FR1103426A - Perfectionnements apportés aux voilures d'aérodynes - Google Patents
Perfectionnements apportés aux voilures d'aérodynesInfo
- Publication number
- FR1103426A FR1103426A FR1103426DA FR1103426A FR 1103426 A FR1103426 A FR 1103426A FR 1103426D A FR1103426D A FR 1103426DA FR 1103426 A FR1103426 A FR 1103426A
- Authority
- FR
- France
- Prior art keywords
- aerodyne
- wings
- improvements made
- aerodyne wings
- Prior art date
- 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
Links
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
- B64C21/025—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for simultaneous blowing and sucking
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1103426T | 1954-02-26 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1103426A true FR1103426A (fr) | 1955-11-03 |
Family
ID=9622204
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1103426D Expired FR1103426A (fr) | 1954-02-26 | 1954-02-26 | Perfectionnements apportés aux voilures d'aérodynes |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1103426A (fr) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2928627A (en) * | 1956-07-10 | 1960-03-15 | Lockheed Aircraft Corp | Aircraft propulsion systems |
DE1091873B (de) * | 1955-12-29 | 1960-10-27 | Robert Pouit | Flugzeug mit Rueckstossantrieb durch mindestens zwei Strahlturbinen |
DE1139028B (de) * | 1959-11-02 | 1962-10-31 | Gen Electric | Einrichtung zum Ablenken einer aus einem Kanal austretenden Stroemung |
US3069115A (en) * | 1958-10-08 | 1962-12-18 | Bristol Aircraft Ltd | Aircraft |
DE1198145B (de) * | 1958-08-01 | 1965-08-05 | Firth Cleveland Ltd | Stroemungskoerper, insbesondere Quertriebsflaeche, mit durch Ausblasen von Stroemungsmittelstrahlen beeinflussbarer Zirkulation |
DE1216117B (de) * | 1961-03-09 | 1966-05-05 | Hawker Siddeley Aviation Ltd | Flugzeug mit schwenkbaren Axialgeblaesen am Tragfluegel |
DE1218885B (de) * | 1962-08-29 | 1966-06-08 | Alan John Alexander | Flugzeug mit stark gepfeilten Tragflaechen, aus deren Vorderkante ein flacher Gasstrahl ausgeblasen wird |
US4117995A (en) * | 1977-02-28 | 1978-10-03 | Runge Thomas M | Aircraft wing lift augmentation device |
US4752049A (en) * | 1985-12-30 | 1988-06-21 | The Boeing Company | Leading edge slat/anti-icing system and method for airfoil |
-
1954
- 1954-02-26 FR FR1103426D patent/FR1103426A/fr not_active Expired
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1091873B (de) * | 1955-12-29 | 1960-10-27 | Robert Pouit | Flugzeug mit Rueckstossantrieb durch mindestens zwei Strahlturbinen |
US2928627A (en) * | 1956-07-10 | 1960-03-15 | Lockheed Aircraft Corp | Aircraft propulsion systems |
DE1198145B (de) * | 1958-08-01 | 1965-08-05 | Firth Cleveland Ltd | Stroemungskoerper, insbesondere Quertriebsflaeche, mit durch Ausblasen von Stroemungsmittelstrahlen beeinflussbarer Zirkulation |
US3069115A (en) * | 1958-10-08 | 1962-12-18 | Bristol Aircraft Ltd | Aircraft |
DE1139028B (de) * | 1959-11-02 | 1962-10-31 | Gen Electric | Einrichtung zum Ablenken einer aus einem Kanal austretenden Stroemung |
DE1216117B (de) * | 1961-03-09 | 1966-05-05 | Hawker Siddeley Aviation Ltd | Flugzeug mit schwenkbaren Axialgeblaesen am Tragfluegel |
DE1218885B (de) * | 1962-08-29 | 1966-06-08 | Alan John Alexander | Flugzeug mit stark gepfeilten Tragflaechen, aus deren Vorderkante ein flacher Gasstrahl ausgeblasen wird |
US4117995A (en) * | 1977-02-28 | 1978-10-03 | Runge Thomas M | Aircraft wing lift augmentation device |
US4752049A (en) * | 1985-12-30 | 1988-06-21 | The Boeing Company | Leading edge slat/anti-icing system and method for airfoil |
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