[go: up one dir, main page]

GB2139288B - Exhaust mixer for bypass gas turbine aeroengines - Google Patents

Exhaust mixer for bypass gas turbine aeroengines

Info

Publication number
GB2139288B
GB2139288B GB08408565A GB8408565A GB2139288B GB 2139288 B GB2139288 B GB 2139288B GB 08408565 A GB08408565 A GB 08408565A GB 8408565 A GB8408565 A GB 8408565A GB 2139288 B GB2139288 B GB 2139288B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
bypass gas
exhaust mixer
turbine aeroengines
aeroengines
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
GB08408565A
Other versions
GB2139288A (en
GB8408565D0 (en
Inventor
Addison Charles Maguire
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 GB08408565A priority Critical patent/GB2139288B/en
Publication of GB8408565D0 publication Critical patent/GB8408565D0/en
Publication of GB2139288A publication Critical patent/GB2139288A/en
Application granted granted Critical
Publication of GB2139288B publication Critical patent/GB2139288B/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
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
GB08408565A 1983-05-05 1984-04-03 Exhaust mixer for bypass gas turbine aeroengines Expired GB2139288B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08408565A GB2139288B (en) 1983-05-05 1984-04-03 Exhaust mixer for bypass gas turbine aeroengines

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8312307 1983-05-05
GB08408565A GB2139288B (en) 1983-05-05 1984-04-03 Exhaust mixer for bypass gas turbine aeroengines

Publications (3)

Publication Number Publication Date
GB8408565D0 GB8408565D0 (en) 1984-05-16
GB2139288A GB2139288A (en) 1984-11-07
GB2139288B true GB2139288B (en) 1987-11-04

Family

ID=26286041

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08408565A Expired GB2139288B (en) 1983-05-05 1984-04-03 Exhaust mixer for bypass gas turbine aeroengines

Country Status (1)

Country Link
GB (1) GB2139288B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5117628A (en) * 1990-01-25 1992-06-02 General Electric Company Mixed flow augmentor pre-mixer

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4045957A (en) * 1976-02-20 1977-09-06 United Technologies Corporation Combined guide vane and mixer for a gas turbine engine

Also Published As

Publication number Publication date
GB2139288A (en) 1984-11-07
GB8408565D0 (en) 1984-05-16

Similar Documents

Publication Publication Date Title
GB2146702B (en) Exhaust mixer for turbofan aeroengine
GB2104967B (en) Exhaust mixer for turbofan aeroengine
GB2149456B (en) Exhaust mixing in turbofan aeroengines
GB8431276D0 (en) Gas turbine engine
GB8626617D0 (en) Gas turbine engine
IL65659A0 (en) Exhaust nozzle for gas turbine engine
JPS57142422A (en) Combustor for gas turbine engine
DE3365942D1 (en) Exhaust duct for gas turbines
GB8726985D0 (en) Turbofan gas turbine engine
GB8624163D0 (en) Turbofan gas turbine engine
GB8616153D0 (en) Turbofan gas turbine engine
GB8428572D0 (en) Exhaust gas turbocharger
IL65660A (en) Exhaust nozzle for gas turbine engine
IL70267A (en) Diffuser for gas turbine engine
DE3360573D1 (en) Combustor for gas turbine
GB8430785D0 (en) Gas turbine engine blade
DK314684D0 (en) AXIAL TURBINE FOR EXHAUST GAS TURBO CHARGERS
DE3467395D1 (en) Gas turbine combustor
DE3561356D1 (en) Combustion apparatus for gas turbine
GB8312111D0 (en) Prediffuser for gas turbine engine
GB8312112D0 (en) Diffuser case for gas turbine engine
GB2100807B (en) Turbine blade for gas turbine engines
GB8404906D0 (en) Controlling gas turbine engines
GB2143275B (en) Silencer for exhaust gases
GB8616154D0 (en) Turbofan gas turbine engine

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee