DE2401212C2 - Schubdüse für ein Unterschallflugzeug-Gasturbinentriebwerk - Google Patents

Schubdüse für ein Unterschallflugzeug-Gasturbinentriebwerk

Info

Publication number
DE2401212C2
DE2401212C2 DE2401212A DE2401212A DE2401212C2 DE 2401212 C2 DE2401212 C2 DE 2401212C2 DE 2401212 A DE2401212 A DE 2401212A DE 2401212 A DE2401212 A DE 2401212A DE 2401212 C2 DE2401212 C2 DE 2401212C2
Authority
DE
Germany
Prior art keywords
nozzle
thrust
convergent
flow
engine
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
DE2401212A
Other languages
German (de)
English (en)
Other versions
DE2401212A1 (de
Inventor
Vincent James Southington Conn. DiSabato
David Lawrence Gladstonbury Conn. Motycka
Martin Sheldon Manchester Conn. Slatkin
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 Technologies 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 Technologies Corp filed Critical United Technologies Corp
Publication of DE2401212A1 publication Critical patent/DE2401212A1/de
Application granted granted Critical
Publication of DE2401212C2 publication Critical patent/DE2401212C2/de
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)
DE2401212A 1973-02-08 1974-01-11 Schubdüse für ein Unterschallflugzeug-Gasturbinentriebwerk Expired DE2401212C2 (de)

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
DE2401212A1 DE2401212A1 (de) 1974-08-15
DE2401212C2 true DE2401212C2 (de) 1983-08-18

Family

ID=23291354

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2401212A Expired DE2401212C2 (de) 1973-02-08 1974-01-11 Schubdüse für ein Unterschallflugzeug-Gasturbinentriebwerk

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)

Families Citing this family (2)

* 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
FR2983917B1 (fr) * 2011-12-07 2013-12-27 Snecma Tuyere convergente-divergente de turbomachine

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

Also Published As

Publication number Publication date
IT1007077B (it) 1976-10-30
CA986319A (en) 1976-03-30
FR2217559A1 (enrdf_load_stackoverflow) 1974-09-06
DE2401212A1 (de) 1974-08-15
GB1447144A (en) 1976-08-25
JPS49111014A (enrdf_load_stackoverflow) 1974-10-23
FR2217559B1 (enrdf_load_stackoverflow) 1977-08-19

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Legal Events

Date Code Title Description
OD Request for examination
8127 New person/name/address of the applicant

Owner name: UNITED TECHNOLOGIES CORP., 06101 HARTFORD, CONN.,

D2 Grant after examination
8364 No opposition during term of opposition