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
Links
- 230000001154 acute effect Effects 0.000 abstract 2
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)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE16332/66A SE313504B (xx) | 1966-11-29 | 1966-11-29 | |
DE1531460A DE1531460C3 (de) | 1966-11-29 | 1967-11-27 | Flugzeugtragflugel |
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 |
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 (xx) | 1966-11-29 | 1966-11-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
SE313504B true SE313504B (xx) | 1969-08-11 |
Family
ID=20302080
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE16332/66A SE313504B (xx) | 1966-11-29 | 1966-11-29 |
Country Status (4)
Country | Link |
---|---|
US (1) | US3478988A (xx) |
DE (1) | DE1531460C3 (xx) |
GB (1) | GB1212705A (xx) |
SE (1) | SE313504B (xx) |
Families Citing this family (27)
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 |
USRE32907E (en) * | 1981-09-28 | 1989-04-18 | The Boeing Company | Airfoil flap assembly with flap track member |
US4434959A (en) | 1981-09-28 | 1984-03-06 | 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 |
WO2012040446A1 (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*** |
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)
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 |
-
1966
- 1966-11-29 SE SE16332/66A patent/SE313504B/xx unknown
-
1967
- 1967-11-27 DE DE1531460A patent/DE1531460C3/de not_active Expired
- 1967-11-28 GB GB54071/67A patent/GB1212705A/en not_active Expired
- 1967-11-28 US US686225A patent/US3478988A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE1531460A1 (de) | 1972-03-30 |
GB1212705A (en) | 1970-11-18 |
DE1531460B2 (de) | 1973-03-01 |
DE1531460C3 (de) | 1973-09-20 |
US3478988A (en) | 1969-11-18 |
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