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公开(公告)号:US5375973A
公开(公告)日:1994-12-27
申请号:US993862
申请日:1992-12-23
CPC分类号: F01D25/12 , F01D11/08 , Y02T50/67 , Y02T50/675
摘要: This disclosure describes a cooling and manufacturing enhancement for gas turbine engine outer air seals. The invention provides convective cooling in a counter-flow array, internal heat transfer augmentation through the use of boundary layer trip-strips, coolant Mach number control through the use of tapered convective channels, inter-segment purge without additional secondary cooling air, and is castable.
摘要翻译: 本公开描述了用于燃气涡轮发动机外部空气密封件的冷却和制造增强。 本发明提供逆流阵列中的对流冷却,通过使用边界层跳闸条的内部热传递增强,通过使用锥形对流通道的冷却剂马赫数控制,不具有另外的二次冷却空气的段间吹扫,并且 浇注料
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2.
公开(公告)号:US5374161A
公开(公告)日:1994-12-20
申请号:US166426
申请日:1993-12-13
申请人: George W. Kelch , Thomas A. Auxier
发明人: George W. Kelch , Thomas A. Auxier
CPC分类号: F01D11/005 , F01D11/08 , F01D25/12 , Y02T50/675
摘要: A cooling enhancement for a gas turbine engine blade outer air seal is made up of a plurality of arcuate seal segments, and each one has one or more internal cooling passages. Each segment has a supply surface opposite and in spaced relation to a sealing surface, and first and second end surfaces extending from the sealing surface to the supply surface. Each of the end surfaces includes a substantially planar perpendicular surface and a substantially planar canted surface intersecting at an included angle of between 100 degrees and 140 degrees, and the supply surface has a plurality of cooling orifices adjacent the second end surface. At least one cooling passage extends from the first end surface towards the second end surface, and each cooling passage intersects the first end surface and terminates short of the second end surface. Each cooling passage communicates with the supply surface through at least one of the cooling orifices. Protruding from at least one of the substantially canted surfaces is a plurality of stand-off pedestals that are integral with the canted surface.
摘要翻译: 用于燃气涡轮发动机叶片外部空气密封件的冷却增强由多个弓形密封段组成,并且每个具有一个或多个内部冷却通道。 每个段具有与密封表面相对并且间隔开的供应表面,以及从密封表面延伸到供给表面的第一和第二端表面。 每个端面包括基本上平面的垂直表面和以100度和140度之间的夹角相交的基本上平面的倾斜表面,并且供给表面具有与第二端面相邻的多个冷却孔。 至少一个冷却通道从第一端面朝向第二端面延伸,并且每个冷却通道与第一端面相交并且终止于第二端表面之外。 每个冷却通道通过冷却孔中的至少一个与供给表面连通。 从基本上倾斜的表面中的至少一个突起是与倾斜表面成一体的多个悬置基座。
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公开(公告)号:US5201530A
公开(公告)日:1993-04-13
申请号:US778554
申请日:1991-10-18
申请人: George W. Kelch , John L. Shade
发明人: George W. Kelch , John L. Shade
IPC分类号: F16J15/32
CPC分类号: F16J15/3288
摘要: The present invention is a brush seal for use between two components which move relative to each other. The brush seal has multiple layers of bristles, and the bristles within a particular layer have the same cross-sectional area or "thickness". The layers are arranged in the order of increasing thickness, with the bristles of the layer that forms the high pressure face of the brush seal having the smallest cross-sectional area. The larger bristles support the smaller bristles, and a backing plate supports the larger bristles.
摘要翻译: 本发明是用于在相对于彼此移动的两个部件之间使用的刷子密封件。 刷密封具有多层刷毛,并且特定层内的刷毛具有相同的横截面面积或“厚度”。 这些层以增加的厚度的顺序排列,形成刷密封件的高压面的层的刷毛具有最小的横截面积。 较大的刷毛支撑较小的刷毛,并且背板支撑较大的刷毛。
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4.
公开(公告)号:US4907943A
公开(公告)日:1990-03-13
申请号:US198330
申请日:1988-05-25
申请人: George W. Kelch
发明人: George W. Kelch
IPC分类号: F01D3/04
CPC分类号: F01D3/04
摘要: In a gas turbine engine a novel method and apparatus that measures axial thrust loads in engine bearings is characterized by a controller which dynamically selects axial loads on an engine thrust bearing by varying internal gas pressures in bearing trim cavities in accordance with a predetermined schedule.
摘要翻译: 在燃气涡轮发动机中,测量发动机轴承中的轴向推力载荷的新颖方法和装置的特征在于控制器,该控制器根据预定的时间表,通过改变轴承装饰空腔中的内部气体压力来动态地选择发动机推力轴承上的轴向载荷。
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公开(公告)号:US5649806A
公开(公告)日:1997-07-22
申请号:US155989
申请日:1993-11-22
申请人: Joseph A. Scricca , George W. Kelch
发明人: Joseph A. Scricca , George W. Kelch
CPC分类号: F01D11/08 , F05D2240/11 , F05D2260/20 , F05D2260/221 , Y02T50/67 , Y02T50/676
摘要: This disclosure describes a cooling enhancement for gas turbine engine outer air seals. The invention provides heat transfer using impingement cooling and convective cooling through the use of tortuous cooling air passages, and film effective film cooling through the use of cooling air discharge slots that are oriented so as to discharge coolant into the working fluid flowpath with a minimum of momentum exchange between the cooling air and the working fluid.
摘要翻译: 本公开描述了用于燃气涡轮发动机外部空气密封件的冷却增强。 本发明通过使用曲折的冷却空气通道提供使用冲击冷却和对流冷却的热传递,以及通过使用冷却空气排出槽来进行膜有效的膜冷却,所述冷却空气排出槽被定向成将冷却剂排放到工作流体流动路径中, 冷却空气与工作液体之间的动量交换。
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公开(公告)号:US4040161A
公开(公告)日:1977-08-09
申请号:US635188
申请日:1975-11-25
申请人: George W. Kelch
发明人: George W. Kelch
CPC分类号: B21J13/08 , B21K1/36 , Y10T29/53683
摘要: A method is disclosed of removing a plurality of rim blade dies around the circumference of a disc while the disc, blades and blade dies are at a temperature approximating those during the forging operation. The upper disc forming die is removed along with a restraining back-up member around the rim blade dies and the rim blade dies are forced radially outwardly to prevent interference between the blade dies and blades during their cool down period. A blade die removal tool has a plurality of individual radial arms extending outwardly from a central hub. The free ends of the arms engage the blade dies and the ram of the press moves the central hub downwardly to move the blade dies radially outwardly.
摘要翻译: 公开了一种方法,用于在盘,刀片和刀片模具处于与锻造操作期间接近的温度的温度下,围绕圆周的周边移除多个轮辋刀片模具。 上盘形成模具与围绕边缘刀片模具的限制性支撑构件一起被移除,并且边缘刀片模具被径向向外强制以防止在其冷却期间叶片管芯和刀片之间的干涉。 刀片去除工具具有从中心毂向外延伸的多个单独的径向臂。 臂的自由端与刀片接合,并且压力机的冲头将中心毂向下移动以使刀片径向向外移动。
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