AU2001234677A1 - Improved aerobatic aircraft - Google Patents
Improved aerobatic aircraftInfo
- Publication number
- AU2001234677A1 AU2001234677A1 AU2001234677A AU3467701A AU2001234677A1 AU 2001234677 A1 AU2001234677 A1 AU 2001234677A1 AU 2001234677 A AU2001234677 A AU 2001234677A AU 3467701 A AU3467701 A AU 3467701A AU 2001234677 A1 AU2001234677 A1 AU 2001234677A1
- Authority
- AU
- Australia
- Prior art keywords
- improved
- fuselage
- aircraft
- engines
- aerobatic
- 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.)
- Abandoned
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/04—Aircraft not otherwise provided for having multiple fuselages or tail booms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/04—Aircraft characterised by the type or position of power plants of piston type
- B64D27/08—Aircraft characterised by the type or position of power plants of piston type within, or attached to, fuselages
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M11/00—Component parts, details or accessories, not provided for in, or of interest apart from, groups F01M1/00 - F01M9/00
- F01M11/06—Means for keeping lubricant level constant or for accommodating movement or position of machines or engines
- F01M11/062—Accommodating movement or position of machines or engines, e.g. dry sumps
- F01M11/065—Position
- F01M11/067—Position inverted, e.g. for inverted flight
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Transmission Devices (AREA)
- Processes Of Treating Macromolecular Substances (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
- Tires In General (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Polymerisation Methods In General (AREA)
- Graft Or Block Polymers (AREA)
Abstract
An improved aerobatic aircraft design having a first engine located in the nose portion of the fuselage and a second engine located in the tail portion of the fuselage. The thrust components of both the first and second engines are coaxial along the long axis of the fuselage. Both engines can individually provide sufficient power for the aircraft to takeoff, maintain altitude, and/or land.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09494710 | 2000-01-31 | ||
US09/494,710 US6367738B1 (en) | 2000-01-31 | 2000-01-31 | Aerobatic aircraft |
PCT/US2001/003119 WO2001054978A1 (en) | 2000-01-31 | 2001-01-31 | Improved aerobatic aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
AU2001234677A1 true AU2001234677A1 (en) | 2001-08-07 |
Family
ID=23965645
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU2001234677A Abandoned AU2001234677A1 (en) | 2000-01-31 | 2001-01-31 | Improved aerobatic aircraft |
Country Status (9)
Country | Link |
---|---|
US (1) | US6367738B1 (en) |
EP (1) | EP1257467B1 (en) |
AT (1) | ATE368615T1 (en) |
AU (1) | AU2001234677A1 (en) |
CA (1) | CA2398903C (en) |
CZ (1) | CZ20022622A3 (en) |
DE (1) | DE60129671T2 (en) |
RU (1) | RU2274586C2 (en) |
WO (1) | WO2001054978A1 (en) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6969026B2 (en) * | 2002-12-20 | 2005-11-29 | Tsuneo Kayama | Aircraft |
US20060016931A1 (en) * | 2004-01-28 | 2006-01-26 | Malvestuto Frank S | High-lift, low-drag dual fuselage aircraft |
WO2013070296A2 (en) * | 2011-08-19 | 2013-05-16 | Aerovironment, Inc. | Aircraft system for reduced observer visibility |
US9511858B2 (en) * | 2011-08-19 | 2016-12-06 | Aerovironment, Inc. | Inverted-landing aircraft |
US9208689B2 (en) | 2011-08-19 | 2015-12-08 | Aerovironment Inc. | Deep stall aircraft landing |
WO2014108125A1 (en) * | 2013-01-10 | 2014-07-17 | Malte Schwarze | Low-noise, high-efficiency aircraft |
US9527597B1 (en) * | 2013-01-11 | 2016-12-27 | Jaime Sada | Unmanned aerial vehicle with twin-engine fore/AFT configuration and associated systems and methods |
US9567088B2 (en) | 2013-10-15 | 2017-02-14 | Swift Engineering, Inc. | Vertical take-off and landing aircraft |
WO2015138217A1 (en) | 2014-03-13 | 2015-09-17 | Endurant Systems, Llc | Uav configurations and battery augmentation for uav internal combustion engines, and associated systems and methods |
WO2015157114A1 (en) | 2014-04-11 | 2015-10-15 | Sada-Salinas Jaime G | Modular nacelles to provide vertical takeoff and landing (vtol) capabilities to fixed wing aerial vehicles, and associated systems and methods |
US9821909B2 (en) | 2016-04-05 | 2017-11-21 | Swift Engineering, Inc. | Rotating wing assemblies for tailsitter aircraft |
US11208210B2 (en) | 2017-12-01 | 2021-12-28 | Wipaire, Inc. | Float plane technology |
US20200079492A1 (en) | 2018-09-11 | 2020-03-12 | Swift Engineering, Inc. | Systems and methods for aerodynamic deployment of wing structures |
US11597514B2 (en) * | 2019-08-16 | 2023-03-07 | Embraer S.A. | Unmanned aircraft having reduced acoustic signatures |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1538801A (en) * | 1922-11-14 | 1925-05-19 | Theodore P Hall | Airplane |
US1874523A (en) * | 1930-07-08 | 1932-08-30 | Curtiss Aeroplane & Motor Co | Aircraft cowling for tandem motors |
US2140783A (en) * | 1937-08-03 | 1938-12-20 | Miller Bellanca Airplanes Ltd | Airplane construction |
US2678783A (en) * | 1940-04-15 | 1954-05-18 | Myers George Francis | Convertible aircraft |
US4012012A (en) * | 1975-10-30 | 1977-03-15 | Lockheed Aircraft Corporation | Supplemental oil system for engines |
US4089493A (en) | 1976-09-29 | 1978-05-16 | Paulson Allen E | Aircraft with combination power plant |
GB2016397B (en) | 1978-02-02 | 1982-03-24 | Aerospatiale | Aerofoil |
DE3137947C2 (en) * | 1980-09-26 | 1983-10-27 | Rolls-Royce Ltd., London | Lubricating oil system for gas turbine engines suitable for any flight maneuver |
US4447022A (en) | 1982-05-21 | 1984-05-08 | Lion Charles E | Reduced noise monolithic wing-stabilizer aircraft |
US4565530A (en) | 1983-12-05 | 1986-01-21 | Espenhain Donald L | Reciprocating marine propulsion engine |
US5076516A (en) | 1984-10-29 | 1991-12-31 | Wheat Robert B | High drag airfoil apparatus |
US4643639A (en) | 1984-12-24 | 1987-02-17 | Sundstrand Corporation | Adjustable centrifugal pump |
GB8810616D0 (en) * | 1988-05-05 | 1988-06-08 | British Aerospace | Aircraft of split turboprop configuration |
US5086993A (en) * | 1989-02-09 | 1992-02-11 | Aca Industries | Airplane with variable-incidence wing |
US5645250A (en) | 1993-08-26 | 1997-07-08 | Gevers; David E. | Multi-purpose aircraft |
US5520355A (en) * | 1993-09-16 | 1996-05-28 | Jones; Jack M. | Three wing circular planform body |
US5782427A (en) * | 1994-11-28 | 1998-07-21 | Hermach; Carl J. | Tandem-engine aircraft propulsion module |
-
2000
- 2000-01-31 US US09/494,710 patent/US6367738B1/en not_active Expired - Lifetime
-
2001
- 2001-01-31 CA CA002398903A patent/CA2398903C/en not_active Expired - Fee Related
- 2001-01-31 WO PCT/US2001/003119 patent/WO2001054978A1/en active IP Right Grant
- 2001-01-31 RU RU2002123366/11A patent/RU2274586C2/en not_active IP Right Cessation
- 2001-01-31 CZ CZ20022622A patent/CZ20022622A3/en unknown
- 2001-01-31 DE DE60129671T patent/DE60129671T2/en not_active Expired - Lifetime
- 2001-01-31 AT AT01906811T patent/ATE368615T1/en not_active IP Right Cessation
- 2001-01-31 AU AU2001234677A patent/AU2001234677A1/en not_active Abandoned
- 2001-01-31 EP EP01906811A patent/EP1257467B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
WO2001054978A1 (en) | 2001-08-02 |
EP1257467B1 (en) | 2007-08-01 |
CA2398903A1 (en) | 2001-08-02 |
RU2274586C2 (en) | 2006-04-20 |
EP1257467A4 (en) | 2006-02-22 |
CZ20022622A3 (en) | 2003-06-18 |
DE60129671D1 (en) | 2007-09-13 |
CA2398903C (en) | 2006-05-02 |
ATE368615T1 (en) | 2007-08-15 |
US6367738B1 (en) | 2002-04-09 |
EP1257467A1 (en) | 2002-11-20 |
DE60129671T2 (en) | 2008-04-30 |
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