IT1016113B - Perfezionamento nei sistemi di controllo di portanza per aeromobi li - Google Patents

Perfezionamento nei sistemi di controllo di portanza per aeromobi li

Info

Publication number
IT1016113B
IT1016113B IT51307/74A IT5130774A IT1016113B IT 1016113 B IT1016113 B IT 1016113B IT 51307/74 A IT51307/74 A IT 51307/74A IT 5130774 A IT5130774 A IT 5130774A IT 1016113 B IT1016113 B IT 1016113B
Authority
IT
Italy
Prior art keywords
aircraft
improvement
control systems
lift control
lift
Prior art date
Application number
IT51307/74A
Other languages
English (en)
Original Assignee
Rockwell International Corp
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 Rockwell International Corp filed Critical Rockwell International Corp
Application granted granted Critical
Publication of IT1016113B publication Critical patent/IT1016113B/it

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
    • B64C29/0091—Accessories not provided for elsewhere

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Toys (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Automatic Assembly (AREA)
IT51307/74A 1973-06-28 1974-05-30 Perfezionamento nei sistemi di controllo di portanza per aeromobi li IT1016113B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00374429A US3831887A (en) 1973-06-28 1973-06-28 Aircraft control methods

Publications (1)

Publication Number Publication Date
IT1016113B true IT1016113B (it) 1977-05-30

Family

ID=23476782

Family Applications (1)

Application Number Title Priority Date Filing Date
IT51307/74A IT1016113B (it) 1973-06-28 1974-05-30 Perfezionamento nei sistemi di controllo di portanza per aeromobi li

Country Status (11)

Country Link
US (1) US3831887A (it)
JP (1) JPS5037199A (it)
BR (1) BR7405321A (it)
CA (1) CA1003387A (it)
DE (1) DE2426565A1 (it)
ES (1) ES427772A1 (it)
FR (1) FR2235045B1 (it)
GB (1) GB1458059A (it)
IL (1) IL44919A (it)
IT (1) IT1016113B (it)
SE (1) SE412735B (it)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4391424A (en) * 1976-08-30 1983-07-05 Ball Brothers Method and structure for airfoil thrust and lift control
GB2127756A (en) * 1982-09-24 1984-04-18 John Lloyd Protection for under-carriage of air liners
US5016837A (en) * 1987-06-25 1991-05-21 Venturi Applications, Inc. Venturi enhanced airfoil
US5062588A (en) * 1989-02-08 1991-11-05 Boeing Of Canada Ltd. Segmented rotatable nozzles
US5076512A (en) * 1989-02-08 1991-12-31 Boeing Canada Ltd. Ventral segmented nozzles for promoting rapid temperature and pressure decay
GB2469614B (en) * 1989-03-14 2011-03-23 British Aerospace Jet Propulsion Efflux Outlets
US5697468A (en) * 1994-10-04 1997-12-16 Flarecraft Corporation Spoiler system for ground effect vehicles
CN1435355B (zh) * 2002-12-04 2011-01-12 韩国庆 轻型前掠翼喷气机及其用途
US8636241B2 (en) 2005-04-20 2014-01-28 Richard H. Lugg Hybrid jet/electric VTOL aircraft
US7568348B2 (en) * 2005-11-28 2009-08-04 Aerojet-General Corporation Nozzle assembly for rocket and ramjet applications
US7837141B2 (en) * 2006-03-22 2010-11-23 The Boeing Company Reaction drive rotor/wing variable area nozzle
US8079546B2 (en) * 2009-06-18 2011-12-20 The Charles Stark Draper Laboratory, Inc. Samara wing
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
USD868627S1 (en) 2018-04-27 2019-12-03 Jetoptera, Inc. Flying car
WO2017065858A2 (en) 2015-09-02 2017-04-20 Jetoptera, Inc. Ejector and airfoil configurations
US11001378B2 (en) * 2016-08-08 2021-05-11 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
AU2017274156B2 (en) * 2016-03-11 2022-10-13 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2964905A (en) * 1960-12-20 Aircraft control means
US2945641A (en) * 1956-09-20 1960-07-19 Fairey Aviat Ltd Aircraft with wing containing lifting jets
US3045947A (en) * 1959-04-24 1962-07-24 Bertin & Cie Ejectors, particularly for producing lift in aircraft
FR1267920A (fr) * 1960-06-15 1961-07-28 Snecma Dispositif de sustentation pour aérodynes, et plus particulièrement pour aérodynes à décollage vertical sans changement d'assiette
GB1251217A (it) * 1968-11-14 1971-10-27
US3618875A (en) * 1969-02-24 1971-11-09 Gen Electric V/stol aircraft
US3664611A (en) * 1969-12-17 1972-05-23 Flight Dynamics Res Aerodynamic vehicle
US3770227A (en) * 1971-09-10 1973-11-06 Us Air Force Jet wing with multiple thrust augmentors

Also Published As

Publication number Publication date
ES427772A1 (es) 1976-08-01
SE7408500L (it) 1974-12-30
DE2426565A1 (de) 1975-01-16
IL44919A (en) 1977-05-31
BR7405321A (pt) 1976-02-24
GB1458059A (en) 1976-12-08
AU6885074A (en) 1975-11-13
FR2235045A1 (it) 1975-01-24
IL44919A0 (en) 1974-12-31
JPS5037199A (it) 1975-04-07
FR2235045B1 (it) 1979-10-12
SE412735B (sv) 1980-03-17
CA1003387A (en) 1977-01-11
US3831887A (en) 1974-08-27

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