-
公开(公告)号:US20070251760A1
公开(公告)日:2007-11-01
申请号:US11412756
申请日:2006-04-27
IPC分类号: F01N1/02
CPC分类号: F01D25/30 , F02C5/10 , F02K1/827 , F02K3/10 , F05D2260/96 , F05D2260/99 , F23R3/00 , F23R2900/00014
摘要: A turbine engine resonator comprising a panel and a vessel. The panel is along a flow path within the engine and has an aperture. The vessel has a mounting flange secured to the panel. The flange has an aperture mated to the aperture of the panel. The vessel has a body secured to the mounting flange with an interior of the body in communication with the flange aperture. A first portion of the panel extends into the mounting flange aperture and may redirect a leakage flow, if any, to limit an effect of leakage upon resonator performance.
摘要翻译: 一种涡轮发动机谐振器,包括面板和容器。 面板沿着发动机内的流动路径并且具有孔。 容器具有固定到面板上的安装凸缘。 凸缘具有与面板孔径配合的孔。 容器具有固定到安装凸缘的主体,其内部与凸缘孔连通。 面板的第一部分延伸到安装凸缘孔中,并且可以重定向泄漏流(如果有的话),以限制泄漏对谐振器性能的影响。
-
公开(公告)号:US20070034446A1
公开(公告)日:2007-02-15
申请号:US11200563
申请日:2005-08-10
申请人: William Proscia , Christopher Jones
发明人: William Proscia , Christopher Jones
CPC分类号: F04D29/665 , F02K1/827 , F02K3/10 , F05D2260/96 , G10K11/161
摘要: An acoustic liner 20 includes a remote panel 26, a perforated proximate panel 22 transversely spaced from the remote panel and one or more partitions 32 spanning across the space between the panels. At least one baffle 44 cooperates with the partitions to define a resonator chamber 34b and an associated neck 56 for establishing communication between the resonator chamber and a fluid stream G flowing past the proximate panel.
摘要翻译: 声学衬垫20包括远程面板26,与远程面板横向间隔开的穿孔邻近面板22以及穿过面板之间的空间的一个或多个隔板32。 至少一个挡板44与隔板配合以限定谐振器室34b和相关联的颈部56,用于建立谐振腔与流过邻近面板的流体流G之间的连通。
-
公开(公告)号:US20070034447A1
公开(公告)日:2007-02-15
申请号:US11200617
申请日:2005-08-10
申请人: William Proscia , Christopher Jones
发明人: William Proscia , Christopher Jones
CPC分类号: F01D25/30 , F02C7/045 , F02C7/24 , F02K1/44 , F02K1/827 , F02K3/10 , F05D2260/96 , F23M20/005 , G10K11/172
摘要: An acoustic liner 20 includes a remote panel 26, a proximate panel 28 transversely spaced from the remote panel and a resonator chamber 34b residing between the panels. Perforations 38 penetrate the proximate panel in registration with the resonator chamber 34b. A neck 56 with an inlet 58 recessed from the proximate panel establishes communication between the chamber and a fluid stream G flowing past the proximate panel. A bypass coolant passage 66 guides coolant through the perforations without guiding it through the resonator chamber.
-
公开(公告)号:US20050284690A1
公开(公告)日:2005-12-29
申请号:US10878806
申请日:2004-06-28
IPC分类号: B64D33/02 , B64F1/26 , E04H17/00 , F02C7/045 , F02C7/24 , F02K1/82 , F02K99/00 , G10K11/00 , G10K11/172 , F02K11/00
CPC分类号: F02C7/24 , B64D2033/0206 , F02C7/045 , F02K1/827 , F05D2260/96 , G10K11/172 , Y02T50/671
摘要: A cooled acoustic liner useful in a fluid handling duct includes a resonator chamber 52 with a neck 56, a face sheet 86, and a coolant plenum 80 residing between the face sheet and the chamber. Coolant bypasses the resonator chamber, rather than flowing through it, resulting in better acoustic admittance than in liners in which coolant flows through the resonator chamber and neck. In one embodiment, the liner also includes a graze shield 88. Openings 40, 38 penetrate both the face sheet and the shield to establish a relatively low face sheet porosity and a relatively high shield porosity. The shielded embodiment of the invention helps prevent a loss of acoustic admittance due to fluid grazing past the liner. Another embodiment that is not necessarily cooled, includes the resonator chamber, low porosity face sheet and high porosity shield, but no coolant plenum for bypassing coolant around the resonator chamber. An associated method of retrofitting an acoustic treatment into a fluid handling module includes installing openings in the module and mounting a resonator box 44 on the module so that the inlets to the resonator necks register with the installed openings.
摘要翻译: 可用于流体处理管道的冷却的声学衬垫包括具有颈部56,面板86和驻留在面板和腔室之间的冷却剂室80的谐振腔52。 冷却液绕过谐振腔,而不是流过谐振腔,导致比冷却剂流过谐振腔和颈部的衬垫更好的声导。 在一个实施例中,衬垫还包括刮板88.开口40,38同时穿过面片和屏蔽件,以建立相对低的面片孔隙率和相对高的屏蔽孔隙率。 本发明的屏蔽实施例有助于防止由于通过衬垫的流体放牧导致的声导纳损失。 不一定冷却的另一个实施例包括谐振器腔,低孔隙率面片和高孔隙度屏蔽,但没有用于绕过共振腔的冷却剂的冷却剂室。 将声学处理改造成流体处理模块的相关方法包括在模块中安装开口并将谐振器盒44安装在模块上,使得谐振器颈部的入口与安装的开口对齐。
-
公开(公告)号:US20060137352A1
公开(公告)日:2006-06-29
申请号:US11025402
申请日:2004-12-29
申请人: Dilip Prasad , Jinzhang Feng , William Proscia
发明人: Dilip Prasad , Jinzhang Feng , William Proscia
IPC分类号: F02K3/10
CPC分类号: F23R3/002 , F02K1/827 , F05D2260/96 , F23M20/005 , F23R2900/00014
摘要: An augmentor liner is provided that includes an annulus disposed between a first wall and a second wall, and a plurality of baffles. The first wall is disposed radially inside of the second wall. The plurality of baffles extend heightwise between the first wall and the second wall, and are circumferentially spaced apart from one another by a distance. The distance between adjacent baffles is such that an acoustic wave entering an annulus compartment will travel between the first wall and second wall in a direction having a radial component that is substantially greater than a circumferential component. The baffle spacing may alternatively be described as being such that the circumferential component of the acoustic wave is substantially damped and therefore does not materially contribute to undesirable screech.
摘要翻译: 提供增强衬套,其包括设置在第一壁和第二壁之间的环形空间,以及多个挡板。 第一壁径向设置在第二壁的内侧。 多个挡板在第一壁和第二壁之间的高度方向上延伸,并且彼此间隔开一定距离。 相邻挡板之间的距离使得进入环形隔室的声波将沿着具有基本上大于周向部件的径向分量的方向在第一壁和第二壁之间移动。 挡板间隔可替代地被描述为使得声波的圆周分量基本上被阻尼,因此不会对不期望的尖叫声产生实质的影响。
-
公开(公告)号:US20130125556A1
公开(公告)日:2013-05-23
申请号:US13301856
申请日:2011-11-22
申请人: James B. Hoke , William Proscia
发明人: James B. Hoke , William Proscia
CPC分类号: F02C9/28 , F02C7/22 , F02C7/228 , F02C7/232 , F05D2260/964 , F05D2270/14 , F23R3/28 , F23R3/34
摘要: A method of noise control from a combustor of a gas turbine engine includes selectively forming a plurality of local circumferential zones with different fuel-air ratios within the combustor.
摘要翻译: 来自燃气涡轮发动机的燃烧器的噪声控制的方法包括在燃烧器内选择性地形成具有不同燃料 - 空气比的多个局部周向区域。
-
公开(公告)号:US08037688B2
公开(公告)日:2011-10-18
申请号:US11527225
申请日:2006-09-26
CPC分类号: F23R3/34 , F23M20/005 , F23R3/50 , F23R2900/00014
摘要: A method for controlling a temperature distribution within a combustor having a plurality of chamber sections comprising controlling a fuel-to-air ratio in the chamber sections. At least two chamber sections have different fuel-to-air ratios to create a non-uniform temperature distribution within the combustor to reduce thermoacoustic instabilities.
摘要翻译: 一种用于控制具有多个室部分的燃烧器内的温度分布的方法,包括控制室部分中的燃料与空气的比例。 至少两个室部分具有不同的燃料与空气的比例,以在燃烧器内产生不均匀的温度分布,以减少热声不稳定性。
-
公开(公告)号:US07401682B2
公开(公告)日:2008-07-22
申请号:US11200563
申请日:2005-08-10
CPC分类号: F04D29/665 , F02K1/827 , F02K3/10 , F05D2260/96 , G10K11/161
摘要: An acoustic liner 20 includes a remote panel 26, a perforated proximate panel 22 transversely spaced from the remote panel and one or more partitions 32 spanning across the space between the panels. At least one baffle 44 cooperates with the partitions to define a resonator chamber 34b and an associated neck 56 for establishing communication between the resonator chamber and a fluid stream G flowing past the proximate panel.
摘要翻译: 声学衬垫20包括远程面板26,与远程面板横向间隔开的穿孔邻近面板22以及穿过面板之间的空间的一个或多个隔板32。 至少一个挡板44与隔板配合以限定谐振器室34b和相关联的颈部56,用于建立谐振腔与流过邻近面板的流体流G之间的连通。
-
公开(公告)号:US20080072605A1
公开(公告)日:2008-03-27
申请号:US11527225
申请日:2006-09-26
IPC分类号: F02C7/26
CPC分类号: F23R3/34 , F23M20/005 , F23R3/50 , F23R2900/00014
摘要: A method for controlling a temperature distribution within a combustor having a plurality of chamber sections comprising controlling a fuel-to-air ratio in the chamber sections. At least two chamber sections have different fuel-to-air ratios to create a non-uniform temperature distribution within the combustor to reduce thermoacoustic instabilities.
摘要翻译: 一种用于控制具有多个室部分的燃烧器内的温度分布的方法,包括控制室部分中的燃料与空气的比例。 至少两个室部分具有不同的燃料与空气的比例,以在燃烧器内产生不均匀的温度分布,以减少热声不稳定性。
-
公开(公告)号:US07337875B2
公开(公告)日:2008-03-04
申请号:US10878806
申请日:2004-06-28
IPC分类号: B64D33/02
CPC分类号: F02C7/24 , B64D2033/0206 , F02C7/045 , F02K1/827 , F05D2260/96 , G10K11/172 , Y02T50/671
摘要: A cooled acoustic liner useful in a fluid handling duct includes a resonator chamber 52 with a neck 56, a face sheet 86, and a coolant plenum 80 residing between the face sheet and the chamber. Coolant bypasses the resonator chamber, rather than flowing through it, resulting in better acoustic admittance than in liners in which coolant flows through the resonator chamber and neck. In one embodiment, the liner also includes a graze shield 88. Openings 40, 38 penetrate both the face sheet and the shield to establish a relatively low face sheet porosity and a relatively high shield porosity. The shielded embodiment of the invention helps prevent a loss of acoustic admittance due to fluid grazing past the liner. Another embodiment that is not necessarily cooled, includes the resonator chamber, low porosity face sheet and high porosity shield, but no coolant plenum for bypassing coolant around the resonator chamber. An associated method of retrofitting an acoustic treatment into a fluid handling module includes installing openings in the module and mounting a resonator box 44 on the module so that the inlets to the resonator necks register with the installed openings.
摘要翻译: 可用于流体处理管道的冷却的声学衬垫包括具有颈部56,面板86和驻留在面板和腔室之间的冷却剂室80的谐振腔52。 冷却液绕过谐振腔,而不是流过谐振腔,导致比冷却剂流过谐振腔和颈部的衬垫更好的声导。 在一个实施例中,衬垫还包括刮板88。 开口40,38穿透面板和屏蔽件以建立相对低的面板孔隙率和相对较高的屏蔽孔隙率。 本发明的屏蔽实施例有助于防止由于通过衬垫的流体放牧导致的声导纳损失。 不一定冷却的另一个实施例包括谐振器腔,低孔隙率面片和高孔隙度屏蔽,但没有用于绕过共振腔的冷却剂的冷却剂室。 将声学处理改造成流体处理模块的相关方法包括在模块中安装开口并将谐振器盒44安装在模块上,使得谐振器颈部的入口与安装的开口对齐。
-
-
-
-
-
-
-
-
-