GB568667A - Improvements in and relating to aircraft - Google Patents
Improvements in and relating to aircraftInfo
- Publication number
- GB568667A GB568667A GB17352/42A GB1735242A GB568667A GB 568667 A GB568667 A GB 568667A GB 17352/42 A GB17352/42 A GB 17352/42A GB 1735242 A GB1735242 A GB 1735242A GB 568667 A GB568667 A GB 568667A
- Authority
- GB
- United Kingdom
- Prior art keywords
- conduits
- aircraft
- wings
- upper surfaces
- air sucked
- 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
- 238000006243 chemical reaction Methods 0.000 abstract 1
- 238000002485 combustion reaction 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
- B64C21/01—Boundary layer ingestion [BLI] propulsion
-
- 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
-
- 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
Abstract
568,667. Reducing surface friction on aircraft. UMPLEBY, F. Dec. 7, 1942, No. 17352. [Class 4] Air sucked through openings in the upper surfaces of an aircraft fuselage and wings in order to control the boundary layer is fed to the aero-engine or to a jet propulsion device, the conduits being so arranged that a forward reaction due to the airflow around bends in the conduits is obtained. As shown, air sucked through slots 7, 8 in the upper surfaces of the wings and fuselage flows through conduits 6 having rearward bends 9 to internal-combustion, turbo-blower, jet propulsion units 1, 2, 3. The units 1, 2 may drive propellers 10. The conduits 6 may form part of the wing structure.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB17352/42A GB568667A (en) | 1942-12-07 | 1942-12-07 | Improvements in and relating to aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB17352/42A GB568667A (en) | 1942-12-07 | 1942-12-07 | Improvements in and relating to aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB568667A true GB568667A (en) | 1945-04-16 |
Family
ID=10093669
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB17352/42A Expired GB568667A (en) | 1942-12-07 | 1942-12-07 | Improvements in and relating to aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB568667A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2504421A (en) * | 1946-04-25 | 1950-04-18 | Lockheed Aircraft Corp | Aircraft engine and fuselage arrangement |
US2557522A (en) * | 1946-05-28 | 1951-06-19 | Sncase | Aerodynes equipped with reaction jet propulsion means |
US2604277A (en) * | 1945-03-31 | 1952-07-22 | Rateau Soc | Jet propulsion and boundary layer control system for aircraft |
US2657881A (en) * | 1947-04-17 | 1953-11-03 | Douglas Aubrey | Jet propulsion and boundary layer control means |
US2745611A (en) * | 1946-05-29 | 1956-05-15 | Rateau Soc | Jet propulsion and boundary layer control system for aircraft |
US2982495A (en) * | 1951-08-16 | 1961-05-02 | Rolls Royce | Aircraft with tiltable lift engines |
WO2006012809A1 (en) * | 2004-07-31 | 2006-02-09 | Birgit Bergmann | Aerodynamics optimised by combined air intake for an engine and a boundary suctioning layer |
-
1942
- 1942-12-07 GB GB17352/42A patent/GB568667A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2604277A (en) * | 1945-03-31 | 1952-07-22 | Rateau Soc | Jet propulsion and boundary layer control system for aircraft |
US2504421A (en) * | 1946-04-25 | 1950-04-18 | Lockheed Aircraft Corp | Aircraft engine and fuselage arrangement |
US2557522A (en) * | 1946-05-28 | 1951-06-19 | Sncase | Aerodynes equipped with reaction jet propulsion means |
US2745611A (en) * | 1946-05-29 | 1956-05-15 | Rateau Soc | Jet propulsion and boundary layer control system for aircraft |
US2657881A (en) * | 1947-04-17 | 1953-11-03 | Douglas Aubrey | Jet propulsion and boundary layer control means |
US2982495A (en) * | 1951-08-16 | 1961-05-02 | Rolls Royce | Aircraft with tiltable lift engines |
WO2006012809A1 (en) * | 2004-07-31 | 2006-02-09 | Birgit Bergmann | Aerodynamics optimised by combined air intake for an engine and a boundary suctioning layer |
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