GB191408707A - Improvements in Direct Acting Internal Combustion Turbines. - Google Patents

Improvements in Direct Acting Internal Combustion Turbines.

Info

Publication number
GB191408707A
GB191408707A GB191408707DA GB191408707A GB 191408707 A GB191408707 A GB 191408707A GB 191408707D A GB191408707D A GB 191408707DA GB 191408707 A GB191408707 A GB 191408707A
Authority
GB
United Kingdom
Prior art keywords
passages
blades
stator
rotor
combustion turbines
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
Inventor
Jean Jacques Heilmann
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Application granted granted Critical
Publication of GB191408707A publication Critical patent/GB191408707A/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)
  • Sliding Valves (AREA)

Abstract

8707. Heilmann, J. J. April 17, 1913, [Convention date]. Working-fluid supply. -Relates to multipleexpansion modifications of the radial-flow internal-combustion turbines described in Specification 4518/11. The compressed gases are admitted by a distributing-valve 1 and rotating sleeve 21 to explosion chambers formed by passages 8 in the stator member 2, passages 9 in the rotor member 3, and reaction pockets 10 in the concentric stator member 4. Ignition is effected by plugs 11, and the exhaust gases expand through blades 13 in the stator member 4, blades 15 in the rotor member 5, and finally through stator blades 17 into discharge chambers 18 acting as silencers. The rotor members are connected by a common end disk to the central shaft. A number of turbines having successively staggered working passages may be arranged on the same shaft.
GB191408707D 1913-04-17 1914-04-06 Improvements in Direct Acting Internal Combustion Turbines. Expired GB191408707A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE191408707X 1913-04-17

Publications (1)

Publication Number Publication Date
GB191408707A true GB191408707A (en) 1914-11-05

Family

ID=32513723

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191408707D Expired GB191408707A (en) 1913-04-17 1914-04-06 Improvements in Direct Acting Internal Combustion Turbines.

Country Status (1)

Country Link
GB (1) GB191408707A (en)

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