SE397506B - SLOT-FITTED SPOILER FOR AN AIRCRAFT WING - Google Patents
SLOT-FITTED SPOILER FOR AN AIRCRAFT WINGInfo
- Publication number
- SE397506B SE397506B SE7215264A SE1526472A SE397506B SE 397506 B SE397506 B SE 397506B SE 7215264 A SE7215264 A SE 7215264A SE 1526472 A SE1526472 A SE 1526472A SE 397506 B SE397506 B SE 397506B
- Authority
- SE
- Sweden
- Prior art keywords
- slot
- wing
- spoiler
- aircraft wing
- fitted
- Prior art date
Links
- 238000000926 separation method Methods 0.000 abstract 1
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
- 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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
- Toys (AREA)
- Air-Flow Control Members (AREA)
Abstract
1404153 Aircraft wing MITSUBISHI JUKOGYO KK 22 Nov 1972 [24 Nov 1971] 54098/72 Heading B7G [Also in Division F2] An aircraft wing 1 is provided with a spoiler 2 located in a slot 4 through the wing and mounted at 5 for upward pivoting, and means located in the slot for causing vortices 10 in air flowing from the underside of the wing through the slot when the spoiler 2 is raised. Such means may be a sawtooth edged plate 7 or a plurality of rods (8), Figs. 9-12 (not shown), and may be located on the trailing edge of the spoiler 2 or on the wing 1 to the rear of the slot 4, Figs. 13, 14 (not shown). The wing has a trailing edge flap 3, and the effect of the vortexproducing means is to delay boundary-layer separation when the flap is deployed.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP46093591A JPS5211520B2 (en) | 1971-11-24 | 1971-11-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
SE397506B true SE397506B (en) | 1977-11-07 |
Family
ID=14086525
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE7215264A SE397506B (en) | 1971-11-24 | 1972-11-23 | SLOT-FITTED SPOILER FOR AN AIRCRAFT WING |
Country Status (5)
Country | Link |
---|---|
JP (1) | JPS5211520B2 (en) |
DE (1) | DE2253877C3 (en) |
FR (1) | FR2160854B1 (en) |
GB (1) | GB1404153A (en) |
SE (1) | SE397506B (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5131498A (en) * | 1974-09-10 | 1976-03-17 | Kawasaki Heavy Ind Ltd | Hikikomikanona borutetsukusujenereeta |
DE2855016C2 (en) * | 1978-12-20 | 1984-05-03 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Flap arrangement for aircraft |
DE3521329A1 (en) * | 1985-06-14 | 1986-12-18 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Vortex generator and boundary layer deflector arrangement |
US5294080A (en) * | 1993-02-08 | 1994-03-15 | The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration | Lift enhancing tabs for airfoils |
JP4699487B2 (en) * | 2007-05-25 | 2011-06-08 | 三菱重工業株式会社 | Noise reduction structure of high lift generator, wing and high lift generator |
GB0810500D0 (en) | 2008-06-09 | 2008-07-09 | Airbus Uk Ltd | Aircraft wing |
RU2524289C1 (en) * | 2013-02-19 | 2014-07-27 | Юлия Алексеевна Щепочкина | Railway car |
US9193436B2 (en) | 2013-07-03 | 2015-11-24 | The Boeing Company | Flow control structure and associated method for controlling attachment with a control surface |
CN114408158B (en) * | 2022-03-03 | 2024-02-02 | 中国商用飞机有限责任公司 | Turbulent flow device and operation method thereof |
-
1971
- 1971-11-24 JP JP46093591A patent/JPS5211520B2/ja not_active Expired
-
1972
- 1972-11-03 DE DE2253877A patent/DE2253877C3/en not_active Expired
- 1972-11-14 FR FR7240320A patent/FR2160854B1/fr not_active Expired
- 1972-11-22 GB GB5409872A patent/GB1404153A/en not_active Expired
- 1972-11-23 SE SE7215264A patent/SE397506B/en unknown
Also Published As
Publication number | Publication date |
---|---|
DE2253877C3 (en) | 1975-10-16 |
FR2160854B1 (en) | 1977-08-05 |
GB1404153A (en) | 1975-08-28 |
JPS5211520B2 (en) | 1977-03-31 |
FR2160854A1 (en) | 1973-07-06 |
DE2253877A1 (en) | 1973-06-07 |
JPS4858600A (en) | 1973-08-16 |
DE2253877B2 (en) | 1975-03-06 |
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