GB1074658A - A gas turbine installation - Google Patents
A gas turbine installationInfo
- Publication number
- GB1074658A GB1074658A GB2654164A GB2654164A GB1074658A GB 1074658 A GB1074658 A GB 1074658A GB 2654164 A GB2654164 A GB 2654164A GB 2654164 A GB2654164 A GB 2654164A GB 1074658 A GB1074658 A GB 1074658A
- Authority
- GB
- United Kingdom
- Prior art keywords
- groups
- gas
- power turbine
- axis
- gas turbine
- 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
- 238000009434 installation Methods 0.000 title abstract 2
- 239000007789 gas Substances 0.000 abstract 9
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
- F02C6/02—Plural gas-turbine plants having a common power output
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
1,074,658. Gas turbine plant. LICENTIA PATENT-VERWALTUNGS - G.m.b.H. June 26, 1964 [June 28, 1963], No. 26541/64. Heading F1G. A gas turbine installation comprises an electric generator 17, Fig. 3, driven by an axial flow power turbine 14, Fig. 2, which is in turn driven by the gases produced in a set of eight gas turbine type gas generators 12, which set is arranged in two groups 13, one on either side of the vertical plane 10 through the axis 11 of the power turbine, the four gas generators of each group being arranged vertically one above the other, and the machine being situated between the two groups and/or their air intake ducts 16. Each group 13 is divided into two sub-groups, each of which comprises two gas generators 12 producing gases which are collected in a common chamber 23. The four chambers 23 merge into an annular chamber 24. Access to a bearing 19 of the power turbine shaft 20 may be had from above. All the gas generators 12 may be parallel to the power turbine axis 11 or, as shown in Fig. 3, each of the two groups may diverge from the axis 11 at an angle which may be as large as 45‹.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DEL0045235 | 1963-06-28 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1074658A true GB1074658A (en) | 1967-07-05 |
Family
ID=7271054
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2654164A Expired GB1074658A (en) | 1963-06-28 | 1964-06-26 | A gas turbine installation |
Country Status (2)
| Country | Link |
|---|---|
| CH (1) | CH416220A (en) |
| GB (1) | GB1074658A (en) |
-
1964
- 1964-06-19 CH CH802564A patent/CH416220A/en unknown
- 1964-06-26 GB GB2654164A patent/GB1074658A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| CH416220A (en) | 1966-06-30 |
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