GB918778A - Improvements in or relating to gas-turbine engines - Google Patents

Improvements in or relating to gas-turbine engines

Info

Publication number
GB918778A
GB918778A GB21573/59A GB2157359A GB918778A GB 918778 A GB918778 A GB 918778A GB 21573/59 A GB21573/59 A GB 21573/59A GB 2157359 A GB2157359 A GB 2157359A GB 918778 A GB918778 A GB 918778A
Authority
GB
United Kingdom
Prior art keywords
duct
pass
exhaust
wall
downstream
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
GB21573/59A
Other languages
English (en)
Inventor
Valentine Tindale John
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 GB21573/59A priority Critical patent/GB918778A/en
Priority to US33498A priority patent/US3196608A/en
Priority to BE592008A priority patent/BE592008A/fr
Priority to NL252740A priority patent/NL127556C/nl
Priority to ES0259033A priority patent/ES259033A1/es
Priority to CH699460A priority patent/CH384290A/de
Publication of GB918778A publication Critical patent/GB918778A/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
    • F02K1/38—Introducing air inside the jet
    • F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Exhaust Gas After Treatment (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
GB21573/59A 1959-06-23 1959-06-23 Improvements in or relating to gas-turbine engines Expired GB918778A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
GB21573/59A GB918778A (en) 1959-06-23 1959-06-23 Improvements in or relating to gas-turbine engines
US33498A US3196608A (en) 1959-06-23 1960-06-02 Apparatus to admix by-pass air with exhaust gases in a by-pass gas-turbine engine
BE592008A BE592008A (fr) 1959-06-23 1960-06-17 Perfectionnements aux moteurs à turbine à gaz.
NL252740A NL127556C (US06262066-20010717-C00315.png) 1959-06-23 1960-06-17
ES0259033A ES259033A1 (es) 1959-06-23 1960-06-18 Un motor de derivaciën
CH699460A CH384290A (de) 1959-06-23 1960-06-20 Gasturbinenanlage mit Nebenstromkanal

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB21573/59A GB918778A (en) 1959-06-23 1959-06-23 Improvements in or relating to gas-turbine engines

Publications (1)

Publication Number Publication Date
GB918778A true GB918778A (en) 1963-02-20

Family

ID=10165187

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21573/59A Expired GB918778A (en) 1959-06-23 1959-06-23 Improvements in or relating to gas-turbine engines

Country Status (6)

Country Link
US (1) US3196608A (US06262066-20010717-C00315.png)
BE (1) BE592008A (US06262066-20010717-C00315.png)
CH (1) CH384290A (US06262066-20010717-C00315.png)
ES (1) ES259033A1 (US06262066-20010717-C00315.png)
GB (1) GB918778A (US06262066-20010717-C00315.png)
NL (1) NL127556C (US06262066-20010717-C00315.png)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2161862A (en) * 1983-05-27 1986-01-22 Pierre Giraud Double flow turbine engine equipped with a thrust reverser
GB2259954A (en) * 1991-09-27 1993-03-31 Short Brothers Plc Ducted fan turbine engine nozzle assembly

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3508403A (en) * 1968-03-28 1970-04-28 Gen Electric Turbofan engines
SE320225B (US06262066-20010717-C00315.png) * 1968-06-17 1970-02-02 Svenska Flygmotorer Ab
DE2540537C2 (de) * 1975-09-11 1977-11-10 Motoren- und Turbinen-Union München GmbH, 8000 München Gasturbinenstrahltriebwerk zum Antrieb und zur Steuerung eines Flugzeugs
US5265408A (en) * 1992-02-13 1993-11-30 Allied-Signal Inc. Exhaust eductor cooling system
DE10145489B4 (de) * 2001-09-14 2008-11-06 Mtu Aero Engines Gmbh Anordnung zum Vermischen von zwei ursprünglich getrennt geführten Fluidströmen in einem Zweikreis-Strahltriebwerk
US6651929B2 (en) * 2001-10-29 2003-11-25 Pratt & Whitney Canada Corp. Passive cooling system for auxiliary power unit installation
US20080072566A1 (en) * 2006-09-27 2008-03-27 Pratt & Whitney Canada Corp. Bleed holes oriented with gaspath and flared for noise reduction
FR3088373B1 (fr) * 2018-11-09 2021-03-19 Safran Nacelles Joint d’etancheite pour nacelle de turboreacteur d’aeronef

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1382690A (en) * 1917-10-27 1921-06-28 Stokes Charles Lawrence Apparatus for silencing and exhausting gases and method therffor
US2088591A (en) * 1935-12-27 1937-08-03 Atlantic Refining Co Mixing device
US2308059A (en) * 1941-04-03 1943-01-12 Ammiel F Decker Exhaust device for internal combustion engines
US2588532A (en) * 1943-05-12 1952-03-11 Allis Chalmers Mfg Co Jet propulsion unit
US2426833A (en) * 1943-11-05 1947-09-02 Power Jets Res & Dev Ltd Apparatus for mixing fluids
US2626501A (en) * 1944-10-07 1953-01-27 Turbolectric Corp Gas turbine power plant having compressor, turbine, and hollow shaft therebetween
US2653446A (en) * 1948-06-05 1953-09-29 Lockheed Aircraft Corp Compressor and fuel control system for high-pressure gas turbine power plants
US2600733A (en) * 1950-12-06 1952-06-17 Standard Oil Co Gas mixing apparatus
GB777803A (en) * 1953-01-15 1957-06-26 Pye Ltd Improvements in or relating to television receivers
GB760493A (en) * 1954-01-07 1956-10-31 Coventry Climax Eng Ltd Improvements in exhaust systems for internal combustion engines
US2978865A (en) * 1956-02-06 1961-04-11 Curtiss Wright Corp Turbo fan exhaust mixing device
GB852829A (en) * 1957-04-03 1960-11-02 Rolls Royce Improvements in or relating to gas-turbine jet propulsion engines
US2999672A (en) * 1958-04-09 1961-09-12 Curtiss Wright Corp Fluid mixing apparatus
US3048376A (en) * 1958-04-09 1962-08-07 Curtiss Wright Corp Fluid mixing apparatus
US2984967A (en) * 1959-01-27 1961-05-23 Alfred M Caddell Exhaust temperature air-cooling system

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2161862A (en) * 1983-05-27 1986-01-22 Pierre Giraud Double flow turbine engine equipped with a thrust reverser
GB2259954A (en) * 1991-09-27 1993-03-31 Short Brothers Plc Ducted fan turbine engine nozzle assembly
GB2259954B (en) * 1991-09-27 1994-12-14 Short Brothers Plc Ducted fan turbine engine nozzle assembly

Also Published As

Publication number Publication date
BE592008A (fr) 1960-10-17
CH384290A (de) 1964-11-15
ES259033A1 (es) 1960-12-01
US3196608A (en) 1965-07-27
NL127556C (US06262066-20010717-C00315.png) 1969-11-17

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