BE595414A - Tuyère ayant la forme d'un nez de requin et pourvue d'un déflecteur de poussée. - Google Patents

Tuyère ayant la forme d'un nez de requin et pourvue d'un déflecteur de poussée.

Info

Publication number
BE595414A
BE595414A BE595414A BE595414A BE595414A BE 595414 A BE595414 A BE 595414A BE 595414 A BE595414 A BE 595414A BE 595414 A BE595414 A BE 595414A BE 595414 A BE595414 A BE 595414A
Authority
BE
Belgium
Prior art keywords
shark
nose
nozzle
shape
thrust deflector
Prior art date
Application number
BE595414A
Other languages
English (en)
Inventor
William Herman Sens
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 BE595414A publication Critical patent/BE595414A/fr

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
    • 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
    • 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
    • F02K1/002—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
    • F02K1/006—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 within one plane only

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Exhaust Silencers (AREA)
  • Control Of Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
BE595414A 1959-10-05 1960-09-26 Tuyère ayant la forme d'un nez de requin et pourvue d'un déflecteur de poussée. BE595414A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US844328A US3019601A (en) 1959-10-05 1959-10-05 Pen-shaped nozzle with thrust deflector

Publications (1)

Publication Number Publication Date
BE595414A true BE595414A (fr) 1961-03-27

Family

ID=25292403

Family Applications (1)

Application Number Title Priority Date Filing Date
BE595414A BE595414A (fr) 1959-10-05 1960-09-26 Tuyère ayant la forme d'un nez de requin et pourvue d'un déflecteur de poussée.

Country Status (6)

Country Link
US (1) US3019601A (fr)
BE (1) BE595414A (fr)
CH (1) CH399916A (fr)
DE (1) DE1159769B (fr)
GB (1) GB900040A (fr)
NL (2) NL255475A (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3080711A (en) * 1960-01-06 1963-03-12 James F Connors Penshape exhaust nozzle for supersonic engine
GB918189A (en) * 1960-07-01 1963-02-13 Rolls Royce Jet propulsion nozzle
US4000610A (en) * 1975-04-28 1977-01-04 General Electric Company Flight maneuverable nozzle for gas turbine engines
US4000611A (en) * 1975-07-01 1977-01-04 General Electric Company Variable area, load balancing nozzle
FR2537657A1 (fr) * 1982-12-08 1984-06-15 Snecma Tuyere a section variable pour un turboreacteur et avion comportant un tel equipement
US6000635A (en) * 1995-10-02 1999-12-14 Lockheed Martin Corporation Exhaust nozzle for a turbojet engine
EP0959000A1 (fr) * 1998-03-10 1999-11-24 Manuel Munoz Saiz Dispositif pour augmenter la sustentation et réduire la trainée pour aéronefs
US9181899B2 (en) * 2008-08-27 2015-11-10 General Electric Company Variable slope exhaust nozzle
US9810178B2 (en) 2015-08-05 2017-11-07 General Electric Company Exhaust nozzle with non-coplanar and/or non-axisymmetric shape
RU2668309C1 (ru) * 2017-07-20 2018-09-28 Публичное акционерное общество "ОДК - Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Выхлопное сопло турбореактивного двигателя летательного аппарата
CN110496713B (zh) * 2019-09-20 2024-06-18 常熟华东汽车有限公司 除雪车用的矢量喷口结构

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2734698A (en) * 1956-02-14 Aikplane control surface and jet
US2657575A (en) * 1947-08-21 1953-11-03 Harry J Allen Asymmetric adjustable supersonic nozzle
BE498317A (fr) * 1949-10-06
US2840325A (en) * 1951-12-05 1958-06-24 Rolls Royce Aircraft structure
US2758805A (en) * 1952-03-18 1956-08-14 Northrop Aircraft Inc Blast deflector arrangement for jet propelled aircraft
US2866610A (en) * 1956-04-10 1958-12-30 John E M Taylor Aircraft jet thrust control
US2951660A (en) * 1956-06-25 1960-09-06 James V Giliberty Method and means for controlling the jet thrust of an aircraft
US2956759A (en) * 1957-02-21 1960-10-18 English Electric Co Ltd Aircraft wings incorporating power installation for propulsion
US2944765A (en) * 1958-09-01 1960-07-12 Bristol Siddeley Engines Ltd Jet-propelled aircraft

Also Published As

Publication number Publication date
CH399916A (de) 1965-09-30
DE1159769B (de) 1963-12-19
GB900040A (en) 1962-07-04
US3019601A (en) 1962-02-06
NL121474C (fr)
NL255475A (fr)

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