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公开(公告)号：US20200291858A1
公开(公告)日：2020-09-17
申请号：US16798969
申请日：2020-02-24
Applicant: United Technologies Corporation
Inventor： Vito Guardi , Christopher B. Lyons , Nathan Snape
Abstract: A turbine engine includes a compressor section, a combustor in fluid communication with the compressor section, and a turbine section in fluid communication with the combustor. Also included in the turbine engine is a mixing chamber. The mixing chamber is located between the compressor section and the combustor section and the mixing chamber is radially outward of a primary fluid flow path connecting the compressor section, the combustor section, and the turbine section.
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公开(公告)号：US20160245179A1
公开(公告)日：2016-08-25
申请号：US14442547
申请日：2014-01-30
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Ryan K. Snyder , Kari L. Kisselbrack , Jesse Ian Berube , Michael C. O'Brien , Eric J. Helms , Ryan Timothy Matte , Vito Guardi , Bruce Paradise
CPC classification number: F02C7/06 , F01D25/18 , F01D25/32 , F05D2220/32 , F05D2260/83 , F05D2260/98
Abstract: An oil control module for a gas turbine engine is provided comprising a housing on which numerous components of a lubricating system are mounted. The components may include a variable oil reduction valve/shuttle valve, a main oil pressure sensor, a main oil temperature sensor, a main oil filter delta pressure sensor, an oil debris monitor, a lube filter, an active oil damper valve, a cool oil orifice, a knock down orifice and a lube trim orifice. By packing numerous lubricating system components onto or within a housing located adjacent to the gas turbine engine, the oil control module reduces cost and weight and simplifies the maintenance of the lubricating system.
Abstract translation: 提供了一种用于燃气涡轮发动机的油控模块，其包括其上安装有润滑系统的许多部件的壳体。 组件可以包括可变减油阀/往复阀，主油压传感器，主油温度传感器，主油滤清器三角洲压力传感器，油渣监测器，润滑油过滤器，主动减油阀，冷却 油孔，敲击孔和润滑油修整孔。 通过将许多润滑系统部件包装在与燃气涡轮发动机相邻的壳体上或内部，油控制模块降低了成本和重量，并且简化了润滑系统的维护。
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公开(公告)号：US10041409B2
公开(公告)日：2018-08-07
申请号：US14442547
申请日：2014-01-30
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Ryan K. Snyder , Kari L. Kisselbrack , Jesse Ian Berube , Michael C. O'Brien , Eric J. Heims , Ryan Timothy Matte , Vito Guardi , Bruce Paradise
Abstract: An oil control module for a gas turbine engine is provided comprising a housing on which numerous components of a lubricating system are mounted. The components may include a variable oil reduction valve/shuttle valve, a main oil pressure sensor, a main oil temperature sensor, a main oil filter delta pressure sensor, an oil debris monitor, a lube filter, an active oil damper valve, a cool oil orifice, a knock down orifice and a lube trim orifice. By packing numerous lubricating system components onto or within a housing located adjacent to the gas turbine engine, the oil control module reduces cost and weight and simplifies the maintenance of the lubricating system.
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公开(公告)号：US20160177830A1
公开(公告)日：2016-06-23
申请号：US14910283
申请日：2014-08-01
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Vito Guardi , Christopher B. Lyons , Nathan Snape
CPC classification number: F02C7/18 , F01D5/18 , F01D9/065 , F01D25/14 , F02C3/04 , F02C6/08 , F02C7/185 , F02C9/18 , F05D2220/32 , F05D2240/35 , F05D2260/20 , F23R3/283 , F23R3/286 , Y02T50/676
Abstract: A turbine engine includes a compressor section, a combustor in fluid communication with the compressor section, and a turbine section in fluid communication with the combustor. Also included in the turbine engine is a mixing chamber. The mixing chamber is located between the compressor section and the combustor section and the mixing chamber is radially outward of a primary fluid flow path connecting the compressor section, the combustor section, and the turbine section.
Abstract translation: 涡轮发动机包括压缩机部分，与压缩机部分流体连通的燃烧器和与燃烧器流体连通的涡轮部分。 涡轮发动机中还包括混合室。 混合室位于压缩机部分和燃烧器部分之间，并且混合室在连接压缩机部分，燃烧器部分和涡轮部分的主流体流动路径的径向外侧。
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