FR1311826A - Aircraft upgrades - Google Patents
Aircraft upgradesInfo
- Publication number
- FR1311826A FR1311826A FR869951A FR869951A FR1311826A FR 1311826 A FR1311826 A FR 1311826A FR 869951 A FR869951 A FR 869951A FR 869951 A FR869951 A FR 869951A FR 1311826 A FR1311826 A FR 1311826A
- Authority
- FR
- France
- Prior art keywords
- upgrades
- aircraft
- aircraft upgrades
- 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
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
-
- 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
- B64C21/06—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for 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
-
- 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)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR869951A FR1311826A (en) | 1961-08-03 | 1961-08-03 | Aircraft upgrades |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR869951A FR1311826A (en) | 1961-08-03 | 1961-08-03 | Aircraft upgrades |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1311826A true FR1311826A (en) | 1962-12-14 |
Family
ID=8760682
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR869951A Expired FR1311826A (en) | 1961-08-03 | 1961-08-03 | Aircraft upgrades |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1311826A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0436243A2 (en) * | 1989-12-29 | 1991-07-10 | The Boeing Company | Anti-icing system for aircraft |
FR3073202A1 (en) * | 2017-11-09 | 2019-05-10 | Airbus Operations | Wing comprising a leading edge slat and having means for preventing the transition to a turbulent boundary layer |
-
1961
- 1961-08-03 FR FR869951A patent/FR1311826A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0436243A2 (en) * | 1989-12-29 | 1991-07-10 | The Boeing Company | Anti-icing system for aircraft |
EP0436243A3 (en) * | 1989-12-29 | 1991-08-07 | The Boeing Company | Anti-icing system for aircraft |
FR3073202A1 (en) * | 2017-11-09 | 2019-05-10 | Airbus Operations | Wing comprising a leading edge slat and having means for preventing the transition to a turbulent boundary layer |
EP3483060A1 (en) * | 2017-11-09 | 2019-05-15 | Airbus Operations S.A.S. | Wing with a leading edge spout and means for preventing the passage to a turbulent boundary layer |
US11027820B2 (en) | 2017-11-09 | 2021-06-08 | Airbus Operations Sas | Wing comprising a leading edge slat and having means for preventing the transition to a turbulent boundary layer |
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