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 PDF

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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
Application number
PCT/RU1999/000115
Other languages
French (fr)
Other versions
WO1999054181A2 (en
Inventor
Valentin Vasilievich Nazarov
Original Assignee
Otarid Consult Limited
Zisis Gazos
Valentin Vasilievich Nazarov
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Otarid Consult Limited, Zisis Gazos, Valentin Vasilievich Nazarov filed Critical Otarid Consult Limited
Priority to AU35427/99A priority Critical patent/AU3542799A/en
Publication of WO1999054181A2 publication Critical patent/WO1999054181A2/en
Publication of WO1999054181A3 publication Critical patent/WO1999054181A3/en

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

The invention relates to vehicles of airplane's type designated for short-haul and mean-haul operation routes for passenger and freight traffic transportation. Power transfer is performed from gas generators to lift propulsors-fans, cruise propulsor (3) and to a device designed to create a gas jet curtain. Additional modules (5) are disposed on the wing (4) tips. These modules and fuselage are made in the form of aerodynamic airfoils. A static air cushion is created. The propulsion-fans are disposed near the bottom of the vehicle. A jet is created and directed to a supporting surface and intensive suction of boundary layer from the upper airfoil section is also performed. The aircraft is made as the ground-air amphibian type. It comprises the fuselage with passenger cabin and additional compartments. The lift wing end plates (6) mounted on its tips. Lift propulsors-fans form start and landing multi-chamber air cushion that is retained by gas jet curtains. The gas generators are connected to actuators by gas secured to the end plates of the wing.
PCT/RU1999/000115 1998-04-16 1999-04-12 Method of creation of airplane type aircraft forces system and aircraft - ground-air amphibian for its implementation WO1999054181A2 (en)

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
RU98107154/28A 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
RU98107154 1998-04-16

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)

* Cited by examiner, † Cited by third party
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
WO2017065858A2 (en) 2015-09-02 2017-04-20 Jetoptera, Inc. Ejector and airfoil configurations
US11001378B2 (en) 2016-08-08 2021-05-11 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
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
JP7155174B2 (en) 2017-06-27 2022-10-18 ジェトプテラ、インコーポレイテッド Aircraft vertical take-off and landing system configuration
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (4)

* Cited by examiner, † Cited by third party
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
WO1999054181A2 (en) 1999-10-28
RU2127202C1 (en) 1999-03-10
AU3542799A (en) 1999-11-08

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