GB514739A - Improvements in and relating to internal combustion engines and to methods of cooling parts of the same - Google Patents

Improvements in and relating to internal combustion engines and to methods of cooling parts of the same

Info

Publication number
GB514739A
GB514739A GB1439538A GB1439538A GB514739A GB 514739 A GB514739 A GB 514739A GB 1439538 A GB1439538 A GB 1439538A GB 1439538 A GB1439538 A GB 1439538A GB 514739 A GB514739 A GB 514739A
Authority
GB
United Kingdom
Prior art keywords
cooled
relating
methods
internal combustion
same
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
GB1439538A
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 GB1439538A priority Critical patent/GB514739A/en
Publication of GB514739A publication Critical patent/GB514739A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/12Gas-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)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

514,739. Gas turbines. HOLZWARTH, H. May 13, 1938, No. 14395. [Class 110 (iii)] Parts of an internal-combustion engine are cooled by separate cooling fluids at different temperatures, so that the parts where the higher velocities of the working fluid obtain are cooled by the .cooler fluid. The forward portions of the nozzle walls 2 are cooled by cold water which is passed through the bores 9, 10 in such quantity that steam is not generated. The rearward portions and the valve chamber are cooled by hot water in the chamber 19 and passing through bores 16 in the nozzle walls and steam under pressure is generated in the process. The cold water is introduced to and evacuated from side chambers 11 by way of pipes 13.
GB1439538A 1938-05-13 1938-05-13 Improvements in and relating to internal combustion engines and to methods of cooling parts of the same Expired GB514739A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1439538A GB514739A (en) 1938-05-13 1938-05-13 Improvements in and relating to internal combustion engines and to methods of cooling parts of the same

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1439538A GB514739A (en) 1938-05-13 1938-05-13 Improvements in and relating to internal combustion engines and to methods of cooling parts of the same

Publications (1)

Publication Number Publication Date
GB514739A true GB514739A (en) 1939-11-16

Family

ID=10040416

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1439538A Expired GB514739A (en) 1938-05-13 1938-05-13 Improvements in and relating to internal combustion engines and to methods of cooling parts of the same

Country Status (1)

Country Link
GB (1) GB514739A (en)

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