SU1475256A1 - SHIP GAS TURBINE INSTALLATION - Google Patents
SHIP GAS TURBINE INSTALLATIONInfo
- Publication number
- SU1475256A1 SU1475256A1 SU4218681/06A SU4218681A SU1475256A1 SU 1475256 A1 SU1475256 A1 SU 1475256A1 SU 4218681/06 A SU4218681/06 A SU 4218681/06A SU 4218681 A SU4218681 A SU 4218681A SU 1475256 A1 SU1475256 A1 SU 1475256A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- electric generator
- air
- gas turbine
- stator
- installation
- Prior art date
Links
Landscapes
- Motor Or Generator Cooling System (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
Abstract
1. Судовая газотурбинная установка, включающая газотурбинный двигатель с многоступенчатым компрессором, соединенным с заключенным в кожух с образованием воздушной полости электрогенератором, содержащим ротор, установленный с радиальным зазором в статоре, отличающаяся тем, что, с целью повышения эффективности и надежности работы, установка снабжена системой охлаждения электрогенератора, состоящей из воздухоохладителя, коллектора подвода воздуха, расположенного на кожухе электрогенератора и связанного воздухопроводом через воздухоохладитель с компрессором газотурбинного двигателя, вентиляционных каналов, выполненных в статоре и роторе электрогенератора, сообщенных между собой и с воздушным зазором.2. Установка по п.1, отличающаяся тем, что она снабжена коллектором отвода воздуха от электрогенератора, расположенных на электрогенераторе и соединенным на входе с внутренней полостью, а на выходе при помощи воздухопровода с входом ступени низкого давления компрессора газотурбинного двигателя.3. Установка по п.1, отличающаяся тем, что вентиляционные каналы в статоре выполнены радиально, а в роторе - радиально и аксиально.1. Ship gas turbine installation comprising a gas turbine engine with a multi-stage compressor connected to a cased prisoner with the formation of an air cavity by an electric generator containing a rotor mounted with a radial clearance in the stator, characterized in that, in order to increase efficiency and reliability of operation, the installation is equipped with a system cooling of the electric generator consisting of the air cooler, air supply collector located on the casing of the electric generator and connected by an air duct through the air refrigerant with a gas turbine engine compressor, ventilation ducts made in the stator and rotor of the electric generator, interconnected with each other and with an air gap. Installation according to claim 1, characterized in that it is provided with a manifold for venting air from an electric generator, located on the electric generator and connected at the inlet to the internal cavity, and at the outlet by means of an air duct with the entrance of a low-pressure stage of a gas turbine engine compressor. Installation according to claim 1, characterized in that the ventilation ducts in the stator are made radially and in the rotor radially and axially.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU4218681/06A SU1475256A1 (en) | 1987-03-27 | 1987-03-27 | SHIP GAS TURBINE INSTALLATION |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU4218681/06A SU1475256A1 (en) | 1987-03-27 | 1987-03-27 | SHIP GAS TURBINE INSTALLATION |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU1475256A1 true SU1475256A1 (en) | 1999-07-27 |
Family
ID=60534637
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU4218681/06A SU1475256A1 (en) | 1987-03-27 | 1987-03-27 | SHIP GAS TURBINE INSTALLATION |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU1475256A1 (en) |
-
1987
- 1987-03-27 SU SU4218681/06A patent/SU1475256A1/en active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN100434700C (en) | Motor-driven centrifugal air compressor with internal cooling airflow | |
| US5148670A (en) | Gas turbine cogeneration apparatus for the production of domestic heat and power | |
| US6807802B2 (en) | Single rotor turbine | |
| US8096127B2 (en) | Exhaust turbo-supercharger | |
| RU2332579C2 (en) | Turbine air cooling circuit heat exchanger | |
| US3781126A (en) | Turbocharger compressor with dual inlet and collector chambers | |
| CA2247469A1 (en) | Integrally intercooled axial compressor and its application to power plants | |
| US7044718B1 (en) | Radial-radial single rotor turbine | |
| GB1533515A (en) | Support for concentric turbine blade shroud | |
| ATE135440T1 (en) | TURBOCHARGER | |
| US6089010A (en) | System for compensating for a pressure loss in the cooling-air ducting in a gas turbine plant | |
| CN115822775A (en) | Heat dissipation air duct of silent generator set | |
| US4170107A (en) | Method and apparatus for intercooling the charge air of a pressure-charged internal combustion engine | |
| GB2251031A (en) | Cooling air pick up for gas turbine engine | |
| EP0811752A1 (en) | Centrifugal gas turbine | |
| SU1475256A1 (en) | SHIP GAS TURBINE INSTALLATION | |
| US3866423A (en) | Turbocharger compressor with dual inlet and collector chambers | |
| GB1428929A (en) | Supercharger system for an internal combustion engine | |
| SU1462005A1 (en) | Power plant | |
| RU92003195A (en) | AIRCRAFT WITH FLOW LAMINARIZATION SYSTEM | |
| RU2143574C1 (en) | Cooled multistage turbine of turbojet engine | |
| RU2192551C2 (en) | Gas turbine engine with regeneration of heat | |
| RU94007554A (en) | GAS TURBINE INSTALLATION | |
| RU97108483A (en) | TRANSPORT GAS-TURBINE TWO-SHAFT AND THREE-SHAFT ENGINE | |
| GB1347514A (en) | Gas turbine plants |