公开(公告)号：US5353865A

公开(公告)日：1994-10-11

申请号：US860397

申请日：1992-03-30

申请人： Eugene F. Adiutori ,  Byron A. Pritchard, Jr. ,  Stephen Aleshin

发明人： Eugene F. Adiutori ,  Byron A. Pritchard, Jr. ,  Stephen Aleshin

IPC分类号： F28F13/02 ,  F28F13/18

CPC分类号： F28F13/185 ,  F28F13/02 ,  F23R2900/03044 ,  F23R2900/03045 ,  Y02T50/675 ,  Y10S165/908

摘要： An improved heat transfer assembly includes a textured impingement surface and means for impinging cooling air directly upon the textured surface. A component includes a surface textured to increase convective heat transfer with minimal increase in resistance to conductive heat transfer through the component. The textured surface can comprise an array of closely spaced hemispherically shaped protuberances. A method is disclosed for texturing a surface with discrete laser welds.

摘要翻译： 改进的传热组件包括纹理化的冲击表面和用于将冷却空气直接撞击在纹理表面上的装置。 组件包括纹理化的表面以增加对流传热，同时对通过部件的传导热传递的阻力的最小增加。 纹理表面可以包括紧密间隔开的半球形突起的阵列。 公开了一种用离散激光焊缝对表面进行纹理化的方法。

公开(公告)号：US5321951A

公开(公告)日：1994-06-21

申请号：US89058

申请日：1993-07-08

申请人： Stephen W. Falls ,  Eric J. Kress ,  Joseph F. Savelli ,  James N. Cooper ,  Byron A. Pritchard, Jr.

发明人： Stephen W. Falls ,  Eric J. Kress ,  Joseph F. Savelli ,  James N. Cooper ,  Byron A. Pritchard, Jr.

IPC分类号： F23R3/14 ,  F23R3/34 ,  F23R3/60 ,  F02C7/22

CPC分类号： F23R3/34 ,  F23R3/14 ,  F05B2260/201 ,  F05B2260/222 ,  Y02T50/675

摘要： A carburetor for the combustor of a gas turbine engine wherein a swirler and a venturi cooperate to atomize and mix air and fuel for the combustor, wherein a downstream mounted integrally formed sleeve and splash plate is provided to control the flow of the air/fuel mixture into the combustor. The integral splash plate and sleeve has protuberances formed on its upstream surface to increase the area impinged by cooling air and thereby enhance cooling of the splash plate flange thereof.

摘要翻译： 一种用于燃气涡轮发动机的燃烧器的化油器，其中旋流器和文丘里管配合雾化和混合用于燃烧器的空气和燃料，其中提供下游安装的整体形成的套筒和飞溅板以控制空气/燃料混合物的流动 进入燃烧器。 一体的飞溅板和套筒具有在其上游表面上形成的突起，以增加被冷却空气冲击的面积，从而增强了其飞溅板凸缘的冷却。

公开(公告)号：US06474070B1

公开(公告)日：2002-11-05

申请号：US09095209

申请日：1998-06-10

申请人： Allen M. Danis ,  Byron A. Pritchard, Jr. ,  Keith K. Taylor ,  Richard W. Stickles ,  Willard J. Dodds ,  Donald L. Gardner

发明人： Allen M. Danis ,  Byron A. Pritchard, Jr. ,  Keith K. Taylor ,  Richard W. Stickles ,  Willard J. Dodds ,  Donald L. Gardner

IPC分类号： F02G300

CPC分类号： F23R3/343 ,  F02G1/055 ,  F23R3/50

摘要： A gas turbine engine combustor includes outer and inner liners joined together at an annular dome. Outer and inner air swirlers and cooperating fuel injectors are mounted in two rows in the combustor dome. The fuel injectors are joined to a common fuel manifold for simultaneously channeling fuel thereto over an operating range from idle to full power for reducing exhaust emissions.

摘要翻译： 燃气涡轮发动机燃烧器包括以环形圆顶连接在一起的外衬里和内衬。 外部和内部空气旋流器和配合的燃料喷射器安装在燃烧器穹顶中的两排中。 燃料喷射器连接到公共燃料歧管，用于在从怠速到全功率的操作范围内同时将燃料引导到其中，以减少废气排放。

公开(公告)号：US06212870B1

公开(公告)日：2001-04-10

申请号：US09158409

申请日：1998-09-22

申请人： James E. Thompson ,  Byron A. Pritchard, Jr. ,  Mark M. Glevicky ,  Paul J. Ogden

发明人： James E. Thompson ,  Byron A. Pritchard, Jr. ,  Mark M. Glevicky ,  Paul J. Ogden

IPC分类号： F23R314

CPC分类号： F23R3/283 ,  F23R3/14 ,  F23R3/60 ,  Y02T50/675

摘要： Assembly of the combustor dome in a gas turbine engine is facilitated by providing a self-fixturing configuration. The combustor dome assembly is made up of a dome plate having a plurality of swirler assemblies mounted therein. Each swirler assembly is provided with a locating pin that extends between the dome plate and the swirler assembly for positioning the swirler assembly with respect to the dome plate without the use of fixturing tools. Preferably, the swirler assembly includes a swirl cup and an outlet sleeve mounted in the dome plate. The locating pin is pressed into a hole formed in the swirl cup. One end of the pin is received in a slot formed in the dome plate, and the other end of the pin is received in a slot formed in the outlet sleeve. Thus, the locating pin sets the circumferential orientation of the swirler assembly in relation to the dome plate. A shoulder on the swirl cup sets the cup axially with respect to the dome plate, and a shoulder on the outlet sleeve sets the sleeve axially with respect to the swirl cup.

摘要翻译： 燃气涡轮发动机中的燃烧器穹顶的组装通过提供自固定构型而被促进。 燃烧器穹顶组件由安装在其中的多个旋流器组件的圆顶板构成。 每个旋流器组件设置有定位销，该定位销在圆顶板和旋流器组件之间延伸，用于相对于圆顶板定位旋流器组件而不使用夹具。 优选地，旋流器组件包括旋转杯和安装在圆顶板中的出口套筒。 定位销被压入形成在旋转杯中的孔中。 销的一端容纳在形成在圆顶板中的槽中，并且销的另一端容纳在形成在出口套筒中的槽中。 因此，定位销相对于圆顶板设置旋流器组件的圆周方向。 旋转杯上的肩部将杯子相对于圆顶板轴向设置，并且出口套筒上的肩部将套筒相对于旋转杯轴向设置。

公开(公告)号：US5285635A

公开(公告)日：1994-02-15

申请号：US81482

申请日：1993-06-22

申请人： Joseph F. Savelli ,  Byron A. Pritchard, Jr.

发明人： Joseph F. Savelli ,  Byron A. Pritchard, Jr.

IPC分类号： F23R3/34 ,  F23R3/42 ,  F23R3/46 ,  F02C3/14

CPC分类号： F23R3/34 ,  F23R3/42

摘要： A double annular combustor having concentrically disposed inner and outer annular combustors is provided with inner and outer dome plates. Each dome plate has an inner portion and an outer portion. A cowl structure having an inner portion, an outer portion and a middle portion is also provided. The cowl outer portion is connected to the outer dome plate outer portion, the cowl inner portion is connected to the inner dome plate inner portion, and the cowl middle portion is connected to the outer dome plate inner portion and the inner dome plate outer portion. at an outer end, an inner end, and a middle portion. Additionally, the inner and outer annular combustors may lie in distinct radial planes, whereby the dome plate of the downstream annular combustor includes a section extending upstream to the cowl middle portion.

摘要翻译： 具有同心配置的内外环形燃烧器的双环形燃烧器设置有内圆顶板和外圆顶板。 每个圆顶板具有内部部分和外部部分。 还提供了具有内部部分，外部部分和中间部分的整流罩结构。 整流罩外部连接到外圆顶板外部，前后内连接到内圆顶板内部，并且整流罩中部连接到外圆顶板内部和内圆顶板外部。 在外端，内端和中间部分。 此外，内环形燃烧器和外环形燃烧器可以位于不同的径向平面中，由此下游环形燃烧器的圆顶板包括在整流罩中部的上游延伸的部分。