DE3114820C2 - - Google Patents

Info

Publication number
DE3114820C2
DE3114820C2 DE19813114820 DE3114820A DE3114820C2 DE 3114820 C2 DE3114820 C2 DE 3114820C2 DE 19813114820 DE19813114820 DE 19813114820 DE 3114820 A DE3114820 A DE 3114820A DE 3114820 C2 DE3114820 C2 DE 3114820C2
Authority
DE
Germany
Prior art keywords
pressure
medium
stage
low
gas turbine
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 - Fee Related
Application number
DE19813114820
Other languages
German (de)
English (en)
Other versions
DE3114820A1 (de
Inventor
Raymond Monclova Ohio Us Smith
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.)
TDY Industries LLC
Original Assignee
Teledyne Industries Inc
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 Teledyne Industries Inc filed Critical Teledyne Industries Inc
Priority to DE19813114820 priority Critical patent/DE3114820A1/de
Publication of DE3114820A1 publication Critical patent/DE3114820A1/de
Application granted granted Critical
Publication of DE3114820C2 publication Critical patent/DE3114820C2/de
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants 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
    • F02K3/04Plants 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
    • F02K3/068Plants 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 being characterised by a short axial length relative to the diameter

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE19813114820 1981-04-11 1981-04-11 "gas-turbo-motor" Granted DE3114820A1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19813114820 DE3114820A1 (de) 1981-04-11 1981-04-11 "gas-turbo-motor"

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19813114820 DE3114820A1 (de) 1981-04-11 1981-04-11 "gas-turbo-motor"

Publications (2)

Publication Number Publication Date
DE3114820A1 DE3114820A1 (de) 1982-11-04
DE3114820C2 true DE3114820C2 (enrdf_load_stackoverflow) 1993-02-04

Family

ID=6130012

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19813114820 Granted DE3114820A1 (de) 1981-04-11 1981-04-11 "gas-turbo-motor"

Country Status (1)

Country Link
DE (1) DE3114820A1 (enrdf_load_stackoverflow)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2625012A (en) * 1950-04-18 1953-01-13 Gen Engineering And Res Corp Gas turbine power plant, including multiple fluid operated turbines
GB1077955A (en) * 1963-05-16 1967-08-02 Bristol Siddeley Engines Ltd Gas turbine jet propulsion units for aircraft
GB1487324A (en) * 1973-11-15 1977-09-28 Rolls Royce Gas turbine engines

Also Published As

Publication number Publication date
DE3114820A1 (de) 1982-11-04

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Legal Events

Date Code Title Description
8110 Request for examination paragraph 44
D2 Grant after examination
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee