GB660690A - Conduit for hot gases under pressure, particularly applicable to exhaust nozzles of jet propulsion units - Google Patents

Conduit for hot gases under pressure, particularly applicable to exhaust nozzles of jet propulsion units

Info

Publication number
GB660690A
GB660690A GB5737/49A GB573749A GB660690A GB 660690 A GB660690 A GB 660690A GB 5737/49 A GB5737/49 A GB 5737/49A GB 573749 A GB573749 A GB 573749A GB 660690 A GB660690 A GB 660690A
Authority
GB
United Kingdom
Prior art keywords
pipe
conduit
hot gases
jet propulsion
under pressure
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
GB5737/49A
Other languages
English (en)
Inventor
Lucien Servanty
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.)
Societe Nationale des Constructions Aeronautiques du Sud Oest SNCASO
Original Assignee
Societe Nationale des Constructions Aeronautiques du Sud Oest SNCASO
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 Societe Nationale des Constructions Aeronautiques du Sud Oest SNCASO filed Critical Societe Nationale des Constructions Aeronautiques du Sud Oest SNCASO
Publication of GB660690A publication Critical patent/GB660690A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78Other construction of jet pipes
    • F02K1/80Couplings or connections
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78Other construction of jet pipes
    • F02K1/82Jet pipe walls, e.g. liners
    • F02K1/822Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
  • Exhaust Silencers (AREA)
GB5737/49A 1948-03-03 1949-03-02 Conduit for hot gases under pressure, particularly applicable to exhaust nozzles of jet propulsion units Expired GB660690A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR660690X 1948-03-03

Publications (1)

Publication Number Publication Date
GB660690A true GB660690A (en) 1951-11-14

Family

ID=9010407

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5737/49A Expired GB660690A (en) 1948-03-03 1949-03-02 Conduit for hot gases under pressure, particularly applicable to exhaust nozzles of jet propulsion units

Country Status (2)

Country Link
FR (1) FR963612A (enrdf_load_stackoverflow)
GB (1) GB660690A (enrdf_load_stackoverflow)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2225381A (en) * 1988-11-25 1990-05-30 Gen Electric Noise suppressor for gas flows
EP2943654A4 (en) * 2013-01-11 2016-07-27 United Technologies Corp SERPENTINE-TYPE BUMPER FOR EXHAUST GAS CHANNEL OF A GAS TURBINE MOTOR

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3645092A (en) * 1969-04-04 1972-02-29 Toyo Kogyo Co Temperature compensating connection between exhaust purifier and pipe

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2225381A (en) * 1988-11-25 1990-05-30 Gen Electric Noise suppressor for gas flows
GB2225381B (en) * 1988-11-25 1993-09-01 Gen Electric Closed cavity noise suppressor
EP2943654A4 (en) * 2013-01-11 2016-07-27 United Technologies Corp SERPENTINE-TYPE BUMPER FOR EXHAUST GAS CHANNEL OF A GAS TURBINE MOTOR
US10605200B2 (en) 2013-01-11 2020-03-31 United Technologies Corporation Serpentine baffle for a gas turbine engine exhaust duct

Also Published As

Publication number Publication date
FR963612A (enrdf_load_stackoverflow) 1950-07-17

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