FR56121E - Perfectionnement aux avions à ailes à fente hypersustentatrice - Google Patents

Perfectionnement aux avions à ailes à fente hypersustentatrice

Info

Publication number
FR56121E
FR56121E FR56121DA FR56121E FR 56121 E FR56121 E FR 56121E FR 56121D A FR56121D A FR 56121DA FR 56121 E FR56121 E FR 56121E
Authority
FR
France
Prior art keywords
development
wing planes
lift slit
slit wing
lift
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.)
Expired
Application number
Other languages
English (en)
Inventor
Max-Louis Holste
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 filed Critical
Application granted granted Critical
Publication of FR56121E publication Critical patent/FR56121E/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/06—Boundary layer controls by explicitly adjusting fluid flow, e.g. by using valves, variable aperture or slot areas, variable pump action or variable fluid pressure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/20—Boundary layer controls by passively inducing fluid flow, e.g. by means of a pressure difference between both ends of a slot or duct
    • 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
FR56121D 1942-12-29 1944-03-15 Perfectionnement aux avions à ailes à fente hypersustentatrice Expired FR56121E (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR978969T 1942-12-29
FR56121T 1944-03-15

Publications (1)

Publication Number Publication Date
FR56121E true FR56121E (fr) 1952-09-17

Family

ID=62222339

Family Applications (2)

Application Number Title Priority Date Filing Date
FR978969D Expired FR978969A (fr) 1942-12-29 1942-12-29 Perfectionnement aux avions à ailes à fente hypersustentatrice
FR56121D Expired FR56121E (fr) 1942-12-29 1944-03-15 Perfectionnement aux avions à ailes à fente hypersustentatrice

Family Applications Before (1)

Application Number Title Priority Date Filing Date
FR978969D Expired FR978969A (fr) 1942-12-29 1942-12-29 Perfectionnement aux avions à ailes à fente hypersustentatrice

Country Status (1)

Country Link
FR (2) FR978969A (fr)

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4726547A (en) * 1985-11-06 1988-02-23 Dornier Gmbh Helicopter with high forward speed
WO2006083547A1 (fr) * 2005-01-31 2006-08-10 The Boeing Company Dispositifs de bec de bord d'attaque pour vehicule aerospatial et procedes correspondants
US7258308B2 (en) 2002-07-02 2007-08-21 The Boeing Company Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface
US7708231B2 (en) 2005-11-21 2010-05-04 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
US7721999B2 (en) 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7726610B2 (en) 2004-09-08 2010-06-01 The Boeing Company Systems and methods for providing differential motion to wing high lift device
US7744040B2 (en) 2005-11-21 2010-06-29 The Boeing Company Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
US7766282B2 (en) 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
US7828250B2 (en) 2004-09-30 2010-11-09 The Boeing Company Leading edge flap apparatuses and associated methods
US7891611B2 (en) 2005-02-04 2011-02-22 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7913955B2 (en) 2003-11-24 2011-03-29 The Boeing Company Aircraft control surface drive system and associated methods
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
USRE44313E1 (en) 1996-10-22 2013-06-25 The Boeing Company Airplane with unswept slotted cruise wing airfoil
US20130313355A1 (en) * 2012-05-22 2013-11-28 Eurocopter Pitching stabilization means and a rotary wing aircraft including such means
US20170137123A1 (en) * 2015-11-17 2017-05-18 Charl E. Janeke System, Apparatus and Methods for an Airspace Plane with Shockwave Piercing Wings

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3575363A (en) * 1969-08-28 1971-04-20 Mc Donnell Douglas Corp Horizontal tail for aircraft
DE3568970D1 (en) * 1984-09-28 1989-04-27 Henri Aubertin Conception of a twin engine ulm
FR2575722B2 (fr) * 1985-01-04 1989-03-03 Aubertin Henri Dispositif hyper-sustentateur pour avion leger
GB201101274D0 (en) * 2011-01-25 2011-03-09 Airbus Operations Ltd Leading edge device for an aircraft

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4726547A (en) * 1985-11-06 1988-02-23 Dornier Gmbh Helicopter with high forward speed
USRE44313E1 (en) 1996-10-22 2013-06-25 The Boeing Company Airplane with unswept slotted cruise wing airfoil
US7258308B2 (en) 2002-07-02 2007-08-21 The Boeing Company Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface
US7913955B2 (en) 2003-11-24 2011-03-29 The Boeing Company Aircraft control surface drive system and associated methods
US7726610B2 (en) 2004-09-08 2010-06-01 The Boeing Company Systems and methods for providing differential motion to wing high lift device
US7828250B2 (en) 2004-09-30 2010-11-09 The Boeing Company Leading edge flap apparatuses and associated methods
WO2006083547A1 (fr) * 2005-01-31 2006-08-10 The Boeing Company Dispositifs de bec de bord d'attaque pour vehicule aerospatial et procedes correspondants
US7891611B2 (en) 2005-02-04 2011-02-22 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7721999B2 (en) 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7744040B2 (en) 2005-11-21 2010-06-29 The Boeing Company Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
US7708231B2 (en) 2005-11-21 2010-05-04 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
US8567726B2 (en) 2005-11-21 2013-10-29 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
US20130313355A1 (en) * 2012-05-22 2013-11-28 Eurocopter Pitching stabilization means and a rotary wing aircraft including such means
US9302762B2 (en) * 2012-05-22 2016-04-05 Airbus Helicopters Pitching stabilization means and a rotary wing aircraft including such means
US20170137123A1 (en) * 2015-11-17 2017-05-18 Charl E. Janeke System, Apparatus and Methods for an Airspace Plane with Shockwave Piercing Wings

Also Published As

Publication number Publication date
FR978969A (fr) 1951-04-20

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