-
公开(公告)号：US11236906B2
公开(公告)日：2022-02-01
申请号：US16664419
申请日：2019-10-25
发明人： Timothy S. Snyder , James B. Hoke
摘要： In accordance with one aspect of the disclosure, a combustor is disclosed. The combustor may include a shell and a liner disposed within the shell. The combustor may further include a grommet at least partially defining a hole communicating through the shell and liner and a cooling channel communicating through the grommet.
-
公开(公告)号：US20210207807A1
公开(公告)日：2021-07-08
申请号：US16736340
申请日：2020-01-07
IPC分类号： F23R3/00
摘要： A combustor for a gas turbine engine includes a combustion chamber defined between an inner shell and an outer shell. The combustor further includes a bulkhead extending between the inner shell and the outer shell. The bulkhead includes a plurality of impingement cooling rings. Each impingement cooling ring of the plurality of impingement cooling rings includes a plurality of impingement cooling holes extending through the bulkhead. The combustor further includes a heat shield panel mounted to the bulkhead so as to define an impingement cooling chamber between the bulkhead and the heat shield panel. The heat shield panel further includes a radial portion between a perimeter and an opening, with respect to an opening center axis, which is free of penetrations. The plurality of impingement cooling holes of each of the plurality of impingement cooling rings are directed toward the radial portion of the heat shield panel.
-
公开(公告)号：US20200318549A1
公开(公告)日：2020-10-08
申请号：US16375018
申请日：2019-04-04
摘要： A combustor for use in a gas turbine engine including: a radially inward heat shield panel; and a radially outward heat shield panel located radially outward of the radially inward heat shield panel, the radially inward heat shield panel and the radially outward heat shield panel being in a facing spaced relationship defining a combustion chamber therebetween, wherein at least one of the radially inward heat shield panel and the radially outward heat shield panel has a non-axisymmetric shape.
-
公开(公告)号：US10317080B2
公开(公告)日：2019-06-11
申请号：US15037484
申请日：2014-12-03
发明人： John S. Tu, Jr. , Timothy S. Snyder , James B. Hoke , James P. Bangerter , Dennis J. Duhamel , David A. Burns
摘要： A liner panel for use in a combustor for a gas turbine engine includes a forward region including a multiple of effusion passages each directed at an orientation consistent with a local swirl direction of combustion gases. Another liner panel for use in a combustor for a gas turbine engine includes a forward region forward of a dilution passage and an aft region aft of the forward region. The forward region includes a multiple of effusion passages each directed generally circumferentially. The aft region includes a multiple of effusion passages each directed at an orientation generally axially. A method of cooling a wall assembly within a combustor of a gas turbine engine includes orienting a multiple of effusion passages within a forward region consistent with a local swirl direction of combustion gases.
-
公开(公告)号：US20190072033A1
公开(公告)日：2019-03-07
申请号：US15697219
申请日：2017-09-06
发明人： Carey Clum , Timothy S. Snyder
摘要： A combustor may comprise a combustion chamber encapsulated by a combustor casing, wherein the combustor casing comprises a casing forward portion, a casing radially inward portion, a casing radially outward portion, and a casing aft portion. The casing radially inward portion may comprise a dirt collector system comprising a hot panel adjacent to the combustion chamber; a cold shell panel coupled to the hot panel such that the hot panel is between the combustion chamber and the cold shell panel; and a dirt collector panel coupled to the cold shell panel such that the cold shell panel is between the hot panel and the dirt collector panel. The cold shell panel and the dirt collector panel at least partially define a dirt collecting space.
-
公开(公告)号：US20150292741A1
公开(公告)日：2015-10-15
申请号：US14680649
申请日：2015-04-07
CPC分类号： F23R3/002 , F02C7/28 , F23R3/005 , F23R3/007 , F23R3/06 , F23R2900/00012 , F23R2900/03042 , F23R2900/03044 , Y02T50/675
摘要： A wall assembly of a combustor for a turbine engine includes a shell and a liner and a sealing interface structure. A cooling cavity is defined between the shell and liner and the sealing interface structure functions to minimize leakage out of the cooling cavity. The sealing interface structure may have a sealing width that is equal to or greater than twice the thickness of the liner and/or may include a chamber located between longitudinal segments of the sealing interface structure that inhibits leakage.
摘要翻译： 用于涡轮发动机的燃烧器的壁组件包括壳体和衬套以及密封接口结构。 在壳体和衬套之间限定了一个冷却腔，并且密封接口结构用于使冷却腔中的泄漏最小化。 密封界面结构可以具有等于或大于衬套厚度的两倍的密封宽度和/或可以包括位于密封界面结构的纵向段之间的室，其阻止泄漏。
-
公开(公告)号：US20130199200A1
公开(公告)日：2013-08-08
申请号：US13832507
申请日：2013-03-15
IPC分类号： F02C7/22
摘要： A fuel system for a gas turbine engine includes a plurality of duplex nozzles arranged on each side of top dead center and a plurality of simplex nozzles. A primary manifold is operable to communicate fuel to a primary flow jet in each of the plurality of duplex nozzles and a secondary manifold is operable to communicate fuel to a secondary flow jet in each of the plurality of duplex nozzles and a secondary flow jet in each of the plurality of simplex nozzles. An equalizer valve that is in communication with both the primary manifold and the secondary manifold distributes fuel at various pressures to both the primary and secondary manifolds.
摘要翻译： 用于燃气涡轮发动机的燃料系统包括布置在上死点的每一侧上的多个双面喷嘴和多个单面喷嘴。 主歧管可操作以将燃料传送到多个双相喷嘴中的每一个中的主流喷射器，并且次级歧管可操作以将燃料传送到多个双相喷嘴中的每一个中的二次流喷射，并且每个二次喷嘴中的次流喷射 的多个单体喷嘴。 与主歧管和次级歧管连通的均衡阀将不同压力的燃料分配到主歧管和次级歧管。
-
公开(公告)号：US11506390B2
公开(公告)日：2022-11-22
申请号：US16705658
申请日：2019-12-06
发明人： Timothy S. Snyder
摘要： A method for operating a fuel injector of a gas turbine engine includes injecting a hydrogen-based primary fuel from a primary fuel passage of the fuel injector directly into a combustion chamber. The primary fuel passage includes a primary fuel outlet located within the combustion chamber. The method further includes injecting a second fuel, different than the hydrogen-based primary fuel, from a secondary fuel passage of the fuel injector into a hood chamber separated from the combustion chamber by a bulkhead. The secondary fuel passage includes a plurality of secondary fuel outlets located within the hood chamber.
-
公开(公告)号：US11346557B2
公开(公告)日：2022-05-31
申请号：US16538544
申请日：2019-08-12
发明人： Timothy S. Snyder
摘要： A guide plate for a swirler assembly is disclosed. In various embodiments, the guide plate includes a guide plate flange configured for engagement with a swirler body having a swirler inlet; and a guide plate collar, the guide plate collar having an aft protrusion with respect to an axial direction extending through the swirler body, the aft protrusion having an aft protrusion tip position configured to be equal to or extend downstream of a swirler inlet forward position with respect to the axial direction and a radially outer surface that forms a radially outer surface angle greater than ninety degrees with respect to a radial direction.
-
公开(公告)号：US11187413B2
公开(公告)日：2021-11-30
申请号：US15697219
申请日：2017-09-06
发明人： Carey Clum , Timothy S. Snyder
摘要： A combustor may comprise a combustion chamber encapsulated by a combustor casing, wherein the combustor casing comprises a casing forward portion, a casing radially inward portion, a casing radially outward portion, and a casing aft portion. The casing radially inward portion may comprise a dirt collector system comprising a hot panel adjacent to the combustion chamber; a cold shell panel coupled to the hot panel such that the hot panel is between the combustion chamber and the cold shell panel; and a dirt collector panel coupled to the cold shell panel such that the cold shell panel is between the hot panel and the dirt collector panel. The cold shell panel and the dirt collector panel at least partially define a dirt collecting space.
-
-
-
-
-
-
-
-
-
搜索结果
54 条记录 (耗时 0.021 秒)
