WO2000001576A3 - A device for generating an aerodynamic force by differentially accelerating the fluid in the two sides of a surface - Google Patents
A device for generating an aerodynamic force by differentially accelerating the fluid in the two sides of a surface Download PDFInfo
- Publication number
- WO2000001576A3 WO2000001576A3 PCT/BR1999/000057 BR9900057W WO0001576A3 WO 2000001576 A3 WO2000001576 A3 WO 2000001576A3 BR 9900057 W BR9900057 W BR 9900057W WO 0001576 A3 WO0001576 A3 WO 0001576A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- convergent
- channel
- divergent
- fluid
- differentially
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
Abstract
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU45949/99A AU4594999A (en) | 1998-07-06 | 1999-07-05 | A device for generating an aerodynamic force by differentially accelerating the fluid in the two sides of surface |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BRPI9806466-5 | 1998-07-06 | ||
BR9806466A BR9806466A (en) | 1998-07-06 | 1998-07-06 | High aerodynamic support devices by |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2000001576A2 WO2000001576A2 (en) | 2000-01-13 |
WO2000001576A3 true WO2000001576A3 (en) | 2000-06-15 |
Family
ID=4071466
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/BR1999/000057 WO2000001576A2 (en) | 1998-07-06 | 1999-07-05 | A device for generating an aerodynamic force by differentially accelerating the fluid in the two sides of a surface |
Country Status (3)
Country | Link |
---|---|
AU (1) | AU4594999A (en) |
BR (1) | BR9806466A (en) |
WO (1) | WO2000001576A2 (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2527628C2 (en) * | 2012-07-31 | 2014-09-10 | Алексей Валентинович Ильин | Method of increasing aircraft wing lift |
US10464668B2 (en) | 2015-09-02 | 2019-11-05 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
US11001378B2 (en) | 2016-08-08 | 2021-05-11 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
CA2996285C (en) | 2015-09-02 | 2023-10-31 | Jetoptera, Inc. | Ejector and airfoil configurations |
RU2670161C1 (en) * | 2017-06-06 | 2018-10-18 | Борис Никифорович Сушенцев | Aircraft (options) |
BR112019027805A2 (en) | 2017-06-27 | 2020-07-07 | Jetoptera, Inc. | configuration of vertical take-off and landing system for aerial vehicles |
RU2694478C1 (en) * | 2018-11-12 | 2019-07-15 | Борис Никифорович Сушенцев | Wing with variable aerodynamic characteristics and aircraft (versions) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2353245A1 (en) * | 1973-10-24 | 1975-04-30 | Dornier Gmbh | High lift wing flaps for aeroplane wings - can be swung from body stored position to leading and trailing edges |
DE2819649A1 (en) * | 1978-05-05 | 1979-11-08 | Berthold Loewe | Propulsive suction generating aircraft wing - has air ducted from underside to top behind point of max. thickness, and leading and trailing edge flaps |
US4830315A (en) * | 1986-04-30 | 1989-05-16 | United Technologies Corporation | Airfoil-shaped body |
DE3827796A1 (en) * | 1988-08-16 | 1990-02-22 | Eduard Weinert | Auxiliary wing |
-
1998
- 1998-07-06 BR BR9806466A patent/BR9806466A/en not_active Application Discontinuation
-
1999
- 1999-07-05 AU AU45949/99A patent/AU4594999A/en not_active Abandoned
- 1999-07-05 WO PCT/BR1999/000057 patent/WO2000001576A2/en active Application Filing
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2353245A1 (en) * | 1973-10-24 | 1975-04-30 | Dornier Gmbh | High lift wing flaps for aeroplane wings - can be swung from body stored position to leading and trailing edges |
DE2819649A1 (en) * | 1978-05-05 | 1979-11-08 | Berthold Loewe | Propulsive suction generating aircraft wing - has air ducted from underside to top behind point of max. thickness, and leading and trailing edge flaps |
US4830315A (en) * | 1986-04-30 | 1989-05-16 | United Technologies Corporation | Airfoil-shaped body |
DE3827796A1 (en) * | 1988-08-16 | 1990-02-22 | Eduard Weinert | Auxiliary wing |
Also Published As
Publication number | Publication date |
---|---|
BR9806466A (en) | 2000-03-21 |
AU4594999A (en) | 2000-01-24 |
WO2000001576A2 (en) | 2000-01-13 |
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