AU2001234677A1 - Improved aerobatic aircraft - Google Patents

Improved aerobatic aircraft

Info

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
Application number
AU2001234677A
Inventor
John Wadleigh
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of AU2001234677A1 publication Critical patent/AU2001234677A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/04Aircraft not otherwise provided for having multiple fuselages or tail booms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/04Aircraft characterised by the type or position of power plants of piston type
    • B64D27/08Aircraft characterised by the type or position of power plants of piston type within, or attached to, fuselages
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/10Aircraft characterised by the type or position of power plants of gas-turbine type 
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01MLUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
    • F01M11/00Component parts, details or accessories, not provided for in, or of interest apart from, groups F01M1/00 - F01M9/00
    • F01M11/06Means for keeping lubricant level constant or for accommodating movement or position of machines or engines
    • F01M11/062Accommodating movement or position of machines or engines, e.g. dry sumps
    • F01M11/065Position
    • F01M11/067Position 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.
AU2001234677A 2000-01-31 2001-01-31 Improved aerobatic aircraft Abandoned AU2001234677A1 (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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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