GB1212743A - A lift and propulsion system on an aircraft - Google Patents

A lift and propulsion system on an aircraft

Info

Publication number
GB1212743A
GB1212743A GB25023/68A GB2502368A GB1212743A GB 1212743 A GB1212743 A GB 1212743A GB 25023/68 A GB25023/68 A GB 25023/68A GB 2502368 A GB2502368 A GB 2502368A GB 1212743 A GB1212743 A GB 1212743A
Authority
GB
United Kingdom
Prior art keywords
conduits
fairings
conduit
aircraft
slots
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.)
Expired
Application number
GB25023/68A
Other languages
English (en)
Inventor
Jean Henri Bertin
Marcel Pierre Le Nabour
Jean Lucien Charles Cayla
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.)
Bertin Technologies SAS
Original Assignee
Bertin et Cie SA
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
Priority claimed from FR107669A external-priority patent/FR1548297A/fr
Application filed by Bertin et Cie SA filed Critical Bertin et Cie SA
Publication of GB1212743A publication Critical patent/GB1212743A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B64C29/005—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors the motors being fixed relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/38—Jet flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
GB25023/68A 1967-05-24 1968-05-24 A lift and propulsion system on an aircraft Expired GB1212743A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR107669A FR1548297A (https=) 1967-05-24 1967-05-24
FR141237A FR94023E (fr) 1967-05-24 1968-02-26 Systeme sustentateur ou propulso sustentateur pour aéronefs.

Publications (1)

Publication Number Publication Date
GB1212743A true GB1212743A (en) 1970-11-18

Family

ID=26176744

Family Applications (1)

Application Number Title Priority Date Filing Date
GB25023/68A Expired GB1212743A (en) 1967-05-24 1968-05-24 A lift and propulsion system on an aircraft

Country Status (6)

Country Link
US (1) US3545701A (https=)
BE (1) BE715615A (https=)
CH (1) CH489390A (https=)
DE (1) DE1756465C3 (https=)
FR (1) FR94023E (https=)
GB (1) GB1212743A (https=)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2287454C1 (ru) * 2005-04-26 2006-11-20 Владимир Степанович Григорчук Транспортный самолет
RU2373110C1 (ru) * 2008-06-19 2009-11-20 Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Аэродинамический орган управления летательного аппарата
CN106628171A (zh) * 2016-12-01 2017-05-10 向仲宇 一种分割式可改变扑翼面积的扑翼飞行器
EP4019408A1 (en) * 2020-12-22 2022-06-29 Hyundai Motor Company Air mobility vehicle

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3666209A (en) * 1970-02-24 1972-05-30 Boeing Co V/stol aircraft with variable tilt wing
US3770227A (en) * 1971-09-10 1973-11-06 Us Air Force Jet wing with multiple thrust augmentors
US3830451A (en) * 1973-06-28 1974-08-20 Rockwell International Corp Aircraft control system
US3860200A (en) * 1973-09-05 1975-01-14 Rockwell International Corp Airfoil
US4017041A (en) * 1976-01-12 1977-04-12 Nelson Wilbur C Airfoil tip vortex control
US4442986A (en) * 1982-08-30 1984-04-17 The United States Of America As Represented By The Secretary Of The Navy Leading edge augmentor wing-in-ground effect vehicle
US5076512A (en) * 1989-02-08 1991-12-31 Boeing Canada Ltd. Ventral segmented nozzles for promoting rapid temperature and pressure decay
US5062588A (en) * 1989-02-08 1991-11-05 Boeing Of Canada Ltd. Segmented rotatable nozzles
RU2120396C1 (ru) * 1997-01-06 1998-10-20 Николай Александрович Дученко Движитель
GB0301370D0 (en) * 2003-01-22 2003-02-19 Secr Defence A wing for a compound helicopter
DE10313729B4 (de) * 2003-03-27 2007-11-29 Airbus Deutschland Gmbh Luftauslaßventil für ein Flugzeug
US20050116087A1 (en) * 2003-06-11 2005-06-02 Page John S.Jr. Aircraft converts drag to lift
US20080230656A1 (en) * 2006-04-11 2008-09-25 Moshe Kretchmer Aircraft wings having hinged vanes and aircraft having said wings
FR2911116B1 (fr) * 2007-01-05 2009-02-06 Airbus France Sas Dispositif de sortie d'air pour un aeronef
FR2915733B1 (fr) * 2007-05-04 2009-06-05 Airbus France Sas Dispositif de sortie d'air mobile pour un aeronef
US8336828B2 (en) * 2009-11-12 2012-12-25 The Boeing Company Traversing jet actuator
FR2990926B1 (fr) * 2012-05-22 2014-11-28 Eurocopter France Moyen de stabilisation en tangage et aeronef a voilure tournante muni d'un tel moyen
US10370100B2 (en) * 2015-03-24 2019-08-06 United States Of America As Represented By The Administrator Of Nasa Aerodynamically actuated thrust vectoring devices
USD868627S1 (en) 2018-04-27 2019-12-03 Jetoptera, Inc. Flying car
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
EP4306789A3 (en) 2015-09-02 2024-06-12 Jetoptera, Inc. Fluidic propulsive system
US10669026B2 (en) * 2016-04-01 2020-06-02 Albert Aguilar Lift cell modules and lift pods
US10106246B2 (en) 2016-06-10 2018-10-23 Coflow Jet, LLC Fluid systems that include a co-flow jet
US10315754B2 (en) 2016-06-10 2019-06-11 Coflow Jet, LLC Fluid systems that include a co-flow jet
WO2019056053A1 (en) * 2017-09-22 2019-03-28 AMSL Innovations Pty Ltd TILT ACTUATION SYSTEM FOR VERTICAL TAKE-OFF AND LANDING AIRCRAFT (ADAV)
US10683076B2 (en) 2017-10-31 2020-06-16 Coflow Jet, LLC Fluid systems that include a co-flow jet
US11293293B2 (en) 2018-01-22 2022-04-05 Coflow Jet, LLC Turbomachines that include a casing treatment
US11111025B2 (en) 2018-06-22 2021-09-07 Coflow Jet, LLC Fluid systems that prevent the formation of ice
US11920617B2 (en) 2019-07-23 2024-03-05 Coflow Jet, LLC Fluid systems and methods that address flow separation
WO2021257271A1 (en) 2020-06-17 2021-12-23 Coflow Jet, LLC Fluid systems having a variable configuration
WO2022204278A1 (en) 2021-03-26 2022-09-29 Coflow Jet, LLC Wind turbine blades and wind turbine systems that include a co-flow jet
CN117858832A (zh) * 2021-05-19 2024-04-09 杰托普特拉股份有限公司 自适应流体推进系统

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2287454C1 (ru) * 2005-04-26 2006-11-20 Владимир Степанович Григорчук Транспортный самолет
RU2373110C1 (ru) * 2008-06-19 2009-11-20 Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Аэродинамический орган управления летательного аппарата
CN106628171A (zh) * 2016-12-01 2017-05-10 向仲宇 一种分割式可改变扑翼面积的扑翼飞行器
EP4019408A1 (en) * 2020-12-22 2022-06-29 Hyundai Motor Company Air mobility vehicle
US11891186B2 (en) 2020-12-22 2024-02-06 Hyundai Motor Company Air mobility vehicle with a cooling air intake flap positioned below a rotary wing

Also Published As

Publication number Publication date
CH489390A (fr) 1970-04-30
DE1756465A1 (de) 1970-04-02
BE715615A (https=) 1968-11-25
FR94023E (fr) 1969-06-20
US3545701A (en) 1970-12-08
DE1756465B2 (de) 1973-03-29
DE1756465C3 (de) 1973-10-18

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees