FR2427248A1 - Aeronef mixte - Google Patents

Aeronef mixte

Info

Publication number
FR2427248A1
FR2427248A1 FR7914653A FR7914653A FR2427248A1 FR 2427248 A1 FR2427248 A1 FR 2427248A1 FR 7914653 A FR7914653 A FR 7914653A FR 7914653 A FR7914653 A FR 7914653A FR 2427248 A1 FR2427248 A1 FR 2427248A1
Authority
FR
France
Prior art keywords
central body
heavy loads
flight
translational
thrust
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.)
Granted
Application number
FR7914653A
Other languages
English (en)
Other versions
FR2427248B1 (fr
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.)
INT CYCLO CRANE LICENSING
Original Assignee
INT CYCLO CRANE LICENSING
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 INT CYCLO CRANE LICENSING filed Critical INT CYCLO CRANE LICENSING
Publication of FR2427248A1 publication Critical patent/FR2427248A1/fr
Application granted granted Critical
Publication of FR2427248B1 publication Critical patent/FR2427248B1/fr
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/06—Rigid airships; Semi-rigid airships

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Tires In General (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

Aéronef mixte comprenant un corps central rempli d'un gaz plus léger que l'air et une structure portante à voilure et moteurs pour soulever des charges importantes. Le corps central peut tourner autour d'un axe horizontal en vol stationnaire et ne tourne pas pendant le vol en translation, des éléments aérodynamiques de la structure portante assurant la poussée ascensionnelle et la poussée en translation, avec éventuellement un pilotage automatique ou commandé à distance. Application au transport de charges très lourdes sous élingue.
FR7914653A 1978-05-30 1979-05-30 Aeronef mixte Granted FR2427248A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US91018678A 1978-05-30 1978-05-30

Publications (2)

Publication Number Publication Date
FR2427248A1 true FR2427248A1 (fr) 1979-12-28
FR2427248B1 FR2427248B1 (fr) 1982-10-01

Family

ID=25428426

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7914653A Granted FR2427248A1 (fr) 1978-05-30 1979-05-30 Aeronef mixte

Country Status (11)

Country Link
US (1) US4482110A (fr)
JP (1) JPS54157999A (fr)
AR (1) AR226158A1 (fr)
AU (1) AU522258B2 (fr)
BR (1) BR7903329A (fr)
CA (1) CA1171835A (fr)
DE (1) DE2922059C2 (fr)
FR (1) FR2427248A1 (fr)
GB (1) GB2030098B (fr)
MX (1) MX146565A (fr)
ZA (1) ZA792253B (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2547272A1 (fr) * 1983-06-08 1984-12-14 Lindenbaum Bernard Systeme aerien de soulevement de charges
WO1993013979A1 (fr) * 1992-01-10 1993-07-22 Buoyant Copter, Inc. Aeronef hybride

Families Citing this family (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4366936A (en) * 1979-08-06 1983-01-04 Ferguson F D Aircraft having buoyant gas balloon
US4365772A (en) * 1979-08-06 1982-12-28 Ferguson F D Aircraft having buoyant gas balloon
ZA804728B (en) * 1979-08-06 1982-03-31 F Ferguson Aircraft having buoyant gas balloon
JPS5744598A (en) * 1980-08-29 1982-03-13 Ferguson Frederick Aircraft with floating gas balloon
US4695012A (en) * 1983-06-08 1987-09-22 Bernard Lindenbaum Aerial load-lifting system
US4735552A (en) * 1985-10-04 1988-04-05 Watson William K Space frame wind turbine
JPH034640Y2 (fr) * 1988-10-11 1991-02-06
IL89468A (en) * 1989-03-03 1994-08-26 Gamzon Eliyahu Method and system for supporting an airborne vehicle in space
US5005783A (en) * 1990-01-18 1991-04-09 The United States Of America As Represented By The Secretary Of The Air Force Variable geometry airship
US5082205A (en) * 1990-08-09 1992-01-21 Caufman Robert L Semi-buoyant composite aircraft with non-rotating aerostat
US5265827A (en) * 1991-06-17 1993-11-30 Northrop Corporation Paddle wheel rotorcraft
US5931411A (en) * 1996-12-19 1999-08-03 Aereon Corporation Hovering aircraft
US5971320A (en) * 1997-08-26 1999-10-26 Jermyn; Phillip Matthew Helicopter with a gyroscopic rotor and rotor propellers to provide vectored thrust
US6142414A (en) * 1999-01-26 2000-11-07 Doolittle; William Rotor--aerostat composite aircraft
FR2832976B1 (fr) * 2001-12-05 2004-04-16 Didier Costes Dirigeable a charge suspendue
US7427047B2 (en) * 2004-05-10 2008-09-23 Omid Saeed Tehrani Powered aircraft including inflatable and rotatable bodies exhibiting a circular cross-section perpendicular to its rotation axis and in order to generate a lift force
JP2006001435A (ja) * 2004-06-18 2006-01-05 Mutsuro Bunto 多目的飛行船
US7093788B2 (en) * 2004-07-15 2006-08-22 Raytheon Company Rotating flying wing aircraft and control system
US7219854B2 (en) * 2005-03-04 2007-05-22 Information Systems Laboratories, Inc. Cycloidal hybrid advanced surface effects vehicle
DE202005009621U1 (de) 2005-06-21 2005-12-15 Singer, Csaba Senkrechtstartendes Hybridflugzeug
US7264202B2 (en) * 2005-11-01 2007-09-04 Information Systems Laboratories, Inc. Tri-cycloidal airship
US8157205B2 (en) * 2006-03-04 2012-04-17 Mcwhirk Bruce Kimberly Multibody aircrane
US20080011900A1 (en) * 2006-07-15 2008-01-17 Javier Quintana Apparatus and method to control the flight dynamics in a lighter-than-air airship
US7967238B2 (en) * 2006-09-05 2011-06-28 The Boeing Company Composite air vehicle having a heavier-than-air vehicle tethered to a lighter-than-air vehicle
US7890222B1 (en) * 2007-04-04 2011-02-15 Textron Innovations Inc. Mechanical flight control auxiliary power assist system
US8886371B2 (en) 2011-01-10 2014-11-11 William C. Peters Method and system for high fidelity VTOL and hover capability
US9611024B2 (en) 2011-08-03 2017-04-04 Lockheed Martin Corporation Ballonet measurement system
US9623954B2 (en) 2014-07-25 2017-04-18 Hyalta Aeronautices, Inc. Hybrid lighter-than-air vehicle
US10377465B2 (en) 2014-07-25 2019-08-13 Hyalta Aeronautics, Inc. Hybrid lighter-than-air vehicle
US10287000B2 (en) 2014-07-25 2019-05-14 Hyalta Aeronautics, Inc. Hybrid lighter-than-air vehicle
CN105083521A (zh) * 2015-09-18 2015-11-25 深圳市惠通环宇科技有限公司 飞艇
US10442525B2 (en) * 2016-05-07 2019-10-15 Optivector Ltd Rotor or propeller blade with dynamically variable geometry and other properties
US10661897B2 (en) 2016-07-18 2020-05-26 Nathan Ian Cobb Vertical takeoff and landing aircraft having telescoping boom for lateral payload deployment counterbalanced through multi-axis thrust vectoring
WO2018140199A2 (fr) * 2017-01-03 2018-08-02 The Texas A&M University System Microvéhicule aérien à rotor cycloïdal
US11433984B2 (en) 2019-04-19 2022-09-06 Lockheed Martin Corporation Ballonet measurement systems and methods
CN111959769B (zh) * 2020-07-09 2024-04-30 中国科学院地理科学与资源研究所 一种通过气囊进行空中悬停的无人机和控制方法
CN112182752B (zh) * 2020-09-25 2022-11-18 中国直升机设计研究所 一种直升机飞行姿态预测方法
DE102022114599B4 (de) 2022-06-09 2024-02-08 Louis Gagnon Fluggerät

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3856236A (en) * 1973-05-07 1974-12-24 All American Ind Composite aircraft

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE141948C (fr) *
US1189138A (en) * 1912-09-21 1916-06-27 Oscar J Laisy Airship.
US1430393A (en) * 1921-03-05 1922-09-26 Lynde Carleton John Dirigible
US1519866A (en) * 1921-06-29 1924-12-16 Marchetti Alessandro Stabilizer for flying apparatus sustained by propellers
US1817074A (en) * 1928-10-17 1931-08-04 Charles E Glessner Aircraft control
US2037377A (en) * 1929-01-14 1936-04-14 Albert B Gardner Construction for aircraft
US1741699A (en) * 1929-02-14 1929-12-31 Carl H Loock Dirigible airship
US1797502A (en) * 1929-05-22 1931-03-24 Charles S Hall Aircraft
US1838248A (en) * 1930-06-21 1931-12-29 Joseph M Bourland Airship
US2450954A (en) * 1945-09-04 1948-10-12 Charles S Hall Means for indicating the state of gas in cells of aircraft
US2633311A (en) * 1950-08-07 1953-03-31 Henri Van Zandt Convertible fixed-wing paddle wheel aircraft
DE1581059B1 (de) * 1961-03-22 1969-09-04 Kauffmann Hans Luftfahrzeug leichter als Luft
JPS421704Y1 (fr) * 1964-02-22 1967-02-02
JPS423219Y1 (fr) * 1964-03-17 1967-02-25
US3350956A (en) * 1965-07-06 1967-11-07 Gen Dynamics Corp Six-degree of freedom integrated controller
DE1481944A1 (de) * 1966-05-16 1969-05-08 Weidt Carl Adolf Flugzeug
DE1481954A1 (de) * 1966-12-24 1969-03-13 Manfred Werding Flugzeug mit stillsetzbaren Rotorfluegeln
US3976265A (en) * 1973-05-07 1976-08-24 All American Industries, Inc. Semibuoyant composite aircraft
US3957228A (en) * 1975-02-10 1976-05-18 Kennedy Jr Guy H Thermodynamic kite
US4114837A (en) * 1977-03-24 1978-09-19 Skagit Corporation Air transport and lifting vehicle

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3856236A (en) * 1973-05-07 1974-12-24 All American Ind Composite aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2547272A1 (fr) * 1983-06-08 1984-12-14 Lindenbaum Bernard Systeme aerien de soulevement de charges
WO1993013979A1 (fr) * 1992-01-10 1993-07-22 Buoyant Copter, Inc. Aeronef hybride

Also Published As

Publication number Publication date
DE2922059A1 (de) 1979-12-06
DE2922059C2 (de) 1986-09-11
AU4755079A (en) 1979-12-06
MX146565A (es) 1982-07-07
US4482110A (en) 1984-11-13
JPS54157999A (en) 1979-12-13
JPH0151400B2 (fr) 1989-11-02
BR7903329A (pt) 1979-12-11
GB2030098B (en) 1982-10-13
ZA792253B (en) 1980-05-28
GB2030098A (en) 1980-04-02
FR2427248B1 (fr) 1982-10-01
AR226158A1 (es) 1982-06-15
CA1171835A (fr) 1984-07-31
AU522258B2 (en) 1982-05-27

Similar Documents

Publication Publication Date Title
FR2427248A1 (fr) Aeronef mixte
US8141814B2 (en) Lighter-than-air vertical load lifting system
ES2101956T3 (es) Avion de despegue/aterrizaje vertical.
ES8402548A1 (es) Una maquina transportable sobre un vehiculo a motor y apta para elevar una barquilla a diferentes alturas.
GB1108240A (en) A vertical take-off and landing crane aircraft
FR2379432A1 (fr) Appareil d'atterrissage pour amener automatiquement au sol des charges a partir d'un avion volant a basse altitude
Carter Implication of heavy lift helicopter size effect trends and multilift options for filling the need
RU93001590A (ru) Вертостат
GB832542A (en) Improvements in vertical take-off aircraft
GB909923A (en) Improvements in aircraft
RU1723743C (ru) Аэросцепка
RU1837035C (ru) Несуща система летательного аппарата вертикального взлета и посадки
ELLIS An in-flight simulation of approach and landing of a STOL transport with adverse ground effect[Final Report]
BEVERT The ONERA Aeronautics Research Establishment in Cannes(France)
HUEBNER Design guide for load suspension points, slings, and aircraft hard points(Design criteria for load suspension points, slings, and lifting equipment used on military helicopters)[Final Report]
WILLIAMS Short-haul CTOL aircraft research(on reduced energy for commercial air transportation)
GB834731A (en) Improvements in or relating to aircraft
SNESHKO Stability and controllability of aircraft in the operational region of flight conditions((Russian book))(Ustoichivost' i upravliaemost' samoleta v ekspluatatsionnoi oblasti rezhimov poleta)
GARNETT Active arm(external cargo) stabilization system flight demonstration[Final Report, Jul. 1974- Apr. 1976]
ROTONDI Takeoff run of stol aircraft with vectored thrust is developed under the assumption of parabolic drag polar, constant thrust, constant friction coefficient, and a thrust-to-weight ratio of less than unity
Rybakov DEHYDRATION OF AIRCRAFT FUELS AND LUBRICANTS
Janovsky et al. Design optimization of an airbreathing aerospaceplane
RU1819797C (ru) Дирижабль
CARSON et al. Study of methane fuel for subsonic transport aircraft[Final Report, Jan. 1978- Aug. 1979]
Doyle LAUNCH, RECOVERY AND HANDLING SYSTEMS FOR VERTICAL TAKE-OFF AND LANDING UNMANNED AIRCRAFT OPERATING FROM SMALL SHIPS

Legal Events

Date Code Title Description
ST Notification of lapse