SE304182B - - Google Patents

Info

Publication number
SE304182B
SE304182B SE5031/67A SE503167A SE304182B SE 304182 B SE304182 B SE 304182B SE 5031/67 A SE5031/67 A SE 5031/67A SE 503167 A SE503167 A SE 503167A SE 304182 B SE304182 B SE 304182B
Authority
SE
Sweden
Application number
SE5031/67A
Inventor
S Markowski
Original Assignee
United Aircraft 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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of SE304182B publication Critical patent/SE304182B/xx

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • 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
    • 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
    • B64C29/0066—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 with horizontal jet and jet deflector
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Jet Pumps And Other Pumps (AREA)
SE5031/67A 1966-04-12 1967-04-11 SE304182B (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US542166A US3380661A (en) 1966-04-12 1966-04-12 Thrust deflector

Publications (1)

Publication Number Publication Date
SE304182B true SE304182B (de) 1968-09-16

Family

ID=24162620

Family Applications (1)

Application Number Title Priority Date Filing Date
SE5031/67A SE304182B (de) 1966-04-12 1967-04-11

Country Status (5)

Country Link
US (1) US3380661A (de)
DE (2) DE1300037B (de)
FR (1) FR1519221A (de)
GB (1) GB1173467A (de)
SE (1) SE304182B (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3792587A (en) * 1972-07-17 1974-02-19 Gen Electric Exhaust vectoring means
US4828173A (en) * 1987-05-22 1989-05-09 United Technologies Corporation Area controlled, thrust vectoring vane cascade
US4798328A (en) * 1987-05-22 1989-01-17 United Technologies Corporation Area controlled, thrust vectoring vane cascade with nutating control vane
US4760960A (en) * 1987-05-22 1988-08-02 United Technologies Corporation Linkage for area controlled, thrust vectoring vane cascade
FR2632722B1 (fr) * 1988-06-10 1993-09-03 Thomson Brandt Armements Dispositif destine a modifier la trajectoire d'un projectile par impulseurs pyrotechniques
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
US5082209A (en) * 1991-03-01 1992-01-21 United Technologies Corporation Thrust reverser assembly
CN100390397C (zh) * 2005-04-30 2008-05-28 张鸿元 空气压缩航空发动机

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1035487B (de) * 1957-05-07 1958-07-31 Adolf Hartl Sen Strahlduese fuer Flugzeuge mit einer Einrichtung zur Strahlumlenkung
US2995894A (en) * 1957-09-30 1961-08-15 Ryan Aeronautical Company Jet nozzle arrangement for side thrust control
FR1318785A (fr) * 1962-01-12 1963-02-22 Bertin & Cie Perfectionnements aux trompes à jets inducteurs minces, utilisables, notamment, à la sustentation
US3139153A (en) * 1962-04-02 1964-06-30 Remer Edgar M De Jet noise suppressor
GB1060051A (en) * 1965-01-11 1967-02-22 Rolls Royce Improvements in or relating to gas turbine engines
SU507322A1 (ru) * 1973-07-26 1976-03-25 Московский Научно-Исследовательский Институт Косметологии Регул тор гормонального обмена кожи
US3984566A (en) * 1974-02-25 1976-10-05 Scott Eugene J Van Method of alleviating the symptoms of dandruff
US4380549A (en) * 1975-07-23 1983-04-19 Scott Eugene J Van Topical treatment of dry skin
US5654266A (en) * 1992-02-10 1997-08-05 Chen; Chung-Ho Composition for tissues to sustain viability and biological functions in surgery and storage
WO2001013877A1 (en) * 1999-08-20 2001-03-01 Unilever Plc A method for reducing skin irritation and sting from weak carboxylic acid

Also Published As

Publication number Publication date
US3380661A (en) 1968-04-30
DE1300037B (de) 1969-07-24
DE1481676A1 (de) 1969-03-20
GB1173467A (en) 1969-12-10
FR1519221A (fr) 1968-03-29

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