BR7405342D0 - Sistema de aviao desenvolvendo sustentacao aerodinamica e processo para operar o mesmo - Google Patents

Sistema de aviao desenvolvendo sustentacao aerodinamica e processo para operar o mesmo

Info

Publication number
BR7405342D0
BR7405342D0 BR5342/74A BR534274A BR7405342D0 BR 7405342 D0 BR7405342 D0 BR 7405342D0 BR 5342/74 A BR5342/74 A BR 5342/74A BR 534274 A BR534274 A BR 534274A BR 7405342 D0 BR7405342 D0 BR 7405342D0
Authority
BR
Brazil
Prior art keywords
operate
same
aviation system
system developing
aerodynamic support
Prior art date
Application number
BR5342/74A
Other languages
English (en)
Other versions
BR7405342A (pt
Inventor
J Fosness
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
Publication of BR7405342D0 publication Critical patent/BR7405342D0/pt
Publication of BR7405342A publication Critical patent/BR7405342A/pt

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)
  • Jet Pumps And Other Pumps (AREA)
  • Aeration Devices For Treatment Of Activated Polluted Sludge (AREA)
BR5342/74A 1973-06-28 1974-06-28 Sistema de aviao desenvolvendo sustentacao aerodinamica e processo para operar o mesmo BR7405342A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00374744A US3830451A (en) 1973-06-28 1973-06-28 Aircraft control system

Publications (2)

Publication Number Publication Date
BR7405342D0 true BR7405342D0 (pt) 1975-01-07
BR7405342A BR7405342A (pt) 1976-02-24

Family

ID=23478049

Family Applications (1)

Application Number Title Priority Date Filing Date
BR5342/74A BR7405342A (pt) 1973-06-28 1974-06-28 Sistema de aviao desenvolvendo sustentacao aerodinamica e processo para operar o mesmo

Country Status (11)

Country Link
US (1) US3830451A (pt)
JP (1) JPS5037200A (pt)
BR (1) BR7405342A (pt)
CA (1) CA1003386A (pt)
DE (1) DE2427406C2 (pt)
ES (1) ES427773A1 (pt)
FR (1) FR2235046B1 (pt)
GB (1) GB1458060A (pt)
IL (1) IL44920A (pt)
IT (1) IT1018684B (pt)
SE (1) SE412736B (pt)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110147084A (zh) * 2014-07-09 2019-08-20 波音公司 用于操作柔性制造系统的基于计量的系统

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US8016233B2 (en) * 2006-01-30 2011-09-13 The Boeing Company Aircraft configuration
US8628040B2 (en) 2006-01-30 2014-01-14 The Boeing Company Aircraft configuration
US7900865B2 (en) 2006-12-19 2011-03-08 The Boeing Company Airplane configuration
US8066220B2 (en) * 2007-04-23 2011-11-29 Kirstein Joshua M Aircraft engine balanced thrust vectoring system
US20110215204A1 (en) * 2007-06-20 2011-09-08 General Electric Company System and method for generating thrust
US8451144B2 (en) * 2009-02-04 2013-05-28 Honeywell International Inc. Flaps overspeed advisory system
CN102009743B (zh) * 2010-07-01 2013-06-05 北京航空航天大学 基于吹气的机身大迎角俯仰力矩控制方法
RU2534480C1 (ru) * 2013-06-26 2014-11-27 Виктор Семенович Савченков Способ увеличения подъёмной силы крыла самолёта
RU2651947C2 (ru) * 2016-05-04 2018-04-24 Борис Никифорович Сушенцев Реактивный самолет с укороченным либо вертикальным взлетом и посадкой (варианты)
CN106428560A (zh) * 2016-10-28 2017-02-22 中国人民解放军总参谋部第六十研究所 一种亚音速大机动靶机的鸭式气动布局
CN111727312B (zh) * 2017-06-27 2023-07-14 杰拓普特拉股份有限公司 航空飞行器垂直起降系统的配置
WO2019191460A1 (en) * 2018-03-29 2019-10-03 AvionOne Innovations, LLC Load-bearing ducting members for aircraft lift and thrust

Family Cites Families (9)

* 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
SE313504B (pt) * 1966-11-29 1969-08-11 Saab Ab
FR94023E (fr) * 1967-05-24 1969-06-20 Bertin & Cie Systeme sustentateur ou propulso sustentateur pour aéronefs.
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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110147084A (zh) * 2014-07-09 2019-08-20 波音公司 用于操作柔性制造系统的基于计量的系统
CN110147084B (zh) * 2014-07-09 2022-09-06 波音公司 用于操作柔性制造系统的基于计量的系统

Also Published As

Publication number Publication date
ES427773A1 (es) 1976-08-01
SE7408501L (pt) 1974-12-30
GB1458060A (en) 1976-12-08
AU6884874A (en) 1975-11-13
JPS5037200A (pt) 1975-04-07
DE2427406C2 (de) 1986-06-12
FR2235046B1 (pt) 1979-10-12
SE412736B (sv) 1980-03-17
FR2235046A1 (pt) 1975-01-24
IT1018684B (it) 1977-10-20
CA1003386A (en) 1977-01-11
IL44920A (en) 1977-05-31
BR7405342A (pt) 1976-02-24
DE2427406A1 (de) 1975-03-13
IL44920A0 (en) 1974-12-31
US3830451A (en) 1974-08-20

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