GB745344A - Improvements in flying machines having a propelling power plant with an air intake - Google Patents
Improvements in flying machines having a propelling power plant with an air intakeInfo
- Publication number
- GB745344A GB745344A GB22995/51A GB2299551A GB745344A GB 745344 A GB745344 A GB 745344A GB 22995/51 A GB22995/51 A GB 22995/51A GB 2299551 A GB2299551 A GB 2299551A GB 745344 A GB745344 A GB 745344A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- aircraft
- power plant
- axis
- annular
- 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
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/001—Shrouded propellers
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
745,344. Controlling jet-propelled aircraft. ZBOROWSKI, H. P. G. A. R. VON. Oct. 3, 1951 [Oct. 4, 1950], No. 22995/51. Class 4. [Also in Group XXI] An aircraft has an annular tunnel-shaped wing and a propelling power plant in which said wing is the only main aerodynamic supporting surface of the aircraft and is in the form of a body of revolution about a rectilinear axis forming the fore-and-aft axis of the aircraft, the sections of the wing by planes containing said axis being in the form of aerofoils, the power plant being arranged to give a thrust along or thrusts evenly balanced about said fore-and-aft axis, means being provided for exerting an aerodynamic control action in a direction transverse to said axis. An annular wing 1 carries inwardly directed arms 5 to locate a body or fuselage 4 and a turbo-jet engine 8 and flaps 7 are located around the periphery of the body for radial displacement whereby a control effect may be exerted on the aircraft. In other embodiments the flaps may be mounted on an auxiliary aerofoil forward of the body or on the inner or outer surface of the wing 1 or a single auxiliary annular control surface may be mounted ahead of the fuselage with universal freedom of movement. Alternative power plant arrangements comprise an engine driving two contra-rotating propellers in which hot gases from the engine may be used to heat the air flowing through the propeller disc and ram jet units located within the annular space formed by the inner and outer wing surfaces.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR745344X | 1950-10-04 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB745344A true GB745344A (en) | 1956-02-22 |
Family
ID=9146976
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB22995/51A Expired GB745344A (en) | 1950-10-04 | 1951-10-03 | Improvements in flying machines having a propelling power plant with an air intake |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB745344A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2918231A (en) * | 1956-09-17 | 1959-12-22 | Collins Radio Co | Fluid sustained and fluid propelled aircraft |
| US2918232A (en) * | 1956-09-24 | 1959-12-22 | Collins Radio Co | Twin shroud aerodyne |
-
1951
- 1951-10-03 GB GB22995/51A patent/GB745344A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2918231A (en) * | 1956-09-17 | 1959-12-22 | Collins Radio Co | Fluid sustained and fluid propelled aircraft |
| US2918232A (en) * | 1956-09-24 | 1959-12-22 | Collins Radio Co | Twin shroud aerodyne |
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