (1)

Country Link
JP (1) JPS5810277B2 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4637573A (en) * 1983-12-06 1987-01-20 Societe Nationale Industrielle Aerospatiale Arrowlike aircraft wing equipped with a high-lift system and with a pylon for suspending the engine
US6364254B1 (en) 1999-03-10 2002-04-02 Daimlerchrysler Aerospace Airbus Gmbh Aircraft airfoil with close-mounted engine and leading edge high lift system
WO2006093512A1 (en) * 2004-06-15 2006-09-08 The Boeing Company Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
JP2009528220A (en) * 2006-02-28 2009-08-06 エアバス・ユ―ケ―・リミテッド Aircraft wing
RU2761487C1 (en) * 2020-07-02 2021-12-08 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Sweptwing of the aircraft
CN116750185A (en) * 2023-05-17 2023-09-15 中国商用飞机有限责任公司 Leading edge lift-increasing layout

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4637573A (en) * 1983-12-06 1987-01-20 Societe Nationale Industrielle Aerospatiale Arrowlike aircraft wing equipped with a high-lift system and with a pylon for suspending the engine
US6364254B1 (en) 1999-03-10 2002-04-02 Daimlerchrysler Aerospace Airbus Gmbh Aircraft airfoil with close-mounted engine and leading edge high lift system
WO2006093512A1 (en) * 2004-06-15 2006-09-08 The Boeing Company Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
GB2430418A (en) * 2004-06-15 2007-03-28 Boeing Co Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
GB2430418B (en) * 2004-06-15 2008-12-31 Boeing Co Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
JP2009528220A (en) * 2006-02-28 2009-08-06 エアバス・ユ―ケ―・リミテッド Aircraft wing
RU2761487C1 (en) * 2020-07-02 2021-12-08 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Sweptwing of the aircraft
CN116750185A (en) * 2023-05-17 2023-09-15 中国商用飞机有限责任公司 Leading edge lift-increasing layout

Also Published As

Publication number Publication date
JPS5810277B2 (en) 1983-02-24

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