基本信息:
- 专利标题： 복합 사이클 발전소를 위한 가스 터빈 입구 공기 냉각 방법
- 专利标题（英）：Gas turbine inlet air cooling method for combined cycle power plants
- 专利标题（中）：联合循环发电厂燃气轮机入口风冷方式
- 申请号：KR1019990013951 申请日：1999-04-20
- 公开(公告)号：KR100624990B1 公开(公告)日：2006-09-20
- 发明人： 라나싱헤자틸라 , 스미스라웁워필드
- 申请人： 제너럴 일렉트릭 캄파니
- 申请人地址： * River Road, Schenectady, New York *****, U.S.A.
- 专利权人： 제너럴 일렉트릭 캄파니
- 当前专利权人： 제너럴 일렉트릭 캄파니
- 当前专利权人地址： * River Road, Schenectady, New York *****, U.S.A.
- 代理人： 이병호; 정상구; 신현문; 이범래
- 优先权： US09/063,192 1998-04-20
- 主分类号： F02C7/141
- IPC分类号： F02C7/141
전력 발생 시스템, 가스 터빈 발전기, 소모 증기 스트림, 가스 터빈, 복합 사이클 발전소
Based on one or more expansion turbine cycle and combined-cycle power system including a gas turbine for driving one or more generators, a compressor inlet air to the gas turbine is cooled. Kalina (Kalina) is extracted from the distillation / condensation sub-system of a cycle is taken that the temperature is being adjusted to correspond to a low pressure drop is supplied to the low-pressure evaporator to cool the surrounding air by being heat-exchanged with the ambient air flowing to the compressor inlet. The component type mixture partially evaporated from the low pressure evaporator is condensed and returned to the consumption combine this vapor stream (spent vapor stream) from the low-pressure expansion turbine. Thus, since the air cools the compressor inlet for the gas turbine, thereby increasing the mass flow, and turbine output. The power generation system, the gas turbine generator, the steam consumption stream, a gas turbine, combined cycle power plants
公开/授权文献:
- KR1019990083333A 복합 사이클 발전소를 위한 가스 터빈 입구 공기 냉각 방법 公开/授权日：1999-11-25
信息查询:
EspacenetIPC结构图谱:
| F | 机械工程；照明；加热；武器；爆破 |
| --F02 | 燃烧发动机；热气或燃烧生成物的发动机装置 |
| ----F02C | 燃气轮机装置；喷气推进装置的空气进气道；空气助燃的喷气推进装置燃料供给的控制 |
| ------F02C7/00 | 不包含在组F02C1/00至F02C6/00中的或与上述各组无关的特征、部件、零件或附件；喷气推进装置的进气管 |
| --------F02C7/08 | .燃烧前加热供给空气的，如用排出气体 |
| ----------F02C7/14 | ..装置中流体的冷却 |
| ------------F02C7/141 | ...工作流体的 |