GB984955A - Nozzle for a jet engine - Google Patents

Nozzle for a jet engine

Info

Publication number
GB984955A
GB984955A GB286564A GB286564A GB984955A GB 984955 A GB984955 A GB 984955A GB 286564 A GB286564 A GB 286564A GB 286564 A GB286564 A GB 286564A GB 984955 A GB984955 A GB 984955A
Authority
GB
United Kingdom
Prior art keywords
downstream
fixed
jet
nozzle
jet engine
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
GB286564A
Inventor
William Shaw
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB286564A priority Critical patent/GB984955A/en
Priority to DER39515A priority patent/DE1242454B/en
Priority to FR999421A priority patent/FR1417902A/en
Publication of GB984955A publication Critical patent/GB984955A/en
Expired legal-status Critical Current

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
    • F02K1/004—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 by using one or more swivable nozzles rotating about their own axis

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Tires In General (AREA)
  • Control Of Turbines (AREA)

Abstract

984,955. Jet propelled aircraft. ROLLSROYCE Ltd. Jan. 22, 1964, No. 2865/64. Heading B7G. An aircraft is provided with gas turbine jet lift engines 14 each having an outlet nozzle 15 comprising a fixed upstream part 16, a downstream part 17 rotatable, e.g. by a chain 23, or a gear, meshing with a pinion 24, about the axis of the upstream part to vary the flow direction of the jet gases, and an inner member tapering in the downstream direction and having an upstream part 26 fixed to the part 16, and a downstream part 27 fixed, e.g. by struts 30, to the downstream part 17.
GB286564A 1964-01-22 1964-01-22 Nozzle for a jet engine Expired GB984955A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB286564A GB984955A (en) 1964-01-22 1964-01-22 Nozzle for a jet engine
DER39515A DE1242454B (en) 1964-01-22 1964-12-21 Jet nozzle with rotatable outlet part
FR999421A FR1417902A (en) 1964-01-22 1964-12-21 Jet engine nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB286564A GB984955A (en) 1964-01-22 1964-01-22 Nozzle for a jet engine

Publications (1)

Publication Number Publication Date
GB984955A true GB984955A (en) 1965-03-03

Family

ID=9747433

Family Applications (1)

Application Number Title Priority Date Filing Date
GB286564A Expired GB984955A (en) 1964-01-22 1964-01-22 Nozzle for a jet engine

Country Status (2)

Country Link
DE (1) DE1242454B (en)
GB (1) GB984955A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1257021B (en) * 1965-10-04 1967-12-21 Ver Flugtechnische Werke Ges M Airplane with a rotating hub nozzle
DE1288439B (en) * 1965-10-19 1969-01-30 Rolls Royce Airplane with jet engines, each with a large number of individual nozzles
GB2209314A (en) * 1987-09-02 1989-05-10 Manuel Munoz Saiz Lifting arrangement by direct thrust of the engine flow to vertical take-off aircraft
WO2008127260A1 (en) 2006-06-09 2008-10-23 Bell Helicopter Textron Inc. Engine exhaust system with directional nozzle

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1257021B (en) * 1965-10-04 1967-12-21 Ver Flugtechnische Werke Ges M Airplane with a rotating hub nozzle
DE1288439B (en) * 1965-10-19 1969-01-30 Rolls Royce Airplane with jet engines, each with a large number of individual nozzles
GB2209314A (en) * 1987-09-02 1989-05-10 Manuel Munoz Saiz Lifting arrangement by direct thrust of the engine flow to vertical take-off aircraft
WO2008127260A1 (en) 2006-06-09 2008-10-23 Bell Helicopter Textron Inc. Engine exhaust system with directional nozzle
EP2032829A1 (en) * 2006-06-09 2009-03-11 Bell Helicopter Textron Inc. Engine exhaust system with directional nozzle
EP2032829A4 (en) * 2006-06-09 2012-10-10 Bell Helicopter Textron Inc Engine exhaust system with directional nozzle

Also Published As

Publication number Publication date
DE1242454B (en) 1967-06-15

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