GB511925A - Internal combustion turbine - Google Patents

Internal combustion turbine

Info

Publication number
GB511925A
GB511925A GB547939A GB547939A GB511925A GB 511925 A GB511925 A GB 511925A GB 547939 A GB547939 A GB 547939A GB 547939 A GB547939 A GB 547939A GB 511925 A GB511925 A GB 511925A
Authority
GB
United Kingdom
Prior art keywords
rotor
cylinders
slots
piston
air
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
GB547939A
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.)
PHILIPP LAHM
Original Assignee
PHILIPP LAHM
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 PHILIPP LAHM filed Critical PHILIPP LAHM
Priority to GB547939A priority Critical patent/GB511925A/en
Publication of GB511925A publication Critical patent/GB511925A/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
    • F02C5/02—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant

Landscapes

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

Abstract

511,925. Gas turbines; rotary compressors. LAHM, P. Feb. 18, 1939, No. 5479. [Classes 110 (ii) and 110 (iii)] The turbine comprises a rotor 7 having blades 8, and a diametral piston 13 coupling the rotor to a shaft 2. The piston 13 extends through slots 18, 19, in a rotor formed by two cylinders 16, 17, which rotates eccentrically within the rotor 7, having tangential contact as shown. Air is sucked in through ports 12 in the casing 1, slots 10, in rotor extensions 9 to compression chambers 14, 15. Compressed air passes through the slots 10 and passages 4 to a combustion chamber 3 and fuel injected into the chamber for combustion purposes. Reaction surfaces 5 are arranged in the casing wall. Exhaust ports 6 are provided. Oil grooves are arranged between cylinders 16, 17. The chambers within the cylinders 16, 17 may also be used in compressing: air. Cooling medium flows under pressure from inlet 22 in the shaft, to outlet 23, by way of passages 24, 25, in the piston 13 and annularpassages 26, 27, which inter-communicate by ducts 28. Scavenging air may be blown through the chamber 3 from the compressor.
GB547939A 1939-02-18 1939-02-18 Internal combustion turbine Expired GB511925A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB547939A GB511925A (en) 1939-02-18 1939-02-18 Internal combustion turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB547939A GB511925A (en) 1939-02-18 1939-02-18 Internal combustion turbine

Publications (1)

Publication Number Publication Date
GB511925A true GB511925A (en) 1939-08-25

Family

ID=9796969

Family Applications (1)

Application Number Title Priority Date Filing Date
GB547939A Expired GB511925A (en) 1939-02-18 1939-02-18 Internal combustion turbine

Country Status (1)

Country Link
GB (1) GB511925A (en)

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