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FR1239218A - Turbojet - Google Patents

Turbojet

Info

Publication number
FR1239218A
FR1239218A FR808817A FR808817A FR1239218A FR 1239218 A FR1239218 A FR 1239218A FR 808817 A FR808817 A FR 808817A FR 808817 A FR808817 A FR 808817A FR 1239218 A FR1239218 A FR 1239218A
Authority
FR
France
Prior art keywords
turbojet
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
FR808817A
Other languages
French (fr)
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.)
ENTWICKLUNGSBAU PIRNA VEB
Original Assignee
ENTWICKLUNGSBAU PIRNA VEB
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 ENTWICKLUNGSBAU PIRNA VEB filed Critical ENTWICKLUNGSBAU PIRNA VEB
Priority to FR808817A priority Critical patent/FR1239218A/en
Application granted granted Critical
Publication of FR1239218A publication Critical patent/FR1239218A/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
    • 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
    • F02K3/062—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 aft fan

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR808817A 1959-10-29 1959-10-29 Turbojet Expired FR1239218A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR808817A FR1239218A (en) 1959-10-29 1959-10-29 Turbojet

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR808817A FR1239218A (en) 1959-10-29 1959-10-29 Turbojet

Publications (1)

Publication Number Publication Date
FR1239218A true FR1239218A (en) 1960-08-19

Family

ID=8720673

Family Applications (1)

Application Number Title Priority Date Filing Date
FR808817A Expired FR1239218A (en) 1959-10-29 1959-10-29 Turbojet

Country Status (1)

Country Link
FR (1) FR1239218A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3394548A (en) * 1964-09-05 1968-07-30 Daimler Benz Ag Two-stage turbine unit
EP0497472A1 (en) * 1991-01-28 1992-08-05 Williams International Corporation AFT Fan Gas turbine engine
US20170184020A1 (en) * 2015-12-29 2017-06-29 General Electric Company Method and system for in-line distributed propulsion

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3394548A (en) * 1964-09-05 1968-07-30 Daimler Benz Ag Two-stage turbine unit
EP0497472A1 (en) * 1991-01-28 1992-08-05 Williams International Corporation AFT Fan Gas turbine engine
US20170184020A1 (en) * 2015-12-29 2017-06-29 General Electric Company Method and system for in-line distributed propulsion
US10677158B2 (en) * 2015-12-29 2020-06-09 General Electric Company Method and system for in-line distributed propulsion

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