WO1989007073A3 - Aeronef - Google Patents
Aeronef Download PDFInfo
- Publication number
- WO1989007073A3 WO1989007073A3 PCT/DE1989/000072 DE8900072W WO8907073A3 WO 1989007073 A3 WO1989007073 A3 WO 1989007073A3 DE 8900072 W DE8900072 W DE 8900072W WO 8907073 A3 WO8907073 A3 WO 8907073A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- rotors
- rotor
- aircraft
- slipstream
- ailerons
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/003—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage
- B64C39/005—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage about a horizontal transversal axis
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/08—Influencing air flow over aircraft surfaces, not otherwise provided for using Magnus effect
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Retarders (AREA)
Abstract
Un aéronef possède deux rotors (13, 14) entraînés par le moteur qui entraîne simultanément également l'hélice. Le fait que l'empennage se trouve entièrement dans le souffle de l'hélice et qu'en outre les ailerons et les volets d'atterrissage se trouvent dans le jet d'air dirigé vers le bas derrière le rotor, le jet d'air s'écoulant par-dessus le rotor, permet d'obtenir, conjointement avec une incidence en V des deux rotors (13, 14), une portance optimale.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEP3804415.3 | 1988-02-08 | ||
DE3804415A DE3804415A1 (de) | 1986-08-09 | 1988-02-08 | Rotorflugzeuge, lenksysteme |
Publications (2)
Publication Number | Publication Date |
---|---|
WO1989007073A2 WO1989007073A2 (fr) | 1989-08-10 |
WO1989007073A3 true WO1989007073A3 (fr) | 1989-08-24 |
Family
ID=6347306
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/DE1989/000072 WO1989007073A2 (fr) | 1988-02-08 | 1989-02-07 | Aeronef |
Country Status (2)
Country | Link |
---|---|
AU (1) | AU3340089A (fr) |
WO (1) | WO1989007073A2 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2022087C (fr) * | 1990-07-27 | 1995-02-21 | Jean-Paul Picard | Dispositif de sustentation aerienne verticale par soufflage de jets tangentiels sur le dessus de cylindres rotatifs |
GB9207016D0 (en) * | 1992-04-30 | 1992-05-13 | Walden Graeme K | Antigravity lift & propulsion and guidance system |
US5875627A (en) * | 1995-06-07 | 1999-03-02 | Jeswine; William W. | Fluid propulsion system for accelerating and directionally controlling a fluid |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1927535A (en) * | 1929-10-03 | 1933-09-19 | Zap Dev Corp | Aircraft |
US2681775A (en) * | 1951-05-24 | 1954-06-22 | Orazi Paolo | Convertible airplane having autorotatable sustaining elements |
US3140065A (en) * | 1962-06-27 | 1964-07-07 | Alvarez-Calderon Alberto | High lift and control system for aircraft |
GB2195308A (en) * | 1986-09-23 | 1988-04-07 | Lawrence Albert Holmes | Rotating wing aircraft |
DE3627085A1 (de) * | 1986-08-09 | 1988-06-23 | Weissheimer Geb Wengler | Rotorflugzeug ro ii |
-
1989
- 1989-02-07 WO PCT/DE1989/000072 patent/WO1989007073A2/fr unknown
- 1989-02-07 AU AU33400/89A patent/AU3340089A/en not_active Abandoned
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1927535A (en) * | 1929-10-03 | 1933-09-19 | Zap Dev Corp | Aircraft |
US2681775A (en) * | 1951-05-24 | 1954-06-22 | Orazi Paolo | Convertible airplane having autorotatable sustaining elements |
US3140065A (en) * | 1962-06-27 | 1964-07-07 | Alvarez-Calderon Alberto | High lift and control system for aircraft |
DE3627085A1 (de) * | 1986-08-09 | 1988-06-23 | Weissheimer Geb Wengler | Rotorflugzeug ro ii |
GB2195308A (en) * | 1986-09-23 | 1988-04-07 | Lawrence Albert Holmes | Rotating wing aircraft |
Also Published As
Publication number | Publication date |
---|---|
AU3340089A (en) | 1989-08-25 |
WO1989007073A2 (fr) | 1989-08-10 |
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