SE301089B - - Google Patents

Info

Publication number
SE301089B
SE301089B SE1813/66A SE181366A SE301089B SE 301089 B SE301089 B SE 301089B SE 1813/66 A SE1813/66 A SE 1813/66A SE 181366 A SE181366 A SE 181366A SE 301089 B SE301089 B SE 301089B
Authority
SE
Sweden
Application number
SE1813/66A
Inventor
K Oernberg
Original Assignee
Saab Ab
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 Saab Ab filed Critical Saab Ab
Priority to SE1813/66A priority Critical patent/SE301089B/xx
Priority to CH146167A priority patent/CH470287A/de
Priority to AT97167A priority patent/AT280059B/de
Priority to GB5427/67A priority patent/GB1179568A/en
Priority to FR94296A priority patent/FR1511212A/fr
Priority to US615230A priority patent/US3471107A/en
Publication of SE301089B publication Critical patent/SE301089B/xx

Links

Classifications

    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable
    • B64C5/12—Stabilising surfaces adjustable for retraction against or within fuselage or nacelle
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Tires In General (AREA)
SE1813/66A 1966-02-11 1966-02-11 SE301089B (es)

Priority Applications (6)

Application Number Priority Date Filing Date Title
SE1813/66A SE301089B (es) 1966-02-11 1966-02-11
CH146167A CH470287A (de) 1966-02-11 1967-02-01 Verfahren und Vorrichtung zur Unterdrückung von Wirbelablenkungen an der Oberseite von Tragflächen
AT97167A AT280059B (de) 1966-02-11 1967-02-02 Verfahren und Vorrichtung zur Unterdrückung von Wirbelablenkungen an der Oberfläche von Tragflächen
GB5427/67A GB1179568A (en) 1966-02-11 1967-02-03 Improvements relating to Aircraft Wings
FR94296A FR1511212A (fr) 1966-02-11 1967-02-09 Procédé et dispositif pour contrecarrer la déviation d'un vortex à partir de la surface d'ailes où se produisent des vortex interférant entre eux et de même sens de rotation
US615230A US3471107A (en) 1966-02-11 1967-02-10 Stabilizing the vortices over a thin delta wing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE1813/66A SE301089B (es) 1966-02-11 1966-02-11

Publications (1)

Publication Number Publication Date
SE301089B true SE301089B (es) 1968-05-20

Family

ID=20258881

Family Applications (1)

Application Number Title Priority Date Filing Date
SE1813/66A SE301089B (es) 1966-02-11 1966-02-11

Country Status (6)

Country Link
US (1) US3471107A (es)
AT (1) AT280059B (es)
CH (1) CH470287A (es)
FR (1) FR1511212A (es)
GB (1) GB1179568A (es)
SE (1) SE301089B (es)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3744745A (en) * 1971-09-30 1973-07-10 Mc Donnell Douglas Corp Liftvanes
US3892075A (en) * 1973-10-29 1975-07-01 Michael Edward Tibbett Apparatus for vortex generation to precipitate suspended particles in fluid bodies
US4017041A (en) * 1976-01-12 1977-04-12 Nelson Wilbur C Airfoil tip vortex control
US4323209A (en) * 1977-07-18 1982-04-06 Thompson Roger A Counter-rotating vortices generator for an aircraft wing
US4232516A (en) * 1977-10-05 1980-11-11 Rolls-Royce Limited Flow deflecting devices
US4293110A (en) * 1979-03-08 1981-10-06 The Boeing Company Leading edge vortex flap for wings
JPS58500892A (ja) * 1981-06-10 1983-06-02 ザ　ボ−イング　コンパニ− 翼のための前縁渦フラップ
US4485992A (en) * 1981-09-10 1984-12-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Leading edge flap system for aircraft control augmentation
US4643376A (en) * 1982-09-30 1987-02-17 The Boeing Company Shock inducing pod for causing flow separation
US4569494A (en) * 1982-12-23 1986-02-11 The Boeing Company Pitch control of swept wing aircraft
US4685643A (en) * 1983-08-04 1987-08-11 The Boeing Company Nacelle/wing assembly with vortex control device
US4655419A (en) * 1984-12-31 1987-04-07 The Boeing Company Vortex generator
US4739957A (en) * 1986-05-08 1988-04-26 Advanced Aerodynamic Concepts, Inc. Strake fence flap
US5062595A (en) * 1990-04-26 1991-11-05 University Of Southern California Delta wing with lift enhancing flap
US5094411A (en) * 1990-10-19 1992-03-10 Vigyan, Inc. Control configured vortex flaps
US5255881A (en) * 1992-03-25 1993-10-26 Vigyan, Inc. Lift augmentation for highly swept wing aircraft
EP0638042A4 (en) * 1992-04-28 1995-07-05 British Tech Group Usa BODY HAVING REDUCED LEAK EDGE WAVE.
US5230486A (en) * 1992-05-22 1993-07-27 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Underwing compression vortex attenuation device
GB9401691D0 (en) * 1994-01-28 1994-03-23 Hannay Ian Foils
US5806807A (en) * 1995-10-04 1998-09-15 Haney; William R. Airfoil vortex attenuation apparatus and method
US5901925A (en) * 1996-08-28 1999-05-11 Administrator, National Aeronautics And Space Administration Serrated-planform lifting-surfaces
US6095459A (en) * 1997-06-16 2000-08-01 Codina; George Method and apparatus for countering asymmetrical aerodynamic process subjected onto multi engine aircraft
US6138955A (en) * 1998-12-23 2000-10-31 Board Of Supervisors Of Louisiana State University And Agricultural And Mechanical College Vortical lift control over a highly swept wing
GB0514338D0 (en) * 2005-07-13 2005-08-17 Univ City Control of fluid flow separation
GB2466478A (en) * 2008-12-02 2010-06-30 Aerovortex Mills Ltd Suction generation device
US8292220B1 (en) * 2009-03-19 2012-10-23 Northrop Grumman Corporation Flying wing aircraft with modular missionized elements

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA595877A (en) * 1960-04-12 G. Gould Donald Vortex generator
US2125738A (en) * 1936-12-17 1938-08-02 William K Rose Airfoil
US2163655A (en) * 1938-04-02 1939-06-27 Charles H Zimmerman Slotted airplane wing tip
US2885161A (en) * 1948-08-11 1959-05-05 Douglas Aircraft Co Inc Stability control device for aircraft
GB890418A (en) * 1958-11-18 1962-02-28 Secr Aviation Lateral control means for aeroplanes
GB1012270A (en) * 1962-08-29 1965-12-08 Power Jets Res & Dev Ltd Aircraft
US3188022A (en) * 1963-12-05 1965-06-08 Svenska Aeroplan Ab Delta wing canard aircraft

Also Published As

Publication number Publication date
CH470287A (de) 1969-03-31
FR1511212A (fr) 1968-01-26
AT280059B (de) 1970-03-25
GB1179568A (en) 1970-01-28
US3471107A (en) 1969-10-07

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