JPS51135100A - Wing and body assembly - Google Patents

Wing and body assembly

Info

Publication number
JPS51135100A
JPS51135100A JP50155136A JP15513675A JPS51135100A JP S51135100 A JPS51135100 A JP S51135100A JP 50155136 A JP50155136 A JP 50155136A JP 15513675 A JP15513675 A JP 15513675A JP S51135100 A JPS51135100 A JP S51135100A
Authority
JP
Japan
Prior art keywords
wing
body assembly
assembly
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.)
Pending
Application number
JP50155136A
Other languages
English (en)
Japanese (ja)
Inventor
Ripaato Jiyunia Yosefu
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.)
Grumman Corp
Original Assignee
Grumman Aerospace Corp
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 Grumman Aerospace Corp filed Critical Grumman Aerospace Corp
Publication of JPS51135100A publication Critical patent/JPS51135100A/ja
Pending legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • B64C7/02—Nacelles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • 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
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)
JP50155136A 1975-05-16 1975-12-26 Wing and body assembly Pending JPS51135100A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/578,199 US3960345A (en) 1975-05-16 1975-05-16 Means to reduce and/or eliminate vortices, caused by wing body combinations

Publications (1)

Publication Number Publication Date
JPS51135100A true JPS51135100A (en) 1976-11-22

Family

ID=24311839

Family Applications (1)

Application Number Title Priority Date Filing Date
JP50155136A Pending JPS51135100A (en) 1975-05-16 1975-12-26 Wing and body assembly

Country Status (5)

Country Link
US (1) US3960345A (show.php)
JP (1) JPS51135100A (show.php)
BR (1) BR7508679A (show.php)
FR (1) FR2310919A1 (show.php)
IT (1) IT1056174B (show.php)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4264043A (en) * 1976-06-14 1981-04-28 Walker Robert A Stabilizer for aerospace vehicles
US4231536A (en) * 1977-10-11 1980-11-04 The Boeing Company Airfoil for controlling refueling boom
SE8101793L (sv) * 1980-03-25 1981-09-26 Nat Res Dev Luftplan
US4402378A (en) * 1981-01-07 1983-09-06 Amick James L Energy-efficient motorcycle
US4643376A (en) * 1982-09-30 1987-02-17 The Boeing Company Shock inducing pod for causing flow separation
US4685643A (en) * 1983-08-04 1987-08-11 The Boeing Company Nacelle/wing assembly with vortex control device
USD279469S (en) 1983-09-29 1985-07-02 Raisbeck James D Cargo carrier for attachment to the wing of aircraft
DE3815422A1 (de) * 1988-05-06 1989-11-16 Nikolaus Andreadis Flugzeug
US5249762A (en) * 1990-08-21 1993-10-05 Eidetics Internation, Inc. Strakes for landing speed reduction
US5490644A (en) * 1993-12-20 1996-02-13 The Boeing Company Ducted boundary layer diverter
FR2802896B1 (fr) * 1999-12-27 2002-03-29 Aerospatiale Matra Airbus Mat de suspension profile de voilure d'aeronef
FR2807389B1 (fr) * 2000-04-10 2002-06-14 Aerospatiale Matra Airbus Mat de suspension profile de voilure d'aeronef
GB2374331A (en) * 2000-12-15 2002-10-16 Robert Andrew Ledingham Aerofoil with protruding aerodynamic surface
EA008092B1 (ru) * 2003-07-25 2007-02-27 Государственное Учреждение "Федеральное Агентство По Правовой Защите Результатов Интеллектуальной Деятельности Военного, Специального И Двойного Назначения" При Министерстве Юстиции Российской Федерации Тренажер авиационный
US20080203233A1 (en) * 2007-02-23 2008-08-28 Schmidt Willard H Flueted aircraft wing
US7878458B2 (en) * 2007-10-29 2011-02-01 The Boeing Company Method and apparatus for enhancing engine-powered lift in an aircraft
DE102009003084B4 (de) * 2009-05-13 2013-03-14 Airbus Operations Gmbh Verkleidung für eine Auftriebshilfe
US8453974B1 (en) * 2010-12-13 2013-06-04 The Boeing Company Flow channels
US9233757B2 (en) 2011-11-10 2016-01-12 Rohr, Inc. Nacelle
US8727275B2 (en) 2012-01-27 2014-05-20 Rohr, Inc. Nacelle
US9783315B2 (en) 2012-02-24 2017-10-10 Rohr, Inc. Nacelle with longitudinal translating cowling and rotatable sleeves
US9371138B2 (en) 2012-06-07 2016-06-21 Rohr, Inc. Nacelle
CN103612769B (zh) 2013-10-24 2016-09-21 中国商用飞机有限责任公司 翼吊布局飞机中吊挂的整流罩结构
US9937998B2 (en) 2015-02-19 2018-04-10 Rohr, Inc. Method for manufacturing a nacelle strake
US20200324891A1 (en) * 2015-09-02 2020-10-15 Jetoptera, Inc. Adaptive vertical take-off and landing propulsion system
US10974813B2 (en) 2018-01-08 2021-04-13 General Electric Company Engine nacelle for an aircraft
EP3666646B1 (en) * 2018-12-13 2023-02-08 Rohr, Inc. Aerodynamic nacelle strakes as axial locator
US11148782B2 (en) 2018-12-13 2021-10-19 Rohr, Inc. Aerodynamic nacelle strakes as axial locator
WO2022157243A1 (en) 2021-01-22 2022-07-28 Blue Spirit Aero Sas Aircraft having retractable vortex generators
EP4032810A1 (en) * 2021-01-22 2022-07-27 Blue Spirit Aero SAS Aircraft with electric propulsion module

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB191512820A (en) * 1915-09-07 1916-10-05 George Anton Ogrissek Improvements in Air Craft.
FR784301A (fr) * 1935-01-17 1935-07-22 Avions Kellner Bechereau Soc D Perfectionnements apportés aux voilures utilisées en aéronautique
GB460636A (en) * 1935-08-01 1937-02-01 William Edrington Gray Aeroplane stabilising means
US2687262A (en) * 1947-09-19 1954-08-24 Willard R Custer Jet propelled channeled aircraft
GB664288A (en) * 1949-04-14 1952-01-02 Robert Talbot Youngman Improvements in or relating to stabilising devices for aircraft
US2994493A (en) * 1957-10-23 1961-08-01 Thomas A Hartman Channelled fan aircraft
US3129906A (en) * 1959-01-19 1964-04-21 David G Peterson Engine nacelle
GB1152982A (en) * 1966-02-21 1969-05-21 Short Brothers & Harland Ltd Improvements in Anti-Drag Arrangements for Aerial Bodies, or Bodies intended for Movement partly in an Aerial Medium
US3588005A (en) * 1969-01-10 1971-06-28 Scott C Rethorst Ridge surface system for maintaining laminar flow
US3704842A (en) * 1970-10-16 1972-12-05 Willard R Custer Contoured stack of jet engine with channel wing aircraft
US3744745A (en) * 1971-09-30 1973-07-10 Mc Donnell Douglas Corp Liftvanes
DE2149590C3 (de) * 1971-10-05 1974-04-25 Vereinigte Flugtechnische Werkefokker Gmbh, 2800 Bremen Flugzeug mit Kurz -Start- und Landeeigenschaften

Also Published As

Publication number Publication date
US3960345A (en) 1976-06-01
BR7508679A (pt) 1976-11-23
FR2310919A1 (fr) 1976-12-10
FR2310919B1 (show.php) 1980-03-28
IT1056174B (it) 1982-01-30

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