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1. 发明公开

EP0812378A1 PREHEATED INJECTION TURBINE CYCLE 失效
标题翻译：涡轮电路预热注射
公开(公告)号：EP0812378A1
公开(公告)日：1997-12-17
申请号：EP96907124.0
申请日：1996-02-28
申请人： Rosenblatt, Joel H.
发明人： Rosenblatt, Joel H.
IPC分类号： F01K25
CPC分类号： F01K25/08
摘要： A power turbine system operating in an organic Rankine cycle with a thermodynamic medium flowing therethrough, including a power turbine (10) having an inlet connected to a conduit (50) and an exhaust (14), a lower temperature engine system having a heat engine, a circulating thermodynamic turbine medium flowing through the heat engine and producing rejected waste heat during engine system operation, a regenerative heat transfer device (6) for heating the turbine medium from the turbine exhaust to produce liquid phase turbine medium at an elevated temperature, a pump (28) for pumping the liquid phase turbine medium at the elevated temperature as a first boiler feed return stream, a boiler feed return stream conduit (50) for conducting the boiler feed return stream to the turbine (10) through branch conduits (51, 52), injectors (53, 54), a pump (55), and a boiler vessel (56) for heating the turbine medium to be fed to the turbine inlet. The injectors are positioned along the turbine cycle between successive stages and are controlled by controlling the mass flow of the injected liquid phase turbine medium into the turbine for effecting a selected vapor quality of the resulting mixture.

2. 发明公开

EP0122017A2 Low temperature engine system 失效
标题翻译： Kalttemperaturmotorsystem。
公开(公告)号：EP0122017A2
公开(公告)日：1984-10-17
申请号：EP84301460.6
申请日：1984-03-06
申请人： Rosenblatt, Joel H.
发明人： Rosenblatt, Joel H.
IPC分类号： F01K25/10
CPC分类号： F01K25/065 , F01K23/04 , F25B29/006
摘要： An improved engine system is provided which includes a synthetic low temperature sink that is developed in conjunction with an absorbtion-refrigeration subsystem (23) having inputs from an external low-grade heat energy supply (21) and from an external source of cooling fluid (24). A low temperature engine is included which has a high temperature end (22) that is in heat exchange communication with the external heat energy source (21) and a low temperature end (36) in heat exchange communication with the synthetic sink provided by the absorbtion-refrigeration subsystem (23). By this invention, it is possible to vary the sink temperature as desired, including temperatures that are lower than ambient temperatures such as that of the external cooling source. This feature enables the use of an external heat input source that is of a very low grade because an advantageously low heat sink temperature can be selected.
摘要翻译：提供了一种改进的发动机系统，其包括与吸收制冷子系统（23）一起开发的合成低温水槽，所述吸收制冷子系统具有来自外部低级能量供应源（21）和来自外部冷却流体源 24）。包括低温发动机，其具有与外部热能源（21）进行热交换连通的高温端（22）和与吸收所提供的合成水槽的热交换连通的低温端（36） - 制冷子系统（23）。通过本发明，可以根据需要改变下沉温度，包括低于环境温度的温度，例如外部冷却源的温度。该特征使得能够使用具有非常低等级的外部热输入源，因为可以选择有利的低散热器温度。

3. 发明授权

EP1135579B1 AMBIENT TEMPERATURE SENSITIVE HEAT ENGINE CYCLE 有权
标题翻译：工作温度敏感热机
公开(公告)号：EP1135579B1
公开(公告)日：2007-04-25
申请号：EP99973094.8
申请日：1999-10-21
申请人： Rosenblatt, Joel H.
发明人： Rosenblatt, Joel H.
IPC分类号： F01K13/00 , F01K25/08
CPC分类号： F01K23/04 , F01K25/08
摘要： A control system (41) capable of responding to temperature sensors detecting changes in available external ambient cooling temperature, and adjusting turbine cycle thermodynamic medium exhaust pressure and temperature as it completes its circulation path through the turbine cycle, to what best saturation pressure conditions are needed to correspond with the temperature detected as the coldest currently available saturation temperature in the condenser (26). Such a system permits condensation of the exhaust to occur at whatever the lowest saturation temperature and pressure available at the time happens to be.

4. 发明公开

EP1135579A1 AMBIENT TEMPERATURE SENSITIVE HEAT ENGINE CYCLE 有权
标题翻译：工作温度敏感热机
公开(公告)号：EP1135579A1
公开(公告)日：2001-09-26
申请号：EP99973094.8
申请日：1999-10-21
申请人： Rosenblatt, Joel H.
发明人： Rosenblatt, Joel H.
IPC分类号： F01K13/00 , F01K25/08
CPC分类号： F01K23/04 , F01K25/08
摘要： A control system (41) capable of responding to temperature sensors detecting changes in available external ambient cooling temperature, and adjusting turbine cycle thermodynamic medium exhaust pressure and temperature as it completes its circulation path through the turbine cycle, to what best saturation pressure conditions are needed to correspond with the temperature detected as the coldest currently available saturation temperature in the condenser (26). Such a system permits condensation of the exhaust to occur at whatever the lowest saturation temperature and pressure available at the time happens to be.

5. 发明公开

EP0812378A4 PREHEATED INJECTION TURBINE CYCLE 失效
标题翻译：涡轮电路预热注射
公开(公告)号：EP0812378A4
公开(公告)日：2000-11-08
申请号：EP96907124
申请日：1996-02-28
申请人： ROSENBLATT JOEL H
发明人： ROSENBLATT JOEL H
IPC分类号： F01K25/08 , F01K25/00
CPC分类号： F01K25/08
摘要： A power turbine system operating in an organic Rankine cycle with a thermodynamic medium flowing therethrough, including a power turbine (10) having an inlet connected to a conduit (50) and an exhaust (14), a lower temperature engine system having a heat engine, a circulating thermodynamic turbine medium flowing through the heat engine and producing rejected waste heat during engine system operation, a regenerative heat transfer device (6) for heating the turbine medium from the turbine exhaust to produce liquid phase turbine medium at an elevated temperature, a pump (28) for pumping the liquid phase turbine medium at the elevated temperature as a first boiler feed return stream, a boiler feed return stream conduit (50) for conducting the boiler feed return stream to the turbine (10) through branch conduits (51, 52), injectors (53, 54), a pump (55), and a boiler vessel (56) for heating the turbine medium to be fed to the turbine inlet. The injectors are positioned along the turbine cycle between successive stages and are controlled by controlling the mass flow of the injected liquid phase turbine medium into the turbine for effecting a selected vapor quality of the resulting mixture.

6. 发明公开

EP0122017A3 Low temperature engine system 失效
标题翻译：低温发动机系统
公开(公告)号：EP0122017A3
公开(公告)日：1985-09-04
申请号：EP84301460
申请日：1984-03-06
申请人： Saulson, Stanley H. , Rosenblatt, Joel H.
发明人： Rosenblatt, Joel H.
IPC分类号： F01K25/10
CPC分类号： F01K25/065 , F01K23/04 , F25B29/006
摘要： An improved engine system is provided which includes a synthetic low temperature sink that is developed in conjunction with an absorbtion-refrigeration subsystem (23) having inputs from an external low-grade heat energy supply (21) and from an external source of cooling fluid (24). A low temperature engine is included which has a high temperature end (22) that is in heat exchange communication with the external heat energy source (21) and a low temperature end (36) in heat exchange communication with the synthetic sink provided by the absorbtion-refrigeration subsystem (23). By this invention, it is possible to vary the sink temperature as desired, including temperatures that are lower than ambient temperatures such as that of the external cooling source. This feature enables the use of an external heat input source that is of a very low grade because an advantageously low heat sink temperature can be selected.

7. 发明公开

EP1135579A4 AMBIENT TEMPERATURE SENSITIVE HEAT ENGINE CYCLE 有权
标题翻译：工作温度敏感热机
公开(公告)号：EP1135579A4
公开(公告)日：2004-03-03
申请号：EP99973094
申请日：1999-10-21
申请人： ROSENBLATT JOEL H
发明人： ROSENBLATT JOEL H
IPC分类号： F01K23/04 , F01K25/08 , F01K13/00
CPC分类号： F01K23/04 , F01K25/08
摘要： A control system (41) capable of responding to temperature sensors detecting changes in available external ambient cooling temperature, and adjusting turbine cycle thermodynamic medium exhaust pressure and temperature as it completes its circulation path through the turbine cycle, to what best saturation pressure conditions are needed to correspond with the temperature detected as the coldest currently available saturation temperature in the condenser (26). Such a system permits condensation of the exhaust to occur at whatever the lowest saturation temperature and pressure available at the time happens to be.

8. 发明授权

EP0812378B1 PREHEATED INJECTION TURBINE CYCLE 失效
标题翻译：涡轮电路预热注射
公开(公告)号：EP0812378B1
公开(公告)日：2003-04-16
申请号：EP96907124.0
申请日：1996-02-28
申请人： Rosenblatt, Joel H.
发明人： Rosenblatt, Joel H.
IPC分类号： F01K25/00
CPC分类号： F01K25/08
摘要： A power turbine system operating in an organic Rankine cycle with a thermodynamic medium flowing therethrough, including a power turbine (10) having an inlet connected to a conduit (50) and an exhaust (14), a lower temperature engine system having a heat engine, a circulating thermodynamic turbine medium flowing through the heat engine and producing rejected waste heat during engine system operation, a regenerative heat transfer device (6) for heating the turbine medium from the turbine exhaust to produce liquid phase turbine medium at an elevated temperature, a pump (28) for pumping the liquid phase turbine medium at the elevated temperature as a first boiler feed return stream, a boiler feed return stream conduit (50) for conducting the boiler feed return stream to the turbine (10) through branch conduits (51, 52), injectors (53, 54), a pump (55), and a boiler vessel (56) for heating the turbine medium to be fed to the turbine inlet. The injectors are positioned along the turbine cycle between successive stages and are controlled by controlling the mass flow of the injected liquid phase turbine medium into the turbine for effecting a selected vapor quality of the resulting mixture.

9. 发明授权

EP0122017B1 Low temperature engine system 失效
标题翻译：低温发动机系统
公开(公告)号：EP0122017B1
公开(公告)日：1990-06-13
申请号：EP84301460.6
申请日：1984-03-06
申请人： Rosenblatt, Joel H.
发明人： Rosenblatt, Joel H.
IPC分类号： F01K25/10
CPC分类号： F01K25/065 , F01K23/04 , F25B29/006

10. 发明公开

EP0294982A3 Multi-staged turbine system with bypassable bottom stage 失效
标题翻译：多级涡轮机系统具有可旁观的底部
公开(公告)号：EP0294982A3
公开(公告)日：1989-04-12
申请号：EP88304926.4
申请日：1988-05-31
申请人： Rosenblatt, Joel H.
发明人： Rosenblatt, Joel H.
IPC分类号： F01D1/02 , F01D17/00
CPC分类号： F01K9/003 , F01D1/023 , F01D17/105 , F01K9/04 , F25B15/02 , Y02A30/277 , Y02B30/62
摘要： An improved multi-stage turbine system is provided which includes a high pressure turbine stage assembly (11) and at least one lower pressure turbine stage assembly (12). Each of these turbine assemblies preferably has an inlet opening for introducing a thermodynamic medium in the form of a vapor and a discharge opening for discharging the thermodynamic medium from the turbine assembly at a reduced temperature and pressure. Each of the turbine assemblies is typically mounted on a rotatable shaft (13, 14) and these shafts may be coaxially aligned. An assembly such as a clutch (15) may be provided for releasably interlocking the shafts. The thermodynamic medium is transported, when operating conditions are suitable, from the discharge opening of the high pressure turbine assembly to the inlet opening of the lower pressure turbine assembly. When operating conditions are not thus suitable, the thermodynamic medium is transported from the discharge opening of the high pressure turbine assembly to an apparatus for vapor liquification such as a condenser (61).

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