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41. 发明授权

US3321912A Gas turbine plant 失效
公开(公告)号：US3321912A
公开(公告)日：1967-05-30
申请号：US32367163
申请日：1963-11-14
申请人： SAURER AG ADOLPH
发明人： ULRICH OPRECHT
IPC分类号： F02C3/08 , F23R3/38
CPC分类号： F23R3/38 , F02C3/085

42. 发明授权

US3238718A Gas turbine engine 失效
公开(公告)号：US3238718A
公开(公告)日：1966-03-08
申请号：US34123364
申请日：1964-01-30
申请人： BOEING CO
发明人： HILL HENRY C
IPC分类号： F02C3/08
CPC分类号： F02C3/085

43. 发明授权

US3103325A Radial jet engine 失效
标题翻译：径向喷气发动机
公开(公告)号：US3103325A
公开(公告)日：1963-09-10
申请号：US3577860
申请日：1960-06-13
申请人： LESLIE LEUTZINGER RUDOLPH
发明人： LESLIE LEUTZINGER RUDOLPH
IPC分类号： B64C39/00 , F02C3/08
CPC分类号： B64C39/001 , B64C29/0041 , F02C3/085

44. 发明授权

US2620625A Jet engine having an air compressor driven solely by a fuel gas turbine 失效
标题翻译：喷气发动机具有仅由燃料燃气轮机驱动的空气压缩机
公开(公告)号：US2620625A
公开(公告)日：1952-12-09
申请号：US74844647
申请日：1947-05-16
申请人： PHANEUF EDWARD A
发明人： PHANEUF EDWARD A
IPC分类号： F02C3/08
CPC分类号： F02C3/08 , F02C3/085

45. 发明授权

US2542628A Turbojet propulsion apparatus with separate combustion discharge jets 失效
标题翻译：具有独立燃烧放电喷气机的涡轮喷气推进装置
公开(公告)号：US2542628A
公开(公告)日：1951-02-20
申请号：US70577746
申请日：1946-10-25
申请人： CHRISTOPHER ELBERT E
发明人： CHRISTOPHER ELBERT E
IPC分类号： F02C3/08 , F02C6/00 , F02C7/26 , F23R3/00
CPC分类号： F02C7/26 , F02C3/085 , F02C6/003 , F23R3/00 , Y02T50/671

46. 发明授权

US12116928B2 Aircraft engine having two radially offset turbines 有权
公开(公告)号：US12116928B2
公开(公告)日：2024-10-15
申请号：US18185007
申请日：2023-03-16
申请人： PRATT & WHITNEY CANADA CORP.
发明人： David Menheere
IPC分类号： F02C3/08 , F02C3/045 , F02C3/09 , F02C3/10 , F02C3/107 , F02C3/13 , F02C6/20 , F02C7/36
CPC分类号： F02C3/085 , F02C6/20 , F02C3/045 , F02C3/08 , F02C3/09 , F02C3/10 , F02C3/103 , F02C3/107 , F02C3/13 , F02C7/36
摘要： An aircraft engine, has: a high-pressure spool having a high-pressure turbine drivingly engaged to a high-pressure compressor; and a low-pressure spool having: a first low-pressure turbine downstream of the high-pressure turbine; and a second low-pressure turbine downstream of the first low-pressure turbine, one or more of the first low-pressure turbine and the second low-pressure turbine drivingly engaged to a rotatable load, the first low-pressure turbine and the second low-pressure turbine radially offset from one another relative to a central axis of the aircraft engine.

47. 发明申请

US20050120719A1 Internally insulated turbine assembly 审中-公开
标题翻译：内部绝缘涡轮组件
公开(公告)号：US20050120719A1
公开(公告)日：2005-06-09
申请号：US10730573
申请日：2003-12-08
申请人： Andrew Olsen
发明人： Andrew Olsen
IPC分类号： F01D1/08 , F01D25/14 , F02C3/08 , F02C7/24 , F02C7/00
CPC分类号： F01D1/08 , F01D25/145 , F02C3/085 , F02C7/24 , F05D2250/82 , Y02E20/14
摘要： A combustion turbine engine suited to operation in response to a flow of high-temperature gas. The combustion turbine engine generally includes an outer housing including walls that define an inlet, an outlet, and an inner surface. An insulation cartridge is disposed within the outer housing and defines an inner space. The insulation cartridge includes a wall and a core and is operable to at least partially thermally insulate the outer housing from the flow of high-temperature gas. A turbine rotor is disposed substantially within the inner space and is rotatable in response to the flow of high-temperature gas.
摘要翻译：适用于响应于高温气体流动而操作的燃气轮机。燃气涡轮发动机通常包括外壳，外壳包括限定入口，出口和内表面的壁。绝缘筒设置在外壳内并限定内部空间。绝缘筒包括壁和芯，并且可操作以使外壳与高温气体的流动至少部分热绝缘。涡轮转子基本上设置在内部空间内并可响应于高温气体的流动而旋转。

48. 发明申请

US20040034998A1 Vane and method of construction thereof 失效
标题翻译：叶片及其构造方法
公开(公告)号：US20040034998A1
公开(公告)日：2004-02-26
申请号：US10650293
申请日：2003-08-27
发明人： William F. Beacom
IPC分类号： B23P015/04
CPC分类号： F02C3/085 , F01D9/00 , Y10T29/4932 , Y10T29/49321 , Y10T29/49336 , Y10T29/49799 , Y10T403/1608
摘要： Vanes of the type for directing a fluid radially are fabricated by forming the vanes integrally to a support structure made from a sacrificial material which is removed in assembly so that the vanes are supported for operative use. In one embodiment, the vanes are formed in the dams of an annular burner by preforming the vanes supported to a disk; the vanes and disk apparatus is fitted to side plates which are then brazed together and the disk portion and complementary side plate portions are removed, for defining the dam that is affixed to the liner of the annular combustor. Other configurations are contemplated that are tailored to fit the intended embodiment. The vane and support portion made from a sacrificial material constitute an apparatus of this invention.
摘要翻译：通过将叶片整体地形成为由牺牲材料制成的支撑结构而形成用于引导径向流体的类型的叶片，所述支撑结构在组装中被移除，使得叶片被支撑以供操作使用。在一个实施例中，叶片通过预先支撑在盘上的叶片形成在环形燃烧器的坝中; 叶片和圆盘装置装配到侧板上，然后将其钎焊在一起，并且去除圆盘部分和互补侧板部分，以便限定固定在环形燃烧器的衬套上的坝。考虑到适合于预期实施例的其它配置。由牺牲材料制成的叶片和支撑部分构成本发明的装置。

49. 发明申请

US20040007219A1 Power generation device 审中-公开
标题翻译：发电装置
公开(公告)号：US20040007219A1
公开(公告)日：2004-01-15
申请号：US10464451
申请日：2003-06-19
发明人： Katsumi Asada
IPC分类号： F02M025/07
CPC分类号： F02C3/085 , F05D2220/40 , F05D2230/61 , Y02E20/14
摘要： To provide a practical and quite novel power generation device that is suitable for the mass-production with high productivity in an extremely low cost manner and with a high energy efficiency and a structure in view of the circumstances of the compact, light-weight and high power, a power generation system comprising an automotive turbocharger having a turbine rotated by a gas flow of exhaust gas and a compressor provided coaxially with the turbine and rotated by rotation of the turbine for compressing and feeding sucked air, a combustion device for mixing the sucked air compressed and fed by the compressor and fuel together and igniting and burning the mixture, a portion for introducing exhaust gas of the combustion device to the turbine to rotate the turbine by the gas flow of exhaust gas, and an output rotary shaft rotated by the turbine and provided to the compressor on the intake air side whereby a power generation device is rotated by the rotation of the output rotary shaft to generate an electric power.
摘要翻译：提供一种实用且相当新颖的发电装置，其适用于以低成本方式高生产率的大规模生产，并且考虑到紧凑，重量轻和高的环境，具有高能量效率和结构动力发电系统，包括具有通过排气气流旋转的涡轮机的汽车涡轮增压器和与涡轮机同轴设置并通过涡轮机的旋转而被旋转以压缩和供给吸入空气的压缩机，用于混合被吸入的燃料的燃烧装置由压缩机和燃料一起供给的空气和燃料一起点燃和燃烧混合物，一部分用于将燃烧装置的废气引入到涡轮机，以便通过废气的气流使涡轮旋转;以及输出旋转轴，涡轮机，并且在进气侧设置到压缩机，由此通过输出旋转轴的旋转将发电装置旋转到g 激发电力。

50. 发明授权

US5855112A Gas turbine engine with recuperator 失效
标题翻译：燃气涡轮发动机与换热器
公开(公告)号：US5855112A
公开(公告)日：1999-01-05
申请号：US875306
申请日：1998-03-30
申请人： Takashi Bannai , Tsuneo Endou , Masahiko Izumi , Ken Ohya
发明人： Takashi Bannai , Tsuneo Endou , Masahiko Izumi , Ken Ohya
IPC分类号： F02C3/05 , F02C3/08 , F02C3/14 , F02C7/08 , F02C7/32 , F23R3/34 , F23R3/40 , F23R3/44 , F28D9/00
CPC分类号： F02C7/08 , F02C3/05 , F02C3/085 , F02C3/14 , F23R3/40 , F23R3/44 , F28D9/0018 , F28D9/0025 , F05D2250/311
摘要： A gas turbine engine E includes a compressor wheel 9 and a turbine wheel 10 fixed to a rotary shaft 8, a can-type combustor 18 disposed on an extension of the axis L of the rotary shaft 8, and an circular plate-type heat exchanger 12 disposed to surround a radially outer portion of the can-type combustor 18. The compressor wheel 9, the turbine wheel 10, the can-type combustor 18 and the plate-type heat exchanger 12 are disposed coaxially with the axis L of the rotary shaft 8. Therefore, the flows of compressed air and combustion gas are symmetrized with respect to the axis L, and the distribution of temperature within a casing is also symmetrized with respect to the axis L. Thus, the flows of compressed air and combustion gas within the gas turbine engine E can be axially symmetrized, and the generation of a thermal distortion can be prevented.
摘要翻译： PCT No.PCT / JP96 / 02179 Sec。 371日期1998年3月30日 102（e）1998年3月30日PCT PCT 1996年8月2日PCT公布。第WO97 / 09524号公报日期1997年3月13日燃气涡轮发动机E包括压缩机叶轮9和固定在旋转轴8上的涡轮叶轮10，设置在旋转轴8的轴线L的延伸部上的罐型燃烧器18，板状热交换器12设置成围绕罐型燃烧器18的径向外部。压缩机叶轮9，涡轮机叶轮10，罐型燃烧器18和板式热交换器12与因此，压缩空气和燃烧气体的流动相对于轴线L对称，壳体内的温度分布也相对于轴线L对称。因此，流动燃气涡轮发动机E内的压缩空气和燃烧气体可以轴向对称，并且可以防止产生热变形。

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