GB216384A - Improvements in and relating to explosion turbines - Google Patents

Improvements in and relating to explosion turbines

Info

Publication number
GB216384A
GB216384A GB1847223A GB1847223A GB216384A GB 216384 A GB216384 A GB 216384A GB 1847223 A GB1847223 A GB 1847223A GB 1847223 A GB1847223 A GB 1847223A GB 216384 A GB216384 A GB 216384A
Authority
GB
United Kingdom
Prior art keywords
chambers
exhaust
compressor
expansion
rotor
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
GB1847223A
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.)
DONALD LELAND SELLMAN
Original Assignee
DONALD LELAND SELLMAN
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 DONALD LELAND SELLMAN filed Critical DONALD LELAND SELLMAN
Priority to GB1847223A priority Critical patent/GB216384A/en
Publication of GB216384A publication Critical patent/GB216384A/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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion 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

216,384. Sellman, D. L. July 17, 1923. Radial-flow unbladed type; working-fluid supply.-In a turbine of the Barker's mill type a number of explosion chambers in the rotor register alternately with expansion chambers 21 and exhaust chambers 22 in the stator, the expansion and exhaust chambers being connected in pairs by passages 23. The exhaust 17 are connected to a suction fan 20 through a manifold 19. The explosive mixture is supplied from a compressor 25 in series with a compressor-fan 29 and connected to a fuel-supply pipe 32. The intake and exhaust manifolds communicate with ports formed in sealing rings 43, 44 engaging grooves in the rotor.
GB1847223A 1923-07-17 1923-07-17 Improvements in and relating to explosion turbines Expired GB216384A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1847223A GB216384A (en) 1923-07-17 1923-07-17 Improvements in and relating to explosion turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1847223A GB216384A (en) 1923-07-17 1923-07-17 Improvements in and relating to explosion turbines

Publications (1)

Publication Number Publication Date
GB216384A true GB216384A (en) 1924-05-29

Family

ID=10113008

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1847223A Expired GB216384A (en) 1923-07-17 1923-07-17 Improvements in and relating to explosion turbines

Country Status (1)

Country Link
GB (1) GB216384A (en)

Similar Documents

Publication Publication Date Title
US3941104A (en) Multiple turbocharger apparatus and system
GB196452A (en) Improvements in or relating to internal combustion turbine engines
GB290014A (en) Internal combustion turbine
GB216384A (en) Improvements in and relating to explosion turbines
GB420860A (en) Improvements in and relating to rotary piston internal combustion engines
GB486195A (en) Improvements in rotary internal combustion engines
GB271268A (en) Improvements in or relating to internal combustion turbines
GB676512A (en) Improvements relating to exhaust gas turbine installations
GB337092A (en) Improvements in internal combustion turbines
GB1104529A (en) Gas turbine engine
GB412006A (en) Improvements in rotary engines
GB191408433A (en) Improvements in and relating to Hydraulic Turbines.
GB191419537A (en) Internal Combustion Turbine.
GB191408707A (en) Improvements in Direct Acting Internal Combustion Turbines.
GB1110302A (en) Pressure exchanger
GB104244A (en) Improvements in and relating to Rotary Engines.
GB816753A (en) Rotary pump, motor or internal combustion engine
GB182939A (en) Internal combustion turbine
GB537838A (en) Multi-combustion rotary engine
GB567661A (en) Improvements in rotary internal combustion engines
GB401152A (en) Arrangement of several exhaust-driven turbo blowers in combination with multi-cylinder internal combustion engines
GB113697A (en) An Improved Rotary Engine.
GB277655A (en) Improvements in explosion turbines
GB527108A (en) Improvements in or relating to internal combustion engines employing supercharging
GB146549A (en) Improvements in or relating to rotary internal combustion engines