FR61015E - - Google Patents

Info

Publication number
FR61015E
FR61015E FR61015DA FR61015E FR 61015 E FR61015 E FR 61015E FR 61015D A FR61015D A FR 61015DA FR 61015 E FR61015 E FR 61015E
Authority
FR
France
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
French (fr)
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.)
Publication date
Application granted granted Critical
Publication of FR61015E publication Critical patent/FR61015E/fr
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
    • B64C9/146—Adjustable control surfaces or members, e.g. rudders forming slots at an other wing location than the rear or the front
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • 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
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/20—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by multiple flaps
    • 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
    • B64C2230/00—Boundary layer controls
    • B64C2230/04—Boundary layer controls by actively generating fluid flow
    • 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
    • B64C2230/16—Boundary layer controls by blowing other fluids over the surface than air, e.g. He, H, O2 or exhaust gases
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR61015D 1946-12-03 Expired FR61015E (zh)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
FR937234T 1946-12-03
FR57988T 1948-02-03
FR58273T 1948-02-21
FR58474T 1948-05-18

Publications (1)

Publication Number Publication Date
FR61015E true FR61015E (zh) 1955-03-23

Family

ID=62222341

Family Applications (5)

Application Number Title Priority Date Filing Date
FR61015D Expired FR61015E (zh) 1946-12-03
FR937234D Expired FR937234A (fr) 1946-12-03 1946-12-03 Perfectionnements apportés à l'hypersustentateur des engins de navigation aérienne
FR57988D Expired FR57988E (fr) 1946-12-03 1948-02-03 Perfectionnements apportés à l'hypersustentateur des engins de navigation aérienne
FR58273D Expired FR58273E (fr) 1946-12-03 1948-02-21 Perfectionnements apportés à l'hypersustentateur des engins de navigation aérienne
FR58474D Expired FR58474E (fr) 1946-12-03 1948-05-18 Perfectionnements apportés à l'hypersustentateur des engins de navigation aérienne

Family Applications After (4)

Application Number Title Priority Date Filing Date
FR937234D Expired FR937234A (fr) 1946-12-03 1946-12-03 Perfectionnements apportés à l'hypersustentateur des engins de navigation aérienne
FR57988D Expired FR57988E (fr) 1946-12-03 1948-02-03 Perfectionnements apportés à l'hypersustentateur des engins de navigation aérienne
FR58273D Expired FR58273E (fr) 1946-12-03 1948-02-21 Perfectionnements apportés à l'hypersustentateur des engins de navigation aérienne
FR58474D Expired FR58474E (fr) 1946-12-03 1948-05-18 Perfectionnements apportés à l'hypersustentateur des engins de navigation aérienne

Country Status (1)

Country Link
FR (5) FR937234A (zh)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3246335A (en) * 1964-01-15 1966-04-12 Alvarez-Calderon Alberto Double slotted flap
EP3088300A1 (en) * 2015-04-28 2016-11-02 The Boeing Company Aerodynamic surface assembly

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1013968B (de) * 1954-05-03 1957-08-14 Edward Munroe Lanier Tragflaeche fuer Flugzeuge mit mindestens einem sich von der Tragflaechenunterseite zur Oberseite erstreckenden Staukanal
DE1179809B (de) * 1959-01-24 1964-10-15 Josef Ksoll Quertriebsflaeche, insbesondere Flugzeugtragfluegel, mit einem Vorfluegel
IT1067613B (it) * 1976-08-09 1985-03-16 Bizzarri Alfredo Sistema di aspirazione e di spinta applicabile per sostentamento e propulsione di aeromobili per spinta e frenata di veicioli ter restri e navali e per altre applicazioni
EP0932548B1 (en) 1996-10-22 2003-01-22 The Boeing Company Airplane with unswept slotted cruise wing airfoil
WO2001074660A1 (en) * 2000-04-03 2001-10-11 Parish Overton L Iv Vane-airfoil combination
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
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7494094B2 (en) 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
US7264206B2 (en) 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
US7322547B2 (en) * 2005-01-31 2008-01-29 The Boeing Company Aerospace vehicle leading edge slat devices and corresponding methods
US7338018B2 (en) 2005-02-04 2008-03-04 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
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
US7475854B2 (en) 2005-11-21 2009-01-13 The Boeing Company Aircraft trailing edge devices, including devices with non-parallel motion paths, 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
CN110072773B (zh) * 2016-12-12 2022-10-21 庞巴迪公司 飞机缝翼

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3246335A (en) * 1964-01-15 1966-04-12 Alvarez-Calderon Alberto Double slotted flap
EP3088300A1 (en) * 2015-04-28 2016-11-02 The Boeing Company Aerodynamic surface assembly
US10507906B2 (en) 2015-04-28 2019-12-17 The Boeing Company Aerodynamic surface assembly defining a fluidic actuation orifice
AU2016201107B2 (en) * 2015-04-28 2020-03-19 The Boeing Company Aerodynamic surface assembly defining a fluidic actuation orifice

Also Published As

Publication number Publication date
FR58273E (fr) 1953-11-18
FR58474E (fr) 1953-11-30
FR57988E (fr) 1953-09-18
FR937234A (fr) 1948-08-11

Similar Documents

Publication Publication Date Title
FR954564A (zh)
BE463006A (zh)
FR61015E (zh)
AT165703B (zh)
AT189954B (zh)
BE472705A (zh)
BE375336A (zh)
BE464077A (zh)
BE464863A (zh)
BE463580A (zh)
BE463324A (zh)
BE463154A (zh)
BE463045A (zh)
BE462695A (zh)
SE120663C1 (zh)
NL94984C (zh)
NL63183C (zh)
NL60831C (zh)
BE463719A (zh)
BE479289A (zh)
BE478152A (zh)
BE477023A (zh)
BE473866A (zh)
BE464883A (zh)
BE464875A (zh)