GB191111008A - Improvements in Explosion Turbines. - Google Patents

Improvements in Explosion Turbines.

Info

Publication number
GB191111008A
GB191111008A GB191111008DA GB191111008A GB 191111008 A GB191111008 A GB 191111008A GB 191111008D A GB191111008D A GB 191111008DA GB 191111008 A GB191111008 A GB 191111008A
Authority
GB
United Kingdom
Prior art keywords
valve
piston
air
stem
ports
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
Max Imhoff
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 GB191111008A publication Critical patent/GB191111008A/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
    • F02C5/04—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 the combustion chambers being formed at least partly in the turbine rotor
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04F—FINISHING WORK ON BUILDINGS, e.g. STAIRS, FLOORS
    • E04F13/00—Coverings or linings, e.g. for walls or ceilings
    • E04F13/07—Coverings or linings, e.g. for walls or ceilings composed of covering or lining elements; Sub-structures therefor; Fastening means therefor
    • E04F13/08—Coverings or linings, e.g. for walls or ceilings composed of covering or lining elements; Sub-structures therefor; Fastening means therefor composed of a plurality of similar covering or lining elements
    • E04F13/14—Coverings or linings, e.g. for walls or ceilings composed of covering or lining elements; Sub-structures therefor; Fastening means therefor composed of a plurality of similar covering or lining elements stone or stone-like materials, e.g. ceramics concrete; of glass or with an outer layer of stone or stone-like materials or glass
    • E04F13/145—Coverings or linings, e.g. for walls or ceilings composed of covering or lining elements; Sub-structures therefor; Fastening means therefor composed of a plurality of similar covering or lining elements stone or stone-like materials, e.g. ceramics concrete; of glass or with an outer layer of stone or stone-like materials or glass with an outer layer of glass

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Architecture (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

11,008. Imhoff, M. May 6, 1910, [Convention date]. Radial - flow (unbladed) type; oppositelyrunning rotor type; working-fluid supply.- Pistons moving under centrifugal force in the rotary radial cylinders of a gas turbine effect the suction and compression of the charge and the periodic admission of the exploded gases to the reaction nozzles. Radial cylinders z, secured to a shaft w, are fitted with pistons k. As each piston k is thrown outwards by centrifugal force it draws air behind it through ports o controlled by a spring-pressed valve m, and compresses air in the cylinder space before it. When the piston strikes the valve-stem t, fuel is injected through the valve p into the compressed air, and the mixture is ignited. The explosion drives the piston inwards, causing it to strike a spring f on the stem of a valve v, which thereupon opens and admits the combustion products to a reaction nozzle d. Channels< >u in the cylinder walls permit compressed air to escape from the inner to the outer side of the inwardly-moving piston. In a modification a mixture of gas and air may be drawn through ports l and the valves m. The nozzles may co-operate with an oppositely-running vane-wheel suitably geared to the shaft w.
GB191111008D 1910-05-06 1911-05-06 Improvements in Explosion Turbines. Expired GB191111008A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE191111008X 1910-05-06

Publications (1)

Publication Number Publication Date
GB191111008A true GB191111008A (en) 1911-06-29

Family

ID=32604142

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191111008D Expired GB191111008A (en) 1910-05-06 1911-05-06 Improvements in Explosion Turbines.

Country Status (2)

Country Link
DE (1) DE230289C (en)
GB (1) GB191111008A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE750952C (en) * 1940-02-13 1945-02-03 Internal combustion engine

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1146306B (en) * 1958-08-02 1963-03-28 Hans Rohrbach Dr Ing Internal combustion piston engine with rotating cylinders
FR2664329B1 (en) * 1990-07-04 1994-09-23 Henri Coutzac COMPRESSOR REACTION TURBINE.

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE750952C (en) * 1940-02-13 1945-02-03 Internal combustion engine

Also Published As

Publication number Publication date
DE230289C (en)

Similar Documents

Publication Publication Date Title
GB191111008A (en) Improvements in Explosion Turbines.
US4288981A (en) Turbine-type engine
GB1347692A (en) Prime mover incorporating an internal combustion engine
US3611720A (en) Internal combustion turbine engine
GB130414A (en) Improvements in and relating to Internal Combustion Prime Movers.
GB737082A (en) Improvements in free-piston compressors or gas generators
US1342314A (en) Gas-turbine
GB296564A (en) Improvements in rotary engines and pumps
RU2190107C2 (en) Method of operation of multi-purpose gas-turbine engine
GB190912683A (en) Improvements in Gas Engines.
GB191308007A (en) Internal Combustion Turbine.
GB191301390A (en) Improvements in or relating to Turbines.
GB191316536A (en) Improvements in Valveless Rotary Internal Combustion Engines.
GB190826070A (en) A New or Improved Construction of Turbine.
GB157241A (en) Improvements relating to internal combustion engines combined with turbines
GB190509941A (en) A New or Improved Rotatory Engine.
GB894177A (en) An internal combustion engine
GB191226567A (en) Improvements in and relating to Gas Turbines and the like.
GB191105361A (en) Improvements in Internal Combustion Turbines.
GB699854A (en) Improvements in gas turbine and jet propulsion power plants
GB190900609A (en) Improvements in and relating to Gas Turbines.
GB136745A (en) Improvements in and relating to Combustion product Generators.
GB191107914A (en) Improvements in Rotary Internal Combustion Engines.
GB191204987A (en) An Improved Combined Explosion or Internal-combustion and Compressed Air Engine.
GB935596A (en)