WO1999054181A3 - Method of creation of airplane type aircraft forces system and aircraft - ground-air amphibian for its implementation - Google Patents
Method of creation of airplane type aircraft forces system and aircraft - ground-air amphibian for its implementation Download PDFInfo
- Publication number
- WO1999054181A3 WO1999054181A3 PCT/RU1999/000115 RU9900115W WO9954181A3 WO 1999054181 A3 WO1999054181 A3 WO 1999054181A3 RU 9900115 W RU9900115 W RU 9900115W WO 9954181 A3 WO9954181 A3 WO 9954181A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- aircraft
- gas
- fans
- wing
- ground
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60V—AIR-CUSHION VEHICLES
- B60V3/00—Land vehicles, waterborne vessels, or aircraft, adapted or modified to travel on air cushions
- B60V3/08—Aircraft, e.g. air-cushion alighting-gear therefor
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU35427/99A AU3542799A (en) | 1998-04-16 | 1999-04-12 | Method of creation of airplane type aircraft forces system and aircraft - ground-air amphibian for its implementation |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU98107154 | 1998-04-16 | ||
RU98107154/28A RU2127202C1 (en) | 1998-04-16 | 1998-04-16 | Method of creating system of forces of aircraft of aeroplane configuration and ground-air amphibious vehicle for implementing this method |
Publications (2)
Publication Number | Publication Date |
---|---|
WO1999054181A2 WO1999054181A2 (en) | 1999-10-28 |
WO1999054181A3 true WO1999054181A3 (en) | 1999-12-23 |
Family
ID=20204838
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/RU1999/000115 WO1999054181A2 (en) | 1998-04-16 | 1999-04-12 | Method of creation of airplane type aircraft forces system and aircraft - ground-air amphibian for its implementation |
Country Status (3)
Country | Link |
---|---|
AU (1) | AU3542799A (en) |
RU (1) | RU2127202C1 (en) |
WO (1) | WO1999054181A2 (en) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2190869B1 (en) * | 2001-04-06 | 2005-02-01 | Gamesa Desarrollos Aeronauticos, S.A. (Soc. Unip) | COMBINED VEHICLE OF SOIL EFFECT AND CONVENTIONAL FLIGHT. |
US6848650B2 (en) * | 2001-10-29 | 2005-02-01 | The Boeing Company | Ground effect airplane |
US7398740B2 (en) * | 2005-01-26 | 2008-07-15 | Boncodin Franz B | Multi-mission/purpose ground-effect craft derived from a common modular platform |
DE102009004239A1 (en) | 2009-01-05 | 2010-07-08 | Ivan Novikov-Kopp | Method for the complex increase of aerodynamic and transport properties, ground effect vehicle for carrying out the method (variants) and flight method |
US9108612B2 (en) * | 2013-04-22 | 2015-08-18 | John Gregory | Hovercraft with multiple, independently-operable lift chambers |
US11001378B2 (en) | 2016-08-08 | 2021-05-11 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
AU2016338382B2 (en) | 2015-09-02 | 2021-04-01 | Jetoptera, Inc. | Ejector and airfoil configurations |
US10464668B2 (en) | 2015-09-02 | 2019-11-05 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
RU2648145C1 (en) * | 2016-11-30 | 2018-03-27 | Федеральное государственное автономное образовательное учреждение высшего образования "Национальный исследовательский Нижегородский государственный университет им. Н.И. Лобачевского" | High-speed air-cushion vessel with aerodynamic discharge |
WO2019005937A1 (en) | 2017-06-27 | 2019-01-03 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
RU2674622C1 (en) * | 2017-11-23 | 2018-12-12 | Общество с ограниченной ответственностью "Техноветер" | Convertiplane |
US11440665B2 (en) | 2018-10-23 | 2022-09-13 | Airbus Operations Gmbh | Vented leading-edge assembly and method for manufacturing a vented leading-edge assembly |
CN111959747A (en) * | 2020-08-26 | 2020-11-20 | 中山大学 | Novel jet-propelled lift-increasing and stability-increasing amphibious aircraft and application method thereof |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3026066A (en) * | 1959-10-19 | 1962-03-20 | Eugene A Coates | Combination land and air vehicle |
US3972490A (en) * | 1975-03-07 | 1976-08-03 | Mcdonnell Douglas Corporation | Trifan powered VSTOL aircraft |
RU2033945C1 (en) * | 1992-05-22 | 1995-04-30 | Научно-производственная кооперативная фирма "ЭКИП" | Flying vehicle, boundary layer suction control system, control system of injection to boundary layer, device for fixing position of shedding of flow from trailing edge of fuselage and its air cushion alighting gear |
RU2068345C1 (en) * | 1990-06-07 | 1996-10-27 | Назаров Валентин Васильевич | Ground-air amphibious vehicle |
-
1998
- 1998-04-16 RU RU98107154/28A patent/RU2127202C1/en not_active IP Right Cessation
-
1999
- 1999-04-12 WO PCT/RU1999/000115 patent/WO1999054181A2/en active Application Filing
- 1999-04-12 AU AU35427/99A patent/AU3542799A/en not_active Abandoned
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3026066A (en) * | 1959-10-19 | 1962-03-20 | Eugene A Coates | Combination land and air vehicle |
US3972490A (en) * | 1975-03-07 | 1976-08-03 | Mcdonnell Douglas Corporation | Trifan powered VSTOL aircraft |
RU2068345C1 (en) * | 1990-06-07 | 1996-10-27 | Назаров Валентин Васильевич | Ground-air amphibious vehicle |
RU2033945C1 (en) * | 1992-05-22 | 1995-04-30 | Научно-производственная кооперативная фирма "ЭКИП" | Flying vehicle, boundary layer suction control system, control system of injection to boundary layer, device for fixing position of shedding of flow from trailing edge of fuselage and its air cushion alighting gear |
Also Published As
Publication number | Publication date |
---|---|
AU3542799A (en) | 1999-11-08 |
WO1999054181A2 (en) | 1999-10-28 |
RU2127202C1 (en) | 1999-03-10 |
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