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公开(公告)号：US5201887A
公开(公告)日：1993-04-13
申请号：US798433
申请日：1991-11-26
IPC分类号： F02K1/82
CPC分类号： F02K1/82
摘要： Damping of the leading edge of a cantilevered mounted liner for the augmentor of a gas turbine engine is obtained by incorporating a generally annular shaped member having a U-shaped cross section and encapsulating the leading edge of the liner in the U-shaped portion of the annular member. A split ring may be included in the U-shaped portion to augment the damping function.
摘要翻译： 通过结合具有U形横截面的大致环形的构件并将衬套的前缘封装在U形部分的U形部分中，获得用于燃气涡轮发动机的增压器的悬臂安装衬套的前缘的阻尼 环形构件。 可以在U形部分中包括开口环以增强阻尼功能。
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公开(公告)号：US5697213A
公开(公告)日：1997-12-16
申请号：US769173
申请日：1996-12-18
CPC分类号： F23R3/002 , F02K1/822 , Y02T50/675
摘要： A liner for a gas turbine engine is provided which includes an outer wall, an inner wall, a plurality of standoffs, a plurality of attachment assemblies, and a plurality of tapered ribs. The inner wall sections each have a first edge and a second edge. The standoffs are attached to the inner wall sections, and separate the inner and outer walls. The attachment assemblies fix at least one standoff, per inner wall section, to the outer wall section. Each tapered rib has a pair of surfaces tapering from a greater end to a lesser end. The tapered ribs are attached to the outer wall, with the lesser end is in contact with the outer wall and the tapered surfaces disposed between, and in contact with, adjacent inner wall sections.
摘要翻译： 提供了一种用于燃气涡轮发动机的衬套，其包括外壁，内壁，多个支座，多个附接组件和多个锥形肋。 内壁部分各自具有第一边缘和第二边缘。 支座附接到内壁部分，并分离内壁和外壁。 附件组件将每个内壁部分至少一个间隔固定到外壁部分。 每个锥形肋具有从较大端到较小端逐渐变细的一对表面。 锥形肋附接到外壁，较小端与外壁和设置在相邻的内壁部分之间并与其相接触的锥形表面接触。
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公开(公告)号：US4799623A
公开(公告)日：1989-01-24
申请号：US116930
申请日：1987-11-04
CPC分类号： F02K1/1223 , F05D2250/323 , F05D2250/324 , Y02T50/671
摘要： A variable area convergent divergent nozzle has floating divergent flaps which shift from a low mode to a high mode depending on internal and external pressure. The lost motion connection which permits this is biased to retain the appropriate mode for long term cruise conditions, to reduce ovalization of the nozzle, and to stabilize and/or dampen vibrations.
摘要翻译： 可变区域会聚发散喷嘴具有浮动发散片，其根据内部和外部压力从低模式转换到高模式。 允许这种偏移的空动连接被偏置以保持用于长期巡航条件的适当模式，以减少喷嘴的椭圆形，以及稳定和/或抑制振动。
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公开(公告)号：US5839663A
公开(公告)日：1998-11-24
申请号：US685323
申请日：1996-07-23
CPC分类号： F02K1/805 , F02K1/1223 , F05D2230/90
摘要： An exhaust nozzle for a gas turbine engine is provided which includes a plurality of flaps and an abradable coating. Each flap includes seal surfaces with depressions disposed therein. The flaps are disposed about a structure within the engine, and are pivotly attached to that structure. Adjacent flaps overlap along the seal surfaces, and movement of the nozzle causes relative motion between the adjacent flaps. The abradable coating is attached to the seal surfaces, and contact between adjacent flaps causes the abradable coating to abrade. The remaining abradable coating fills the depressions within the seal surfaces.
摘要翻译： 提供了一种用于燃气涡轮发动机的排气喷嘴，其包括多个翼片和可磨损涂层。 每个翼片包括其中设置有凹陷的密封表面。 翼片围绕发动机内的结构设置，并且枢转地附接到该结构。 相邻的翼片沿着密封表面重叠，并且喷嘴的运动引起相邻翼片之间的相对运动。 可磨损的涂层附着到密封表面，并且相邻的折板之间的接触导致可磨损的涂层磨损。 剩余的可磨损涂层填充密封表面内的凹陷。
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公开(公告)号：US5704208A
公开(公告)日：1998-01-06
申请号：US567644
申请日：1995-12-05
CPC分类号： F23R3/002 , F02K1/822 , Y02T50/675
摘要： A serviceable liner is provided comprising an outer wall, an inner wall, a plurality of standoffs disposed between the walls, and a plurality of attachment assemblies for attaching the walls to one another. The outer wall includes a plurality of first apertures. The inner wall includes a plurality of sections, each section having at least one second aperture. Each attachment assembly includes a fastener and an insert. An insert is received within each first aperture and a fastener is received within each insert.
摘要翻译： 提供了一种可使用的衬套，其包括外壁，内壁，设置在壁之间的多个支座以及用于将壁彼此附接的多个附接组件。 外壁包括多个第一孔。 内壁包括多个部分，每个部分具有至少一个第二孔。 每个附接组件包括紧固件和插入件。 插入件被容纳在每个第一孔内，并且紧固件被容纳在每个插入物内。
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公开(公告)号：US5367873A
公开(公告)日：1994-11-29
申请号：US9357
申请日：1993-01-26
CPC分类号： F23R3/18
摘要： An improved flameholder for a thrust augmentation combustor includes a toroidal pilot gutter and inner and outer radial gutters, all having U-shaped cross-section and formed from a single piece of metal. The one-piece formation enables design improvements and variations which were not possible in the multiple piece construction of the prior art.
摘要翻译： 用于推力增加燃烧器的改进的火焰稳定器包括环形导向槽和内径和外径向槽，全部具有U形横截面并由单块金属形成。 单件式的结构使得在现有技术的多件结构中不可能实现设计改进和变化。
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公开(公告)号：US5893518A
公开(公告)日：1999-04-13
申请号：US565599
申请日：1995-11-30
CPC分类号： F02K1/12 , Y02T50/672
摘要： The external flaps of a variable exhaust nozzle for a gas turbine engine are attached to the nozzle by a pair of pivotal rods attached to the nozzle's internal support structure and slidably fits into elongated spaced bushings extending along the longitudinal axis of the flaps formed in bosses extending orthogonally from the inner surface of the flaps. The attachment to the support structure includes a unison ball made from composite material that fits into a spherical track formed in a recess in the end of the rods. The method of installation is to insert one of the post into the first bushing that is offset from the second bushing. After the slight engagement of the first post, the second post is pivoted to align with its complementary bushing and the flap is positioned forward to fully engage the rods into the bushings. The aft end hinge of the flap is then attached, A limit pin that is attached to the post travels in a slot designed to limit the travel of the post. Another embodiment includes a damping function in the attachment.
摘要翻译： 用于燃气涡轮发动机的可变排气喷嘴的外部翼片通过附接到喷嘴的内部支撑结构的一对枢转杆附接到喷嘴，并且可滑动地配合到沿着形成在凸起部分中的凸起的纵向轴线延伸的细长间隔的衬套中 从襟翼的内表面正交。 与支撑结构的连接包括由复合材料制成的协调球，其配合到形成在杆的端部中的凹部中的球形轨道。 安装方法是将柱中的一个插入到与第二衬套偏移的第一衬套中。 在第一柱的轻微接合之后，第二柱枢转以与其互补衬套对准，并且挡板向前定位以将杆完全接合到衬套中。 然后安装翼片的后端铰链，附接到柱的限位销在设计成限制柱的行进的狭槽中行进。 另一个实施例包括附件中的阻尼功能。
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公开(公告)号：US5082182A
公开(公告)日：1992-01-21
申请号：US571797
申请日：1990-08-23
申请人： Raymond J. Bruchez, Jr. , George E. Mount , James T. Dixon , Russell H. Hagerman , Wayne K. Movick , Aldo Arena , Jim D. Stewart
发明人： Raymond J. Bruchez, Jr. , George E. Mount , James T. Dixon , Russell H. Hagerman , Wayne K. Movick , Aldo Arena , Jim D. Stewart
CPC分类号： F02K1/008 , F05D2250/31 , Y02T50/671
摘要： An axisymmetric thrust vectoring exhaust nozzle includes a plurality of divergent flaps (30) each supported at the upstream end by a universal joint (32) and at the downstream end by a load link (34) connected to a unison ring (36) positioned by actuators (45).
摘要翻译： 轴对称推力矢量排气喷嘴包括多个发散翼片（30），每个翼片（30）在上游端由万向接头（32）支撑，下游端由连接到一个共振环（36）的负载连杆（34） 致动器（45）。
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