FR727831A - Continuous admission, deflagration gas turbine - Google Patents

Continuous admission, deflagration gas turbine

Info

Publication number
FR727831A
FR727831A FR727831DA FR727831A FR 727831 A FR727831 A FR 727831A FR 727831D A FR727831D A FR 727831DA FR 727831 A FR727831 A FR 727831A
Authority
FR
France
Prior art keywords
gas turbine
continuous admission
deflagration gas
deflagration
admission
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
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.)
BROWN
BBC Brown Boveri AG Germany
Original Assignee
BROWN
Brown Boveri und Cie AG Germany
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 BROWN, Brown Boveri und Cie AG Germany filed Critical BROWN
Application granted granted Critical
Publication of FR727831A publication Critical patent/FR727831A/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
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/12—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
FR727831D 1930-12-12 1931-12-04 Continuous admission, deflagration gas turbine Expired FR727831A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE606883T 1930-12-12

Publications (1)

Publication Number Publication Date
FR727831A true FR727831A (en) 1932-06-24

Family

ID=34625007

Family Applications (1)

Application Number Title Priority Date Filing Date
FR727831D Expired FR727831A (en) 1930-12-12 1931-12-04 Continuous admission, deflagration gas turbine

Country Status (5)

Country Link
BE (1) BE384871A (en)
DE (1) DE606883C (en)
FR (1) FR727831A (en)
GB (1) GB374378A (en)
NL (1) NL32738C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2825753A1 (en) * 2001-06-06 2002-12-13 Gerard Andre Machine using internal combustion to produce rotary motion has combustion chambers connected to shaft between compressor and turbine blades

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE962841C (en) * 1951-12-24 1957-04-25 Schilling Estate Company Process for operating fire gases through deflagration producing propellant gas generators and device for carrying out the process
DE942235C (en) * 1951-12-24 1956-04-26 Schilling Estate Company Process and device for operating fuel gas generators producing propellants by deflagration
DE940949C (en) * 1951-12-24 1956-03-29 Schilling Estate Company Process for the operation of fire gases through deflagration producing propellant gas generators and propellant gas generators for the implementation of the process
DE943440C (en) * 1953-01-25 1956-05-17 Habil Fritz A F Schmidt Dr Ing Exhaust control from intermittently working combustion chambers for aircraft jet engines, pulso engines or gas turbines
HUP9602589A3 (en) * 1996-09-23 1999-03-29 Diviak Janos Electrically controlled intermittent gas turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2825753A1 (en) * 2001-06-06 2002-12-13 Gerard Andre Machine using internal combustion to produce rotary motion has combustion chambers connected to shaft between compressor and turbine blades

Also Published As

Publication number Publication date
GB374378A (en) 1932-06-09
DE606883C (en) 1934-12-12
BE384871A (en)
NL32738C (en)

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