GB346108A - Improvements in and relating to regulating arrangements for gas turbine having an internal combustion engine connected in front thereof - Google Patents
Improvements in and relating to regulating arrangements for gas turbine having an internal combustion engine connected in front thereofInfo
- Publication number
- GB346108A GB346108A GB6091/30A GB609130A GB346108A GB 346108 A GB346108 A GB 346108A GB 6091/30 A GB6091/30 A GB 6091/30A GB 609130 A GB609130 A GB 609130A GB 346108 A GB346108 A GB 346108A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- engine
- internal combustion
- gas turbine
- combustion engine
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K23/00—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids
- F01K23/12—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engines being mechanically coupled
- F01K23/14—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engines being mechanically coupled including at least one combustion engine
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
Abstract
346,108. Motor power plant. SIEMENS-SHUCKERTWERKE AKT.- GES., Siemensstadt, Berlin. Feb. 24, 1930, No. 6091. Convention date, Feb. 26, 1929. [Class 110 (iii).] In a plant comprising a gas turbine T driven by the exhaust of an internal combustion engine U, regulation is effected by varying the supply of fuel and/or air to the internalcombustion engine. In Fig. 3 the motor units are mechanically coupled, and a speed governor F controls the fuel admission valve V of the unit U. It may also control the suction valve A of the air compressor K which supplies the engine U. The valve A may be controlled by the pressure conditions in the supply pipe b of the turbine T as shown in Fig. 5, or by a speed governor driven by the engine U. As shown in Fig. 5, the power units need not be coupled together. A governor-controlled safety valve for excessive speeds, or a valve for the prevention of excessive reduction of pressure, may be arranged in the connecting pipe b.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE346108X | 1929-02-26 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB346108A true GB346108A (en) | 1931-04-09 |
Family
ID=6255018
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB6091/30A Expired GB346108A (en) | 1929-02-26 | 1930-02-24 | Improvements in and relating to regulating arrangements for gas turbine having an internal combustion engine connected in front thereof |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB346108A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2434777A (en) * | 1942-09-30 | 1948-01-20 | English Electric Co Ltd | Power plant comprising a gas turbine and an internal-combustion engine compressor serving as a gas generator thereto |
US2602287A (en) * | 1944-04-15 | 1952-07-08 | United Aircraft Corp | Starting control system for power plants |
US2609656A (en) * | 1944-04-15 | 1952-09-09 | United Aircraft Corp | Gas turbine power plant having fuel cut-off valve actuated by an overspeed governor |
US2755618A (en) * | 1952-04-16 | 1956-07-24 | Adolphe C Peterson | Internal combustion engine and gas turbine driving means |
-
1930
- 1930-02-24 GB GB6091/30A patent/GB346108A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2434777A (en) * | 1942-09-30 | 1948-01-20 | English Electric Co Ltd | Power plant comprising a gas turbine and an internal-combustion engine compressor serving as a gas generator thereto |
US2602287A (en) * | 1944-04-15 | 1952-07-08 | United Aircraft Corp | Starting control system for power plants |
US2609656A (en) * | 1944-04-15 | 1952-09-09 | United Aircraft Corp | Gas turbine power plant having fuel cut-off valve actuated by an overspeed governor |
US2755618A (en) * | 1952-04-16 | 1956-07-24 | Adolphe C Peterson | Internal combustion engine and gas turbine driving means |
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