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1.发明申请公开(公告)号：US20140230441A1
公开(公告)日：2014-08-21
申请号：US13768038
申请日：2013-02-15
申请人： Clinton A. Mayer , Jesse Eng , Cheryl A. Schopf
发明人： Clinton A. Mayer , Jesse Eng , Cheryl A. Schopf
IPC分类号： F02C7/12
CPC分类号： F02C7/12 , F01D25/26 , F05D2260/231
摘要： A heat shield manifold system for an inner casing between a compressor and turbine assembly is disclosed. The heat shield manifold system protects the outer case from high temperature compressor discharge air, thereby enabling the outer case extending between a compressor and a turbine assembly to be formed from less expensive materials than otherwise would be required. In addition, the heat shield manifold system may be configured such that compressor bleed air is passed from the compressor into the heat shield manifold system without passing through a conventional flange to flange joint that is susceptible to leakage.
摘要翻译： 公开了一种用于压缩机和涡轮机组件之间的内壳的隔热罩歧管系统。 隔热罩歧管系统保护外壳免受高温压缩机排放空气的影响，从而使压缩机和涡轮机组件之间延伸的外壳由不需要的材料形成。 此外，隔热罩歧管系统可以被配置成使得压缩机排出的空气从压缩机传递到隔热管歧管系统中，而不会通过常规的法兰到容易泄漏的法兰接头。
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公开(公告)号：US09714611B2
公开(公告)日：2017-07-25
申请号：US13768038
申请日：2013-02-15
申请人： Clinton A. Mayer , Jesse Eng , Cheryl A. Schopf
发明人： Clinton A. Mayer , Jesse Eng , Cheryl A. Schopf
CPC分类号： F02C7/12 , F01D25/26 , F05D2260/231
摘要： A heat shield manifold system for an inner casing between a compressor and turbine assembly is disclosed. The heat shield manifold system protects the outer case from high temperature compressor discharge air, thereby enabling the outer case extending between a compressor and a turbine assembly to be formed from less expensive materials than otherwise would be required. In addition, the heat shield manifold system may be configured such that compressor bleed air is passed from the compressor into the heat shield manifold system without passing through a conventional flange to flange joint that is susceptible to leakage.
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公开(公告)号：US20050242525A1
公开(公告)日：2005-11-03
申请号：US10837006
申请日：2004-04-30
申请人： Stefan Dahlke , Jesse Eng , John Glessner , Daniel Hofmann , Roland Liebe , Kenneth Tamaddoni-Jahromi
发明人： Stefan Dahlke , Jesse Eng , John Glessner , Daniel Hofmann , Roland Liebe , Kenneth Tamaddoni-Jahromi
CPC分类号： F16J15/028 , F23M5/02 , F23M2900/05005 , F23R3/002 , F23R2900/00012
摘要： An inventive hot gas seal for sealing an opening, e.g. a gap or hole, in a heat shield element or between heat shield elements of a heat shield or a liner comprises at least one resilient portion for providing a force which is designed such that the hot gas seal can be held in said opening by said force and/or that the sealing efficiency of the hot gas seal is increased by said force. Thus, further means for holding the seal in place and/or for increasing the sealing efficiency are not necessary. The invention is particularly useful if the design of said resilient portion is such that the force provides a holding action and increases the sealing efficiency, at the same time.
摘要翻译： 用于密封开口的本发明的热气密封，例如， 隔热元件中的间隙或孔，或隔热罩或衬套的隔热元件之间的间隙或孔包括至少一个用于提供力的弹性部分，该弹性部分被设计成使得热气体密封件能够通过所述力保持在所述开口中 和/或通过所述力增加热气密封的密封效率。 因此，不需要用于将密封件保持在适当位置和/或用于提高密封效率的另外的装置。 如果所述弹性部分的设计使得力同时提供保持作用并提高密封效率，则本发明是特别有用的。
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公开(公告)号：US06848260B2
公开(公告)日：2005-02-01
申请号：US10252208
申请日：2002-09-23
申请人： David D. North , Arthur J. Harris, Jr. , Hank Reid , Jesse Eng
发明人： David D. North , Arthur J. Harris, Jr. , Hank Reid , Jesse Eng
摘要： A combustor (40) for a gas turbine engine is provided with a premix pilot fuel stage (42) in order to reduce the emission of oxides of nitrogen from the engine. An in-service engine may be modified to add the premix pilot fuel stage by delivering premix pilot fuel to a ring manifold (42) for tip-feeding a premix pilot fuel outlet member such as a swirler vane (78) or fuel peg (124). In this manner, complex and expensive components such as the top hat (46), support housing (48) and diffusion pilot burner assembly (44) may be used without modification. Thermal stresses caused by the differential cooling of the ring manifold by the premix pilot fuel (96) are reduced by a heat shield (94) installed within the manifold.
摘要翻译： 用于燃气涡轮发动机的燃烧器（40）设置有预混合引燃燃料级（42），以便减少来自发动机的氮氧化物的排放。 可以修改在役发动机以通过将预混合引燃燃料输送到环形歧管（42）来添加预混合引燃燃料级，用于尖端馈送预混燃料出口部件，例如旋流器叶片（78）或燃料栓（124） ）。 以这种方式，可以使用诸如顶帽（46），支撑壳体（48）和扩散导向燃烧器组件（44）的复杂且昂贵的部件。 由预混合引燃燃料（96）对环形歧管进行差速冷却引起的热应力由安装在歧管内的隔热罩（94）减少。
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公开(公告)号：US20140367925A1
公开(公告)日：2014-12-18
申请号：US14184063
申请日：2014-02-19
申请人： Stefan Dahlke , Jesse Eng , John Carl Glessner , Daniel Hofmann , Kenneth Michael Tamaddoni-Jahromi
发明人： Stefan Dahlke , Jesse Eng , John Carl Glessner , Daniel Hofmann , Roland Liebe , Kenneth Michael Tamaddoni-Jahromi
IPC分类号： F16J15/02
CPC分类号： F16J15/028 , F23M5/02 , F23M2900/05005 , F23R3/002 , F23R2900/00012
摘要： A hot gas seal for sealing an opening in a heat shield element or between heat shield elements of a heat shield includes a resilient portion for providing a force which is designed such that the hot gas seal can be held in the opening by the force and/or that the sealing efficiency of the hot gas seal is increased by the force. Further, a hot gas seal assembly for sealing an opening in a heat shield element or between heat shield elements of a heat shield against a hot gas is provided, the assembly including a sealing body and a further sealing element which is in a solid state at room temperature and in a high viscosity liquid state at a temperature of the hot gas.
摘要翻译： 用于密封隔热元件中的开口或隔热罩的隔热元件之间的热气体密封件包括用于提供力的弹性部分，其被设计成使得热气体密封件能够通过该力保持在开口中和/ 或者通过力增加热气密封的密封效率。 此外，提供了一种用于密封隔热元件中的开口或隔热件的热屏蔽元件与热气体的热气密封组件，该组件包括密封体和另一密封元件，该密封体和固定状态处于固态 室温下，在热气体的温度下处于高粘度液体状态。
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公开(公告)号：US08695989B2
公开(公告)日：2014-04-15
申请号：US10837006
申请日：2004-04-30
申请人： Stefan Dahlke , Jesse Eng , John Carl Glessner , Daniel Hofmann , Roland Liebe , Kenneth Michael Tamaddoni-Jahromi
发明人： Stefan Dahlke , Jesse Eng , John Carl Glessner , Daniel Hofmann , Roland Liebe , Kenneth Michael Tamaddoni-Jahromi
IPC分类号： F16J15/02
CPC分类号： F16J15/028 , F23M5/02 , F23M2900/05005 , F23R3/002 , F23R2900/00012
摘要： An inventive hot gas seal for sealing an opening, e.g. a gap or hole, in a heat shield element or between heat shield elements of a heat shield or a liner comprises at least one resilient portion for providing a force which is designed such that the hot gas seal can be held in said opening by said force and/or that the sealing efficiency of the hot gas seal is increased by said force. Thus, further means for holding the seal in place and/or for increasing the sealing efficiency are not necessary. The invention is particularly useful if the design of said resilient portion is such that the force provides a holding action and increases the sealing efficiency, at the same time.
摘要翻译： 用于密封开口的本发明的热气密封，例如， 隔热元件中的间隙或孔，或隔热罩或衬套的隔热元件之间的间隙或孔包括至少一个用于提供力的弹性部分，该弹性部分被设计成使得热气体密封件能够通过所述力保持在所述开口中 和/或通过所述力增加热气密封的密封效率。 因此，不需要用于将密封件保持在适当位置和/或用于提高密封效率的另外的装置。 如果所述弹性部分的设计使得力同时提供保持作用并提高密封效率，则本发明是特别有用的。
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公开(公告)号：US20050242526A1
公开(公告)日：2005-11-03
申请号：US10837007
申请日：2004-04-30
申请人： Stefan Dahlke , Jesse Eng , John Glessner , Daniel Hofmann , Roland Liebe , Kenneth Tamaddoni-Jahromi
发明人： Stefan Dahlke , Jesse Eng , John Glessner , Daniel Hofmann , Roland Liebe , Kenneth Tamaddoni-Jahromi
CPC分类号： F01D11/005 , F01D25/12 , F05D2260/20 , F05D2300/21 , F05D2300/612 , F16J15/064 , F23M5/00 , F23M2900/05005 , F23R3/002 , F23R2900/00012
摘要： An inventive hot gas seal comprises a sealing body and means for allowing a cooling fluid, preferably cooling air, to flow through the interior of the sealing body. Such a hot gas seal can be effectively cooled by guiding a cooling fluid through the interior of the sealing body.
摘要翻译： 本发明的热气体密封件包括密封体和用于允许冷却流体（优选冷却空气）流过密封体内部的装置。 通过引导冷却流体通过密封体的内部，可以有效地冷却这种热气体密封。
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公开(公告)号：US08070435B1
公开(公告)日：2011-12-06
申请号：US12405563
申请日：2009-03-17
申请人： Jesse Eng
发明人： Jesse Eng
IPC分类号： F01D25/00
CPC分类号： F01D25/164 , F05D2240/50 , F16C19/26 , F16C27/04 , F16C2360/23 , Y02T50/671
摘要： A split ring wedge bearing friction damper for an aero engine that allows the engine to operate without an oil tank, a pump, and a lubricant cooler, the friction damper having a damper ring and a wedge ring that both have wedge surfaces in contact so that an axial load can be applied to the bearing outer race to provide damping to the bearing, and so that the damper ring can also have a radial displacement to produce a radial load on the damper ring against the stator bearing support surface in which the axial load provides the friction damping and the radial load eliminates lost motion for maximum damping.
摘要翻译： 一种用于航空发动机的分裂环楔形轴承摩擦阻尼器，其允许发动机在没有油箱，泵和润滑剂冷却器的情况下操作，所述摩擦阻尼器具有阻尼环和楔形环，两者都具有接触的楔形表面，使得 可以将轴向负载施加到轴承外圈以对轴承提供阻尼，并且使得阻尼环也可以具有径向位移，以在阻尼环上产生相对于定子轴承支撑表面的径向载荷，其中轴向载荷 提供摩擦阻尼和径向载荷消除了最大阻尼的运动。
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公开(公告)号：US4822244A
公开(公告)日：1989-04-18
申请号：US108528
申请日：1987-10-15
申请人： Mark S. Maier , Jesse Eng
发明人： Mark S. Maier , Jesse Eng
CPC分类号： F01D5/082 , F01D5/3015
摘要： The performance of a TOBI for a gas turbine engine is improved by providing bypass apertures in the housing of said TOBI for directing a stream of air into the seal sealing the TOBI compartment and bypassing the nozzles of the TOBI to reduce the size of the plume of the TOBI cooling air.
摘要翻译： 通过在所述TOBI的壳体中提供旁通孔来引导用于燃气涡轮发动机的TOBI的性能，用于将空气流引导到密封TOBI室中的密封件中并绕过TOBI的喷嘴，以减小TOBI的羽流的尺寸 TOBI冷却空气。
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公开(公告)号：US5224824A
公开(公告)日：1993-07-06
申请号：US896746
申请日：1992-06-09
申请人： Jesse Eng
发明人： Jesse Eng
CPC分类号： F01D25/246 , F01D25/265 , F01D25/285 , F04D29/522 , F04D29/644 , F05D2230/64
摘要： The last stages of a compressor section of a gas turbine engine that utilizes a drum rotor and segmented stator supported to an axially split outer case suspends the segmented stator case to a full hoop outer case so that the segmented stator displaces axially and thermally grows circumferentially while being constrained radially. A method of assembly and disassembly of the full hoop outer case is provided.
摘要翻译： 燃气涡轮发动机的压缩机部分的最后阶段利用鼓转子和支承在轴向剖开的外壳上的分段定子将分段的定子壳悬挂在一个完整的环外壳上，使得分段的定子轴向位移并沿周向热生长，同时 被径向约束。 提供了一种组装和拆卸全套外壳的方法。
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