GB150923A - Improvements in internal combustion turbines - Google Patents

Improvements in internal combustion turbines

Info

Publication number
GB150923A
GB150923A GB2872719A GB2872719A GB150923A GB 150923 A GB150923 A GB 150923A GB 2872719 A GB2872719 A GB 2872719A GB 2872719 A GB2872719 A GB 2872719A GB 150923 A GB150923 A GB 150923A
Authority
GB
United Kingdom
Prior art keywords
compressor
combustion
striking
reversing
piston
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
GB2872719A
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
Priority to GB2872719A priority Critical patent/GB150923A/en
Publication of GB150923A publication Critical patent/GB150923A/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
    • F02C5/06—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid being generated in an internal-combustion gas generated of the positive-displacement type having essentially no mechanical power output

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)

Abstract

150,923. Schmidt, F., Girard, E. L., and Messlein, M. A. Nov. 19, 1919. Jet-wheels; reversing; working-fluid supply.- An internal-combustion jet-wheel 25 with staggered vanes 31 as shown in Fig. 14 is surrounded by a number of combustion chambers 35, which are fed by compressor cylinders 50 and discharges on to the vanes through reversing-valves 37 and curved slide valves 40. The gases exhaust through ports 47. The compressor pistons 51 are connected in pairs by rods 70, which are reciprocated by links 103, 102, and a crank 93 driven by a gear 91 in mesh with a gear 90 on the rotor shaft 27. For the purpose of periodically shutting off the compressor cylinders from the combustion chambers, each piston 50 is adapted to be oscillated on its rod so as to cut off its supply conduit 53 from the port 58 leading to the combustion chamber. This oscillation is effected by a cam- 62, Fig. 7, engaging a pin 60 on the piston, and the pin 60 is used also (a) to actuate the slide valve 40 by striking a 'bell-crank lever 81, and (b) to open the inlet valve 57 of the compressor cylinder 50 by striking a lever 112.
GB2872719A 1919-11-19 1919-11-19 Improvements in internal combustion turbines Expired GB150923A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2872719A GB150923A (en) 1919-11-19 1919-11-19 Improvements in internal combustion turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2872719A GB150923A (en) 1919-11-19 1919-11-19 Improvements in internal combustion turbines

Publications (1)

Publication Number Publication Date
GB150923A true GB150923A (en) 1920-09-16

Family

ID=10280117

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2872719A Expired GB150923A (en) 1919-11-19 1919-11-19 Improvements in internal combustion turbines

Country Status (1)

Country Link
GB (1) GB150923A (en)

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