-
公开(公告)号：US07934368B2
公开(公告)日：2011-05-03
申请号：US11631923
申请日：2005-07-07
CPC分类号： F01D1/12 , F02C3/05 , F02C5/10 , F05D2230/14 , F05D2250/82 , F05D2250/84 , F05D2260/963
摘要： The present invention provides an ultra micro gas turbine engine which includes a wave rotor. In various embodiments, the ultra micro gas turbine engine of the present invention includes a rotating disk which has a compressor, a wave rotor and a turbine, a first stationary member which includes an inlet and a first wave rotor port end plate, a second stationary member which includes an outlet and a second wave rotor port end plate and a combustion chamber which includes a fuel inlet and an igniter.
摘要翻译： 本发明提供一种包括波转子的超微型燃气涡轮发动机。 在各种实施例中，本发明的超微型燃气涡轮发动机包括具有压缩机，波转子和涡轮机的旋转盘，包括入口和第一波转子端口端板的第一固定构件，第二静止 构件，其包括出口和第二波形转子端口端板以及包括燃料入口和点火器的燃烧室。
-
公开(公告)号：US20080041065A1
公开(公告)日：2008-02-21
申请号：US11631923
申请日：2005-07-07
申请人： Norbert Muller , Florin Iancu , Pezhman Akbari
发明人： Norbert Muller , Florin Iancu , Pezhman Akbari
IPC分类号： F02C3/045
CPC分类号： F01D1/12 , F02C3/05 , F02C5/10 , F05D2230/14 , F05D2250/82 , F05D2250/84 , F05D2260/963
摘要： The present invention provides an ultra micro gas turbine engine which includes a wave rotor. In various embodiments, the ultra micro gas turbine engine of the present invention includes a rotating disk which has a compressor, a wave rotor and a turbine, a first stationary member which includes an inlet and a first wave rotor port end plate, a second stationary member which includes an outlet and a second wave rotor port end plate and a combustion chamber which includes a fuel inlet and an igniter.
摘要翻译： 本发明提供一种包括波转子的超微型燃气涡轮发动机。 在各种实施例中，本发明的超微型燃气涡轮发动机包括具有压缩机，波转子和涡轮机的旋转盘，包括入口和第一波转子端口端板的第一固定构件，第二静止 构件，其包括出口和第二波形转子端口端板以及包括燃料入口和点火器的燃烧室。
-
公开(公告)号：US07555891B2
公开(公告)日：2009-07-07
申请号：US11271483
申请日：2005-11-11
申请人： Norbert Müller , Pezhman Akbari , Janusz Piechna , Florin Iancu
发明人： Norbert Müller , Pezhman Akbari , Janusz Piechna , Florin Iancu
IPC分类号： F02C3/02
CPC分类号： F04D25/04 , F02C3/02 , F04D35/00 , F05D2250/314
摘要： A wave rotor apparatus is provided. In another aspect of the present invention, a radial wave rotor includes fluid passageways oriented in a direction offset from its rotational axis. A further aspect of the present invention employs stacked layers of generally radial channels in a wave rotor. Moreover, turbomachinery is located internal to a wave rotor in yet another aspect of the present invention. In yet another aspect of the present invention, a radial wave rotor has an igniter and fuel injector. Correctional passages are employed in still another aspect of the present invention wave rotor.
摘要翻译： 提供波转子装置。 在本发明的另一方面，径向波转子包括沿与其旋转轴线偏离的方向定向的流体通道。 本发明的另一方面在波形转子中采用大体径向通道的叠层。 此外，在本发明的另一方面，涡轮机械位于波浪转子的内部。 在本发明的另一方面，径向波转子具有点火器和燃料喷射器。 在本发明的波转子的另一方面，采用了惩戒通道。
-
公开(公告)号：US08443583B2
公开(公告)日：2013-05-21
申请号：US12304923
申请日：2007-06-14
申请人： Razi Nalim , Pezhman Akbari
发明人： Razi Nalim , Pezhman Akbari
IPC分类号： F02C3/02
摘要： Apparatus and methods for combustion of fuel. Some embodiments of the inventions include a fuel nozzle which injects fuel into a combustion channel of a wave rotor combustor or a pulse detonation combustor In some embodiments the combustion process includes a backward-propagating detonation wave within a substantially closed channel which compresses discrete quantities of combustible and noncombustible mixture. Yet other embodiments include a precombustion chamber integrated into the wave rotor, the outlet stator or both.
摘要翻译： 用于燃料燃烧的装置和方法。 本发明的一些实施例包括将燃料喷射到波浪转子燃烧器或脉冲爆震燃烧器的燃烧通道中的燃料喷嘴。在一些实施例中，燃烧过程包括在基本封闭的通道内的向后传播的爆震波，其压缩离散量的可燃 和不燃混合物。 其他实施例包括集成到波形转子，出口定子或两者中的预燃室。
-
公开(公告)号：US20060130478A1
公开(公告)日：2006-06-22
申请号：US11271483
申请日：2005-11-11
申请人： Norbert Muller , Pezhman Akbari , Janusz Piechna , Florin Iancu
发明人： Norbert Muller , Pezhman Akbari , Janusz Piechna , Florin Iancu
IPC分类号： F02B33/44
CPC分类号： F04D25/04 , F02C3/02 , F04D35/00 , F05D2250/314
摘要： A wave rotor apparatus is provided. In another aspect of the present invention, a radial wave rotor includes fluid passageways oriented in a direction offset from its rotational axis. A further aspect of the present invention employs stacked layers of generally radial channels in a wave rotor. Moreover, turbomachinery is located internal to a wave rotor in yet another aspect of the present invention. In yet another aspect of the present invention, a radial wave rotor has an igniter and fuel injector. Correctional passages are employed in still another aspect of the present invention wave rotor.
-
-
-
-
搜索结果
5 条记录 (耗时 0.015 秒)
