CA998376A - Airfoil with fluid flow injector means - Google Patents

Airfoil with fluid flow injector means

Info

Publication number
CA998376A
CA998376A CA205,228A CA205228A CA998376A CA 998376 A CA998376 A CA 998376A CA 205228 A CA205228 A CA 205228A CA 998376 A CA998376 A CA 998376A
Authority
CA
Canada
Prior art keywords
airfoil
fluid flow
injector means
flow injector
fluid
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
CA205,228A
Other languages
English (en)
Inventor
Edward M. Petrushka
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.)
Boeing North American Inc
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 CA998376A publication Critical patent/CA998376A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Toys (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Feedback Control In General (AREA)
CA205,228A 1973-09-05 1974-07-19 Airfoil with fluid flow injector means Expired CA998376A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US394581A US3860200A (en) 1973-09-05 1973-09-05 Airfoil

Publications (1)

Publication Number Publication Date
CA998376A true CA998376A (en) 1976-10-12

Family

ID=23559560

Family Applications (1)

Application Number Title Priority Date Filing Date
CA205,228A Expired CA998376A (en) 1973-09-05 1974-07-19 Airfoil with fluid flow injector means

Country Status (12)

Country Link
US (1) US3860200A (sv)
JP (1) JPS5526038B2 (sv)
BR (1) BR7407400D0 (sv)
CA (1) CA998376A (sv)
DE (1) DE2442036A1 (sv)
ES (1) ES429779A1 (sv)
FR (1) FR2242293B1 (sv)
GB (1) GB1468549A (sv)
IL (1) IL45349A (sv)
IT (1) IT1018972B (sv)
SE (1) SE412734B (sv)
SU (1) SU541426A3 (sv)

Families Citing this family (17)

* 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
US5697468A (en) * 1994-10-04 1997-12-16 Flarecraft Corporation Spoiler system for ground effect vehicles
US7802756B2 (en) * 2000-02-14 2010-09-28 Aerovironment Inc. Aircraft control system
GB2397809A (en) * 2002-12-21 2004-08-04 Richard Cyril Adkins V/STOL aircraft with an ejector for providing vertical lift
FR2873096B1 (fr) * 2004-07-15 2007-11-23 Airbus France Sas Avion multimoteur
US7837141B2 (en) * 2006-03-22 2010-11-23 The Boeing Company Reaction drive rotor/wing variable area nozzle
DE102009010150B4 (de) * 2009-02-23 2013-09-19 Airbus Operations Gmbh System und Verfahren zur Notbelüftung einer Flugzeugkabine
US9573690B2 (en) * 2011-09-06 2017-02-21 Honeywell International Inc. Thrust recovery outflow valve with a single bi-fold door and method of controlling aircraft cabin pressure
US8998132B2 (en) * 2011-11-30 2015-04-07 Lockheed Martin Corporation Aerodynamic wing load distribution control
KR101287624B1 (ko) 2013-02-25 2013-07-23 주식회사 네스앤텍 착륙이 용이한 무인비행체
AU2016338382B2 (en) 2015-09-02 2021-04-01 Jetoptera, Inc. Ejector and airfoil configurations
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
RU2630270C2 (ru) * 2016-02-09 2017-09-06 Степан Валентинович Суворов Самолет вертикального взлета и посадки
WO2019062256A1 (zh) * 2017-09-29 2019-04-04 清华大学 一种基于倾转涵道的单升力涵道垂直起降飞机
CN109911180A (zh) * 2019-04-15 2019-06-21 重庆恩斯特龙通用航空技术研究院有限公司 一种轻型飞机襟翼操纵装置

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL110393C (sv) * 1955-11-29 1965-01-15 Bertin & Cie
US3045947A (en) * 1959-04-24 1962-07-24 Bertin & Cie Ejectors, particularly for producing lift in aircraft
FR94023E (fr) * 1967-05-24 1969-06-20 Bertin & Cie Systeme sustentateur ou propulso sustentateur pour aéronefs.
US3664611A (en) * 1969-12-17 1972-05-23 Flight Dynamics Res Aerodynamic vehicle

Also Published As

Publication number Publication date
GB1468549A (en) 1977-03-30
DE2442036A1 (de) 1975-04-10
SE7411190L (sv) 1975-03-06
SE412734B (sv) 1980-03-17
JPS5054100A (sv) 1975-05-13
JPS5526038B2 (sv) 1980-07-10
AU7159474A (en) 1976-01-29
SU541426A3 (ru) 1976-12-30
BR7407400D0 (pt) 1975-07-08
IL45349A (en) 1980-02-29
IT1018972B (it) 1977-10-20
FR2242293B1 (sv) 1979-10-12
ES429779A1 (es) 1976-08-16
US3860200A (en) 1975-01-14
FR2242293A1 (sv) 1975-03-28
IL45349A0 (en) 1976-07-30

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