IT8019775A0 - Effusore di spinta per motore di propulsione a reazione. - Google Patents

Effusore di spinta per motore di propulsione a reazione.

Info

Publication number
IT8019775A0
IT8019775A0 IT8019775A IT1977580A IT8019775A0 IT 8019775 A0 IT8019775 A0 IT 8019775A0 IT 8019775 A IT8019775 A IT 8019775A IT 1977580 A IT1977580 A IT 1977580A IT 8019775 A0 IT8019775 A0 IT 8019775A0
Authority
IT
Italy
Prior art keywords
effuser
thrust
jet propulsion
propulsion engine
engine
Prior art date
Application number
IT8019775A
Other languages
English (en)
Inventor
Leonard John Rodgers
Original Assignee
Rolls Royce
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 filed Critical Rolls Royce
Publication of IT8019775A0 publication Critical patent/IT8019775A0/it

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
    • 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1223—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)
IT8019775A 1979-02-19 1980-02-07 Effusore di spinta per motore di propulsione a reazione. IT8019775A0 (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB7901281.1A GB7901281D0 (en) 1979-02-19 1979-02-19 Thrust nozzle for a jet propulsion engine

Publications (1)

Publication Number Publication Date
IT8019775A0 true IT8019775A0 (it) 1980-02-07

Family

ID=10502504

Family Applications (1)

Application Number Title Priority Date Filing Date
IT8019775A IT8019775A0 (it) 1979-02-19 1980-02-07 Effusore di spinta per motore di propulsione a reazione.

Country Status (4)

Country Link
DE (1) DE3005804B3 (it)
FR (1) FR2849903A1 (it)
GB (2) GB7901281D0 (it)
IT (1) IT8019775A0 (it)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB719268A (en) * 1951-07-31 1954-12-01 Otto Reder Improvements relating to jet propulsion units for aerial or submarine use

Also Published As

Publication number Publication date
DE3005804B3 (de) 2004-04-15
GB7901281D0 (en) 2003-11-12
GB8002303D0 (en) 2003-11-12
FR2849903A1 (fr) 2004-07-16

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