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
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.
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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE750952C (en) * | 1940-02-13 | 1945-02-03 | Internal combustion engine |
Families Citing this family (2)
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. |
-
0
- DE DENDAT230289D patent/DE230289C/de active Active
-
1911
- 1911-05-06 GB GB191111008D patent/GB191111008A/en not_active Expired
Cited By (1)
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) |
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