FR2217559A1 - - Google Patents

Info

Publication number
FR2217559A1
FR2217559A1 FR7401532A FR7401532A FR2217559A1 FR 2217559 A1 FR2217559 A1 FR 2217559A1 FR 7401532 A FR7401532 A FR 7401532A FR 7401532 A FR7401532 A FR 7401532A FR 2217559 A1 FR2217559 A1 FR 2217559A1
Authority
FR
France
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.)
Granted
Application number
FR7401532A
Other languages
French (fr)
Other versions
FR2217559B1 (enrdf_load_stackoverflow
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.)
RTX Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of FR2217559A1 publication Critical patent/FR2217559A1/fr
Application granted granted Critical
Publication of FR2217559B1 publication Critical patent/FR2217559B1/fr
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
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • 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
    • 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)
  • Control Of Turbines (AREA)
FR7401532A 1973-02-08 1974-01-14 Expired FR2217559B1 (enrdf_load_stackoverflow)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US33079273A 1973-02-08 1973-02-08

Publications (2)

Publication Number Publication Date
FR2217559A1 true FR2217559A1 (enrdf_load_stackoverflow) 1974-09-06
FR2217559B1 FR2217559B1 (enrdf_load_stackoverflow) 1977-08-19

Family

ID=23291354

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7401532A Expired FR2217559B1 (enrdf_load_stackoverflow) 1973-02-08 1974-01-14

Country Status (6)

Country Link
JP (1) JPS49111014A (enrdf_load_stackoverflow)
CA (1) CA986319A (enrdf_load_stackoverflow)
DE (1) DE2401212C2 (enrdf_load_stackoverflow)
FR (1) FR2217559B1 (enrdf_load_stackoverflow)
GB (1) GB1447144A (enrdf_load_stackoverflow)
IT (1) IT1007077B (enrdf_load_stackoverflow)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013083908A1 (fr) * 2011-12-07 2013-06-13 Snecma Tuyere convergente-divergente de turbomachine

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2236804A (en) * 1989-07-26 1991-04-17 Anthony Reginald Robins Compound nozzle

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3044258A (en) * 1958-11-25 1962-07-17 Gen Electric Adjustable converging-diverging nozzle
US3520138A (en) * 1969-02-27 1970-07-14 United Aircraft Corp Convertible enginf

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
NEANT *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013083908A1 (fr) * 2011-12-07 2013-06-13 Snecma Tuyere convergente-divergente de turbomachine
FR2983917A1 (fr) * 2011-12-07 2013-06-14 Snecma Tuyere convergente-divergente de turbomachine
US9683516B2 (en) 2011-12-07 2017-06-20 Snecma Convergent-divergent nozzle for a turbine engine

Also Published As

Publication number Publication date
IT1007077B (it) 1976-10-30
CA986319A (en) 1976-03-30
DE2401212A1 (de) 1974-08-15
GB1447144A (en) 1976-08-25
JPS49111014A (enrdf_load_stackoverflow) 1974-10-23
FR2217559B1 (enrdf_load_stackoverflow) 1977-08-19
DE2401212C2 (de) 1983-08-18

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Legal Events

Date Code Title Description
ST Notification of lapse