SE313504B - - Google Patents

Info

Publication number
SE313504B
SE313504B SE16332/66A SE1633266A SE313504B SE 313504 B SE313504 B SE 313504B SE 16332/66 A SE16332/66 A SE 16332/66A SE 1633266 A SE1633266 A SE 1633266A SE 313504 B SE313504 B SE 313504B
Authority
SE
Sweden
Prior art keywords
flap
wing
flaps
slot
forms
Prior art date
Application number
SE16332/66A
Other languages
English (en)
Inventor
A Roeed
J Ertzgaard
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 SE16332/66A priority Critical patent/SE313504B/xx
Priority to FR129863A priority patent/FR1546878A/fr
Priority to DE1531460A priority patent/DE1531460C3/de
Priority to GB54071/67A priority patent/GB1212705A/en
Priority to US686225A priority patent/US3478988A/en
Publication of SE313504B publication Critical patent/SE313504B/xx

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B64C29/005—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors the motors being fixed relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42—Arrangement or adaptation of brakes
    • B64C25/423—Braking devices acting by reaction of gaseous medium
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/58—Wings provided with fences or spoilers
    • 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
    • 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
    • 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
    • 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
    • Y02T50/30—Wing lift efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Control Of Turbines (AREA)
  • Toys (AREA)
SE16332/66A 1966-11-29 1966-11-29 SE313504B (pt)

Priority Applications (5)

Application Number Priority Date Filing Date Title
SE16332/66A SE313504B (pt) 1966-11-29 1966-11-29
FR129863A FR1546878A (fr) 1966-11-29 1967-11-27 Dispositif pour régler la portance d'un avion pendant l'approche et pour inverser la poussée des réacteurs pendant le roulage au sol
DE1531460A DE1531460C3 (de) 1966-11-29 1967-11-27 Flugzeugtragflugel
GB54071/67A GB1212705A (en) 1966-11-29 1967-11-28 An aircraft
US686225A US3478988A (en) 1966-11-29 1967-11-28 Stol aircraft having by-pass turbojet engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE16332/66A SE313504B (pt) 1966-11-29 1966-11-29

Publications (1)

Publication Number Publication Date
SE313504B true SE313504B (pt) 1969-08-11

Family

ID=20302080

Family Applications (1)

Application Number Title Priority Date Filing Date
SE16332/66A SE313504B (pt) 1966-11-29 1966-11-29

Country Status (4)

Country Link
US (1) US3478988A (pt)
DE (1) DE1531460C3 (pt)
GB (1) GB1212705A (pt)
SE (1) SE313504B (pt)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3614028A (en) * 1970-01-12 1971-10-19 Mc Donnell Douglas Corp Turbofan-powered stol aircraft
US3666209A (en) * 1970-02-24 1972-05-30 Boeing Co V/stol aircraft with variable tilt wing
US3830451A (en) * 1973-06-28 1974-08-20 Rockwell International Corp Aircraft control system
US3884433A (en) * 1973-10-11 1975-05-20 Boeing Co Wing mounted thrust reverser
US4074878A (en) * 1975-06-23 1978-02-21 Sherman Irving R Programmed flap system for an aircraft having wings
US4131252A (en) * 1976-06-15 1978-12-26 The Boeing Company Apparatus for compensating for airflow blockage in aircraft slotted flap assemblies
US4252286A (en) * 1979-04-16 1981-02-24 The Boeing Company Simplified core flow thrust control device
DE2924742C2 (de) * 1979-06-20 1983-12-08 Dornier Gmbh, 7990 Friedrichshafen Großflugzeug, insbesondere in Schulterdeckerbauart
GB2089745B (en) * 1980-12-20 1984-09-05 Rolls Royce Thrust deflector
US4434959A (en) 1981-09-28 1984-03-06 The Boeing Company Airfoil flap assembly with flap track member
USRE32907E (en) * 1981-09-28 1989-04-18 The Boeing Company Airfoil flap assembly with flap track member
DE3175717D1 (en) * 1981-12-16 1987-01-29 Boeing Co Flap assembly aircraft wing
US4610410A (en) * 1983-07-22 1986-09-09 Rolls-Royce Limited Compound helicopter and powerplant therefor
US4784355A (en) * 1986-11-10 1988-11-15 The United States Of America As Represented By The Secretary Of The Air Force Flap system for short takeoff and landing aircraft
US5178348A (en) * 1992-02-05 1993-01-12 The Boeing Company Contoured wing/flap assembly and method
US6079672A (en) * 1997-12-18 2000-06-27 Lam; Lawrence Y. Aileron for fixed wing aircraft
US20050242234A1 (en) * 2004-04-29 2005-11-03 The Boeing Company Lifters, methods of flight control and maneuver load alleviation
ES2277716B1 (es) * 2004-12-31 2008-05-16 Airbus España, S.L. Tapa reforzada para ranuras en un contorno aerodinamico.
ES2277715B1 (es) * 2004-12-31 2008-05-16 Airbus España, S.L. Tapa reforzada para escotaduras en un contorno aerodinamico.
US20070290098A1 (en) * 2006-06-15 2007-12-20 Novak Charlie Airfoil having a movable control surface
FR2930235B1 (fr) * 2008-04-21 2011-09-30 Airbus France Mat de suspension pour turbomoteur.
DK200800723A (en) * 2008-05-27 2009-11-28 Fo900 Invest Aps Wind turbine blade with aerodynamic slit near the root
US20120074264A1 (en) * 2010-09-24 2012-03-29 Heaton Clifford D Airplane wing
US10538312B2 (en) * 2012-03-16 2020-01-21 Liebherr-Aerospace Lindenberg Gmbh Operating an aircraft with improved aileron and landing function
CN104691745B (zh) * 2014-07-04 2016-12-07 贵州贵航飞机设计研究所 薄翼型下使用一个作动筒完成双缝襟翼运动的方法及装置
CN112193424A (zh) * 2020-10-19 2021-01-08 中南大学 一种基于非常规布局的外吹式动力增升系统
US11305869B1 (en) 2020-12-23 2022-04-19 Wayfarer Aircraft Research And Development Inc. Systems and methods for aircraft lift enhancement

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3089672A (en) * 1961-05-15 1963-05-14 Andrew P Huchala Undercarriage safeguard system
US3154267A (en) * 1962-03-13 1964-10-27 Charles H Grant Controlled temperature flow around airfoils

Also Published As

Publication number Publication date
US3478988A (en) 1969-11-18
DE1531460C3 (de) 1973-09-20
GB1212705A (en) 1970-11-18
DE1531460A1 (de) 1972-03-30
DE1531460B2 (de) 1973-03-01

Similar Documents

Publication Publication Date Title
GB1212705A (en) An aircraft
US2928238A (en) Jet deflector and orifice control
US3920203A (en) Thrust control apparatus for obtaining maximum thrust reversal in minimum time upon landing of an aircraft
US4019696A (en) Method of and apparatus for enhancing Coanda flow attachment over a wing and flap surface
US4161300A (en) Canard type aircraft
US2941751A (en) Spoiler for aircraft wings
US3863867A (en) Thrust control apparatus for a jet propulsion engine and actuating mechanism therefor
US4463772A (en) Flush inlet for supersonic aircraft
US3971534A (en) Method of and apparatus for controlling flow attachment to the wing and flap surfaces of an upper surface blowing type aircraft
US2734698A (en) Aikplane control surface and jet
JPH037098U (pt)
US3128966A (en) Alvarez-calderon
US3926389A (en) Aircraft of a controllable stability
US3977630A (en) STOL aircraft
US2344945A (en) Means for providing drag in aircraft
US4979699A (en) Flight control augmentation inlet device
US2568812A (en) Aircraft control means
US4003533A (en) Combination airbrake and pitch control device
US3848831A (en) Fuselage flaps for an aircraft
US2738147A (en) Means for turning and braking jet propelled aircraft
US4387869A (en) Mono-element combined supercritical high lift airfoil
US2276522A (en) Wing system for airplanes
US2961192A (en) Jet propelled aircraft
GB1381646A (en) Aircraft with short take-off and landing characteristics
GB2051706A (en) Aircraft wings