SE331952B - - Google Patents

Info

Publication number
SE331952B
SE331952B SE17700/67A SE1770067A SE331952B SE 331952 B SE331952 B SE 331952B SE 17700/67 A SE17700/67 A SE 17700/67A SE 1770067 A SE1770067 A SE 1770067A SE 331952 B SE331952 B SE 331952B
Authority
SE
Sweden
Application number
SE17700/67A
Inventor
A Ingelman-Sundberg
Original Assignee
Ingelman Sundberg A
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 Ingelman Sundberg A filed Critical Ingelman Sundberg A
Priority to SE17700/67A priority Critical patent/SE331952B/xx
Priority to US784424A priority patent/US3586267A/en
Publication of SE331952B publication Critical patent/SE331952B/xx

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/32Air braking surfaces
SE17700/67A 1967-12-22 1967-12-22 SE331952B (zh)

Priority Applications (2)

Application Number Priority Date Filing Date Title
SE17700/67A SE331952B (zh) 1967-12-22 1967-12-22
US784424A US3586267A (en) 1967-12-22 1968-12-17 Arrangement in and relating to aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE17700/67A SE331952B (zh) 1967-12-22 1967-12-22

Publications (1)

Publication Number Publication Date
SE331952B true SE331952B (zh) 1971-01-18

Family

ID=20303878

Family Applications (1)

Application Number Title Priority Date Filing Date
SE17700/67A SE331952B (zh) 1967-12-22 1967-12-22

Country Status (2)

Country Link
US (1) US3586267A (zh)
SE (1) SE331952B (zh)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2188367B1 (zh) * 1972-06-01 1980-03-21 Ibm France
US3952601A (en) * 1974-12-18 1976-04-27 United Technologies Corporation Helicopter rotor blade balancing method
US5211358A (en) * 1991-05-13 1993-05-18 General Dynamics Corporation Airfoil deployment system for missile or aircraft
US5326050A (en) * 1993-02-08 1994-07-05 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Aerodynamic surface distension system for high angle of attack forebody vortex control
US5755408A (en) * 1995-04-03 1998-05-26 Schmidt; Robert N. Fluid flow control devices
US6048581A (en) 1996-09-24 2000-04-11 Mcdonnell Douglas Corporation Elastic ground plane and method
US6209824B1 (en) 1997-09-17 2001-04-03 The Boeing Company Control surface for an aircraft
US6015115A (en) * 1998-03-25 2000-01-18 Lockheed Martin Corporation Inflatable structures to control aircraft
US6105904A (en) * 1998-03-30 2000-08-22 Orbital Research Inc. Deployable flow control device
US6098925A (en) * 1999-08-10 2000-08-08 Northrop Grumman Corporation Adaptive deployable ramp for suppression of aircraft weapons bay acoustic loads
US7143983B2 (en) * 2002-08-28 2006-12-05 Lockheed Martin Corporation Passive jet spoiler for yaw control of an aircraft
US6685143B1 (en) * 2003-01-03 2004-02-03 Orbital Research Inc. Aircraft and missile forebody flow control device and method of controlling flow
US6843452B1 (en) * 2003-06-17 2005-01-18 The Boeing Company Variable trailing edge geometry and spanload control
ES2326352B1 (es) * 2007-09-14 2010-07-15 GAMESA INNOVATION & TECHNOLOGY, S.L. Pala de aerogenerador con alerones deflectables controlados por cambios de la presion en la superficie.
US8152109B2 (en) * 2007-11-29 2012-04-10 Silich Bert A Method and system for controlling fluid flow in relation to a foil and harnessing energy therefrom
GB0810724D0 (en) * 2008-06-12 2008-07-16 Airbus Uk Ltd Slat assembly
US8870125B2 (en) * 2011-07-21 2014-10-28 The Boeing Company Trailing edge split flap with pneumatic actuation
US9359065B2 (en) * 2013-09-24 2016-06-07 The Boeing Company System and method for optimizing performance of an aircraft
GB201409424D0 (en) * 2014-05-28 2014-07-09 Agustawestland Ltd Device which is subject to fluid flow
DE202015000665U1 (de) * 2015-01-24 2015-06-26 Dieter Röhm Vorrichtung eines Sicherheitssystems und/oder Ressourcen-/Energieeffizienz-Verbesserungs - Systems zur Stömungsbeeinflussung eines Aero- oder Hydrodynamischen Körpers (3), nach dem Prinzip einer Rückstromklappe (4)
US10106246B2 (en) 2016-06-10 2018-10-23 Coflow Jet, LLC Fluid systems that include a co-flow jet
US10315754B2 (en) 2016-06-10 2019-06-11 Coflow Jet, LLC Fluid systems that include a co-flow jet
EP3348471B1 (en) * 2017-01-17 2019-09-04 Airbus Operations, S.L. Lifting surface
US10683076B2 (en) 2017-10-31 2020-06-16 Coflow Jet, LLC Fluid systems that include a co-flow jet
CN108298062B (zh) * 2018-01-15 2021-03-12 上海理工大学 可自动约束的自适应襟翼
US11293293B2 (en) 2018-01-22 2022-04-05 Coflow Jet, LLC Turbomachines that include a casing treatment
US11111025B2 (en) 2018-06-22 2021-09-07 Coflow Jet, LLC Fluid systems that prevent the formation of ice
EP3667072A1 (en) * 2018-12-13 2020-06-17 Siemens Gamesa Renewable Energy A/S Adaptable spoiler for a wind turbine blade
EP3667061A1 (en) * 2018-12-13 2020-06-17 Siemens Gamesa Renewable Energy A/S Adaptable spoiler for a wind turbine rotor blade
GB2600584B (en) 2019-07-23 2024-03-06 Coflow Jet Llc Fluid systems and methods that address flow separation

Also Published As

Publication number Publication date
US3586267A (en) 1971-06-22

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