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FR825164A - Combustion or exhaust gas turbine, with partial intake - Google Patents

Combustion or exhaust gas turbine, with partial intake

Info

Publication number
FR825164A
FR825164A FR825164DA FR825164A FR 825164 A FR825164 A FR 825164A FR 825164D A FR825164D A FR 825164DA FR 825164 A FR825164 A FR 825164A
Authority
FR
France
Prior art keywords
combustion
exhaust gas
gas turbine
partial intake
intake
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)
Inventor
Leist Karl
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 filed Critical
Application granted granted Critical
Publication of FR825164A publication Critical patent/FR825164A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR825164D 1937-05-24 1937-08-03 Combustion or exhaust gas turbine, with partial intake Expired FR825164A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE825164X 1937-05-24

Publications (1)

Publication Number Publication Date
FR825164A true FR825164A (en) 1938-02-24

Family

ID=6747465

Family Applications (1)

Application Number Title Priority Date Filing Date
FR825164D Expired FR825164A (en) 1937-05-24 1937-08-03 Combustion or exhaust gas turbine, with partial intake

Country Status (1)

Country Link
FR (1) FR825164A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2419689A (en) * 1942-11-05 1947-04-29 Raymond K Mcclintock Gas turbine
DE897634C (en) * 1942-06-23 1953-11-23 Karl Dr-Ing Leist Exhaust gas turbine system for internal combustion engines with partial admission of the turbine blades
EP0098363A1 (en) * 1982-06-14 1984-01-18 Rockwell International Corporation Gas turbine with blade temperature control

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE897634C (en) * 1942-06-23 1953-11-23 Karl Dr-Ing Leist Exhaust gas turbine system for internal combustion engines with partial admission of the turbine blades
US2419689A (en) * 1942-11-05 1947-04-29 Raymond K Mcclintock Gas turbine
EP0098363A1 (en) * 1982-06-14 1984-01-18 Rockwell International Corporation Gas turbine with blade temperature control

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