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101. 发明授权

US3768248A Exhaust manifolding 失效
标题翻译：排气管
公开(公告)号：US3768248A
公开(公告)日：1973-10-30
申请号：US3768248D
申请日：1971-12-27
申请人： CATERPILLAR TRACTOR CO
发明人： GRGURICH W , SWANSON M
IPC分类号： F02B37/02 , F02B37/04
CPC分类号： F02B37/02 , Y02T10/144
摘要： There is disclosed a unique manifold arrangement for turbocharged internal combustion engines having a multiple of four cylinders. The manifold system is arranged to provide even spacing between alternate sets of non-interfering cylinders to provide an even flow of exhaust to the branches of the manifold.
摘要翻译：公开了具有四个气缸的倍数的涡轮增压内燃机的独特的歧管装置。歧管系统被布置成在替代的非干涉气缸组之间提供均匀间隔，以向歧管的分支提供均匀的排气流。

102. 发明授权

US3673798A Turbocharged internal combustion engine 失效
标题翻译：涡轮内燃机
公开(公告)号：US3673798A
公开(公告)日：1972-07-04
申请号：US3673798D
申请日：1971-01-08
申请人： GEN MOTORS CORP
发明人： KUEHL PAUL B
IPC分类号： F02B3/06 , F02B37/02 , F02C6/12 , F02B37/04 , F02D39/04
CPC分类号： F02C6/12 , F02B3/06 , F02B37/02 , F02B75/22 , Y02T10/144
摘要： In preferred form, a V-type internal combustion engine is provided with a combination turbocharger and manifold mounted between the cylinder banks in a compact arrangement. Exhaust manifolds on the outer walls of the cylinder banks interconnect the cylinder exhaust passages with the usual exhaust heat passage extending transversely of the cylinder head through which exhaust gases are delivered to the turbine to the central manifoldturbocharger unit. The combination unit provides water cooling and oil lubrication features in addition to a compact and practical construction.

103. 发明授权

US3673797A Compound power plant 失效
标题翻译：化学发电厂
公开(公告)号：US3673797A
公开(公告)日：1972-07-04
申请号：US3673797D
申请日：1970-12-08
申请人： PERKINS SERVICES NV
发明人： WILKINSON WILLIAM H
IPC分类号： F02B37/10 , F02B37/16 , F02C7/36 , F02D25/00 , F02D29/00 , F02B37/04
CPC分类号： F02B37/105 , F02B37/166 , F02C7/36 , F02D25/00 , F02D29/00 , Y02T10/144
摘要： A power plant for driving a load comprises an internal combustion engine, an exhaust turbine, primary and secondary compressors, and first and second planetary differentials each having an input and two outputs. The first differential has its input driven by the engine output, its first output connected to the load, and its second output driving the secondary compressor. The turbine drives the primary compressor and the second differential, which has its first output connected to the first differential input and its second output connected to the load. The compressor discharges flow in series or in parallel through a heat exchanger to the engine inlet manifold and the engine exhaust drives the turbine. A portion of the net compressor discharge is by-passed around the engine through a heat exchanger to recover heat from the turbine exhaust, and through an afterburner to the exhaust turbine. A speed control device connects the second output of the first differential and the load. The speed control device comprises a variable displacement hydrostatic pump driving a variable displacement hydrostatic motor, and a control for the displacements; it may also comprise an electric generator and motor set with a control for the fields.

104. 发明授权

US3574997A High pressure hot gas generator for turbines 失效
标题翻译：用于涡轮机的高压热发电机
公开(公告)号：US3574997A
公开(公告)日：1971-04-13
申请号：US3574997D
申请日：1969-03-26
申请人： GERALD H SYROVY
发明人： SYROVY GERALD H
IPC分类号： F02B1/04 , F02C5/06 , F02B37/04 , F02K5/02
CPC分类号： F02C5/06 , F02B1/04 , Y02T50/671
摘要： A constant displacement air compressor is combined with a reciprocating type combustion chamber utilizing a modified diesel cycle process in such a manner that substantially all of the power developed by the reciprocating combustion chamber is employed to drive the air compressor. The air compressor in turn provides scavenging air to displace the combusted gases in the reciprocating combustion chamber, the scavenged air and gases constituting extremely high-pressure hot gas. This generated gas may then be directed to drive a turbine, power from the system for external work being derived from the turbine. This invention relates generally to power plants for both mobile including aircraft and boats and stationary use and more particularly to a high-pressure hot gas generator for driving turbines.

105. 发明授权

US3469393A Turbocharged internal combustion engine 失效
标题翻译： TURBOCHARGED内燃机
公开(公告)号：US3469393A
公开(公告)日：1969-09-30
申请号：US3469393D
申请日：1967-03-06
申请人： DONALD WILFRED TRYHORN , WHITWORTH & CO
发明人： TRYHORN DONALD WILFRED
IPC分类号： F02B33/44 , F02B37/007 , F02B37/02 , F02B37/04 , F02B75/02 , F02B33/34 , F02D39/04
CPC分类号： F02B37/02 , F01N13/107 , F02B33/34 , F02B33/44 , F02B37/004 , F02B37/007 , F02B37/04 , F02B39/04 , F02B2075/025 , Y02T10/144

106. 发明授权

US3270730A Internal combustion engines 失效
公开(公告)号：US3270730A
公开(公告)日：1966-09-06
申请号：US40861764
申请日：1964-11-03
申请人： GEAROID TIMONEY SEAMUS
发明人： GEAROID TIMONEY SEAMUS
IPC分类号： F02B1/00 , F02B33/00 , F02B37/04 , F02B39/04
CPC分类号： F02B39/04 , F02B1/00 , F02B33/00 , F02B37/04 , F02B2700/023 , F02M2700/333 , Y02T10/144

107. 发明授权

US3257797A Tandem supercharging system 失效
标题翻译：串联增压系统
公开(公告)号：US3257797A
公开(公告)日：1966-06-28
申请号：US36863264
申请日：1964-05-19
申请人： NORDBERG MANUFACTURING CO
发明人： LIEBERHERR HANS U
IPC分类号： F02B29/04 , F02B33/44 , F02B37/007 , F02B37/013 , F02B37/04 , F02B37/12
CPC分类号： F02B37/12 , F02B29/0412 , F02B29/0418 , F02B29/0493 , F02B33/443 , F02B37/004 , F02B37/007 , F02B37/013 , F02B37/04 , Y02T10/144 , Y02T10/146

108. 发明授权

US2525460A Marine propulsion plant 失效
标题翻译：海运推进厂
公开(公告)号：US2525460A
公开(公告)日：1950-10-10
申请号：US53266344
申请日：1944-04-25
申请人： FRITZ ROESCH
发明人： FRITZ ROESCH
IPC分类号： F02B37/04 , F02B37/10 , F02D29/02
CPC分类号： F02B37/10 , F02B37/04 , F02B37/105 , F02D29/02 , Y02T10/144

109. 发明授权

US2444456A Supercharging system for internal-combustion engines 失效
标题翻译：内燃机增压系统
公开(公告)号：US2444456A
公开(公告)日：1948-07-06
申请号：US49921843
申请日：1943-08-19
申请人： JARVIS C MARBLE , LESLIE M MERRILL , PERCY H BATTEN
发明人： ALF LYSHOLM
IPC分类号： F02B29/04 , F02B37/04 , F02B39/08
CPC分类号： F02B37/04 , F02B29/0431 , F02B39/08 , Y02T10/144 , Y02T10/146

110. 发明授权

US2443717A Exhaust gas and hot air turbine system 失效
标题翻译：废气和热风涡轮机系统
公开(公告)号：US2443717A
公开(公告)日：1948-06-22
申请号：US44153742
申请日：1942-05-02
申请人： TURBO ENGINEERING CORP
发明人： RUDOLPH BIRMANN
IPC分类号： F02B37/04 , F02B37/16 , F02C1/05 , F02C6/12 , F02K3/12
CPC分类号： F02C6/12 , F02B37/04 , F02B37/166 , F02C1/05 , F02K3/12 , Y02T10/144

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