GB436709A - Improvements in internal combustion turbines - Google Patents
Improvements in internal combustion turbinesInfo
- Publication number
- GB436709A GB436709A GB7680/35A GB768035A GB436709A GB 436709 A GB436709 A GB 436709A GB 7680/35 A GB7680/35 A GB 7680/35A GB 768035 A GB768035 A GB 768035A GB 436709 A GB436709 A GB 436709A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotors
- gases
- rotor
- rings
- march
- 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
- 238000002485 combustion reaction Methods 0.000 title abstract 2
- 239000007789 gas Substances 0.000 abstract 5
- 238000001816 cooling Methods 0.000 abstract 1
- 239000000446 fuel Substances 0.000 abstract 1
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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
436,709. Gas turbines. MARTINKA, M., 7, Schweizerstrasse, Duisburg, Germany. March 12, 1935, No. 7680. Convention date, March 22, 1934. [Class 110 (iii)] Relates to gas turbine plant in which the power rotor f and the rotor g driving the compressor are mounted on independent coaxial shafts and consists in supplying the fixed guide rings d, e with gases from a single combustion chamber a without the interposition of pipes or regulators. In Fig. 1, the gases traverse the rotors in parallel; in Fig. 2, in series. The rotors may run in the same or in opposite directions and may have different speeds. The compressor rotor may have several rings of blades. The rotors exhaust through diffuser rings to a regenerator. In the series arrangement the gases may be reheated between the rotors. Cooling air may be introduced into the chamber through the space m. Regulation is effected by controlling the fuel supply ; the speed may rise slightly as the load increases.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE436709X | 1934-03-22 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB436709A true GB436709A (en) | 1935-10-16 |
Family
ID=6506940
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB7680/35A Expired GB436709A (en) | 1934-03-22 | 1935-03-12 | Improvements in internal combustion turbines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB436709A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2473356A (en) * | 1942-04-18 | 1949-06-14 | Turbo Engineering Corp | Combustion gas turbine arrangement |
| US2504181A (en) * | 1950-04-18 | Double compound independent rotor | ||
| US2555924A (en) * | 1948-11-27 | 1951-06-05 | Bbc Brown Boveri & Cie | Fluid cooled rotor structure |
| US2650060A (en) * | 1948-04-27 | 1953-08-25 | Edward A Stalker | Gas turbine adapted as a starter |
| US20140196432A1 (en) * | 2013-01-14 | 2014-07-17 | Vinh Minh Glisttenmeer Lam | The tesla twin turbines combustion engine module |
-
1935
- 1935-03-12 GB GB7680/35A patent/GB436709A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2504181A (en) * | 1950-04-18 | Double compound independent rotor | ||
| US2473356A (en) * | 1942-04-18 | 1949-06-14 | Turbo Engineering Corp | Combustion gas turbine arrangement |
| US2650060A (en) * | 1948-04-27 | 1953-08-25 | Edward A Stalker | Gas turbine adapted as a starter |
| US2555924A (en) * | 1948-11-27 | 1951-06-05 | Bbc Brown Boveri & Cie | Fluid cooled rotor structure |
| US20140196432A1 (en) * | 2013-01-14 | 2014-07-17 | Vinh Minh Glisttenmeer Lam | The tesla twin turbines combustion engine module |
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