IT7826715A0 - Ugello di scarico complanare specialmente per turbomotori a gas. - Google Patents

Ugello di scarico complanare specialmente per turbomotori a gas.

Info

Publication number
IT7826715A0
IT7826715A0 IT7826715A IT2671578A IT7826715A0 IT 7826715 A0 IT7826715 A0 IT 7826715A0 IT 7826715 A IT7826715 A IT 7826715A IT 2671578 A IT2671578 A IT 2671578A IT 7826715 A0 IT7826715 A0 IT 7826715A0
Authority
IT
Italy
Prior art keywords
complanar
exhaust nozzle
gas turbo
turbo engines
nozzle especially
Prior art date
Application number
IT7826715A
Other languages
English (en)
Other versions
IT1098087B (it
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT7826715A0 publication Critical patent/IT7826715A0/it
Application granted granted Critical
Publication of IT1098087B publication Critical patent/IT1098087B/it

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
    • F02K1/40—Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Exhaust Silencers (AREA)
IT26715/78A 1977-11-17 1978-08-11 Ugello di scarico complanare specialmente per turbomotori a gas IT1098087B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US85242077A 1977-11-17 1977-11-17

Publications (2)

Publication Number Publication Date
IT7826715A0 true IT7826715A0 (it) 1978-08-11
IT1098087B IT1098087B (it) 1985-08-31

Family

ID=25313265

Family Applications (1)

Application Number Title Priority Date Filing Date
IT26715/78A IT1098087B (it) 1977-11-17 1978-08-11 Ugello di scarico complanare specialmente per turbomotori a gas

Country Status (4)

Country Link
JP (1) JPS5472313A (it)
DE (1) DE2835902A1 (it)
FR (1) FR2409387A1 (it)
IT (1) IT1098087B (it)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007063018A1 (de) 2007-12-21 2009-06-25 Rolls-Royce Deutschland Ltd & Co Kg Düse mit Leitelementen
CN115949530B (zh) * 2023-03-09 2023-06-30 中国航发四川燃气涡轮研究院 一种异形喷管的隐身装置

Also Published As

Publication number Publication date
JPS5472313A (en) 1979-06-09
FR2409387A1 (fr) 1979-06-15
IT1098087B (it) 1985-08-31
DE2835902A1 (de) 1979-05-23

Similar Documents

Publication Publication Date Title
IT1073329B (it) Ugello di scarico a spinta orientabile particolarmente per turbomotori a gas
IT7828914A0 (it) Perfezionamenti apportati ai dispositivi di combustione per motori a turbina a gas.
IT7821288A0 (it) Motore per turbina a gas.
IT7824102A0 (it) Turbomotore a gas e mezzi per raffreddare il medesimo.
IT1079420B (it) Turbocompressore a gas di scarico
IT8019702A0 (it) Cappottatura di motore a turbina agas.
IT8423443A0 (it) Complesso di combustione per motore a turbina a gas.
IT8020445A0 (it) Motore a turbina a gas.
JPS5641436A (en) Exhaust nozzle for gas turbine engines
AT364961B (de) Brennkammer, insbesondere fuer gasturbinentriebwerke
IT1096061B (it) Dispositivo per la manutenzione di propulsori a turbina a gas,in particolare di propulsori a turbogetto
IT8026202A0 (it) Sovralimentatore a gas di scarico.
GB1551881A (en) Gas turbine engine powerplants
IT8119348A0 (it) Complesso di aspirazione per turbomotori a gas.
IT8022694A0 (it) Diffusore particolarmente adattoper turbomotori a gas.
NL7607123A (nl) Geluiddemper voor straalmotoren.
IT7827281A0 (it) Complesso di iniettore dicombustibile per un motore a turbina a gas.
IT1089612B (it) Apparecchio di combustione per un motore da turbina a gas
IT7831299A0 (it) Complesso turbocompressore a gas di scarico.
IT8521926A0 (it) Ugello di scarico orientabile per un motore a turbina a gas.
IT1097195B (it) Sistema di controllo integrato per un turbomotore a gas
GB1541706A (en) Exhaust nozzles for gas turbine engines
IT7825805A0 (it) Perfezionato controllo di riserva per turbomotore a gas.
IT7926982A0 (it) Camera di combustione per turbomotore a gas.
IT1073779B (it) Contenitore per propulsori a turbina a gas in particolare per propulsori a turbogetto