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IT1175605B - Aeroplano a doppio sistema di ali o multi-ala - Google Patents

Aeroplano a doppio sistema di ali o multi-ala

Info

Publication number
IT1175605B
IT1175605B IT22347/84A IT2234784A IT1175605B IT 1175605 B IT1175605 B IT 1175605B IT 22347/84 A IT22347/84 A IT 22347/84A IT 2234784 A IT2234784 A IT 2234784A IT 1175605 B IT1175605 B IT 1175605B
Authority
IT
Italy
Prior art keywords
wings
airplane
double
double wings
wings airplane
Prior art date
Application number
IT22347/84A
Other languages
English (en)
Other versions
IT8422347A0 (it
Inventor
Elbert Leander Rutan
Original Assignee
Elbert Leander Rutan
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 Elbert Leander Rutan filed Critical Elbert Leander Rutan
Publication of IT8422347A0 publication Critical patent/IT8422347A0/it
Application granted granted Critical
Publication of IT1175605B publication Critical patent/IT1175605B/it

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable
    • B64C5/14—Varying angle of sweep
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/54—Varying in area
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/12—Canard-type aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/12—Adjustable control surfaces or members, e.g. rudders surfaces of different type or function being simultaneously adjusted
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/34—Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/30—Wing lift efficiency
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)
  • Retarders (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • General Details Of Gearings (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Details Of Aerials (AREA)
IT22347/84A 1983-08-18 1984-08-17 Aeroplano a doppio sistema di ali o multi-ala IT1175605B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/524,332 US4641800A (en) 1983-08-18 1983-08-18 Tandem or multi-winged high performance aircraft

Publications (2)

Publication Number Publication Date
IT8422347A0 IT8422347A0 (it) 1984-08-17
IT1175605B true IT1175605B (it) 1987-07-15

Family

ID=24088750

Family Applications (1)

Application Number Title Priority Date Filing Date
IT22347/84A IT1175605B (it) 1983-08-18 1984-08-17 Aeroplano a doppio sistema di ali o multi-ala

Country Status (10)

Country Link
US (1) US4641800A (it)
JP (1) JPS60110599A (it)
AU (1) AU561636B2 (it)
DE (1) DE3430377A1 (it)
FR (1) FR2550755B1 (it)
GB (1) GB2145049B (it)
IE (1) IE55398B1 (it)
IL (1) IL72708A (it)
IT (1) IT1175605B (it)
SE (1) SE452297B (it)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
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DE3710914A1 (de) * 1987-04-01 1988-10-20 Florian Dipl Ing Windischbauer Fluggeraet variabler geometrie
US4848700A (en) * 1987-04-16 1989-07-18 Lockheed John A Canard control system for aircraft
US5071088A (en) * 1989-11-29 1991-12-10 The United States Of America As Represented By The Secretary Of The Navy High lift aircraft
US5020740A (en) * 1990-03-28 1991-06-04 Thomas Hugh O Pitch control trimming system for canard design aircraft
RU2000251C1 (ru) * 1992-03-04 1993-09-07 Краснов Ю.К. УТ(54) ЛЕТАТЕЛЬНЫЙ АППАРАТ СХЕМЫ КА "Летательный аппарат схемы "утка"
US5839691A (en) 1996-05-22 1998-11-24 Lariviere; Jean Soulez Vertical takeoff and landing aircraft
US5992796A (en) * 1997-03-13 1999-11-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Secondary wing system for use on an aircraft
DE19835191C1 (de) * 1998-08-04 2000-04-20 Daimler Chrysler Ag Flugsteuerungseinrichtung zur Verbesserung der Längsstabilität eines geregelten Flugzeugs
US6857599B2 (en) * 2002-12-30 2005-02-22 Aerion Corporation Highly swept canard with low sweep wing supersonic aircraft configuration
US7870334B2 (en) * 2003-11-12 2011-01-11 International Business Machines Corporation Distributed task queues in a multiple-port storage system
US20050045764A1 (en) * 2003-08-29 2005-03-03 Supersonic Aerospace International, Llc Canard position and dihedral for boom reduction and pitch/directional control
US8763951B2 (en) * 2003-11-04 2014-07-01 Frank C. Smith, Jr. Cargo oriented personal aircraft
US20060016931A1 (en) * 2004-01-28 2006-01-26 Malvestuto Frank S High-lift, low-drag dual fuselage aircraft
JP2007112199A (ja) * 2005-10-18 2007-05-10 Osamu Miyake 無線操縦飛行機
FR2907422B1 (fr) * 2006-10-20 2009-12-18 Astrium Sas Aeronef a vol mixte aerodynamique et spatial, et procede de pilotage associe.
FR2915179B1 (fr) * 2007-04-23 2009-05-29 Airbus France Sa Aeronef a impact environnemental reduit.
US8191820B1 (en) * 2007-12-11 2012-06-05 Northrop Gurmman Corporation Flying wing aircraft
US8292220B1 (en) * 2009-03-19 2012-10-23 Northrop Grumman Corporation Flying wing aircraft with modular missionized elements
FR2949434B1 (fr) 2009-08-28 2011-10-07 Benjamin Parzy Aeronef comportant au moins deux groupes motopropulseurs electriques montes a l'arriere
DE102010012414A1 (de) * 2010-03-23 2011-09-29 Deutsches Zentrum für Luft- und Raumfahrt e.V. Bemanntes Luftfahrzeug
WO2011140551A1 (en) * 2010-05-07 2011-11-10 Ohio University Multi-modal vehicle
WO2012107650A1 (fr) * 2011-02-11 2012-08-16 Airbus Operations (S.A.S) Avion à système propulsif arrière
EP2687437B1 (en) * 2012-07-16 2017-01-18 Airbus Operations, S.L. Aircraft lifting surface with variable sweep distribution along the span
US8727264B1 (en) 2013-06-11 2014-05-20 Elbert L. Rutan Dynamic tow maneuver orbital launch technique
US8960590B2 (en) 2013-07-18 2015-02-24 Elbert L. Rutan Pressure-equalizing cradle for booster rocket mounting
CN108137150B (zh) * 2015-09-02 2021-07-06 杰托普特拉股份有限公司 流体推进系统
US10669026B2 (en) 2016-04-01 2020-06-02 Albert Aguilar Lift cell modules and lift pods
DE102017122359A1 (de) * 2017-09-26 2019-03-28 Paul Schreiber Luftfahrzeug in Drachenkonfiguration
US11691713B2 (en) * 2019-03-17 2023-07-04 Behrang Mehrgan VTOL having retractable wings
US11691726B2 (en) * 2019-06-19 2023-07-04 Darius Sharifzadeh Vertical take-off and landing aircraft
FR3101853B1 (fr) * 2019-10-15 2022-04-29 Safran Nacelles Avion à nacelle déportée affleurant le sillage de l’aile
WO2021206970A1 (en) * 2020-04-07 2021-10-14 MightyFly Inc. System and method for package transportation
GB2620625A (en) * 2022-07-14 2024-01-17 Airbus Operations Ltd Aircraft wing trailing edge device

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB814450A (en) * 1954-03-15 1959-06-03 Roe A V & Co Ltd Improvements in tail-first aircraft
GB951346A (it) *
FR413781A (fr) * 1910-03-15 1910-08-18 Maurice Verlaine Aéroplane biplan
GB493655A (en) * 1936-06-29 1938-10-12 Derde Hillegomsche Mij Tot Exp Improvements in and relating to aircraft
US2744698A (en) * 1949-03-11 1956-05-08 Baynes Aircraft Interiors Ltd High speed aircraft wing and tail surfaces having variable sweepback
FR1032665A (fr) * 1950-12-23 1953-07-03 Perfectionnements apportés aux engins de navigation aérienne
US2924400A (en) * 1953-05-22 1960-02-09 Nord Aviation Apparatus for enabling the manoeuvrability and the stability of a supersonic aircraft to be controlled
FR1117803A (fr) * 1953-12-31 1956-05-28 United Aircraft Corp Perfectionnements à des avions
US3330501A (en) * 1965-09-27 1967-07-11 Theodore C Barber Airplane construction
IL33185A (en) * 1969-10-14 1973-10-25 Bouhnik J Variable delta wing aircraft
US3738595A (en) * 1969-10-14 1973-06-12 J Bouchnik Delta-wing aircraft
US3776491A (en) * 1971-06-25 1973-12-04 R Oulton Aircraft with compound wing
US3926389A (en) * 1972-05-24 1975-12-16 Messerschmitt Boelkow Blohm Aircraft of a controllable stability
US4093156A (en) * 1976-08-27 1978-06-06 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Supersonic transport

Also Published As

Publication number Publication date
IT8422347A0 (it) 1984-08-17
SE452297B (sv) 1987-11-23
JPH0316319B2 (it) 1991-03-05
JPS60110599A (ja) 1985-06-17
AU561636B2 (en) 1987-05-14
FR2550755A1 (fr) 1985-02-22
US4641800A (en) 1987-02-10
GB8420087D0 (en) 1984-09-12
FR2550755B1 (fr) 1990-11-02
IE55398B1 (en) 1990-08-29
AU3201584A (en) 1985-02-21
SE8404077L (sv) 1985-02-19
DE3430377C2 (it) 1991-07-25
GB2145049B (en) 1986-09-03
DE3430377A1 (de) 1985-04-04
SE8404077D0 (sv) 1984-08-13
GB2145049A (en) 1985-03-20
IL72708A (en) 1989-02-28
IE842135L (en) 1985-02-18

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