专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US5161950A Dual alloy turbine disk 失效
标题翻译：双合金涡旋盘
公开(公告)号：US5161950A
公开(公告)日：1992-11-10
申请号：US417096
申请日：1989-10-04
申请人： Daniel D. Krueger , Bruce P. Bardes , Richard G. Menzies , Swami Ganesh , Jeffrey F. Wessels , Sulekh C. Jain , Michael E. Sauby , Keh-Minn Chang
发明人： Daniel D. Krueger , Bruce P. Bardes , Richard G. Menzies , Swami Ganesh , Jeffrey F. Wessels , Sulekh C. Jain , Michael E. Sauby , Keh-Minn Chang
IPC分类号： F01D5/02 , B23K20/22 , C22C19/03 , C22C19/05 , C22F1/00 , C22F1/10 , F01D5/28
CPC分类号： B23K20/22 , F01D5/28 , F05D2300/603 , Y02T50/672 , Y10T29/49316
摘要： A dual alloy disk made from a rim alloy having high stress rupture and creep resistance as well as good hold time fatigue crack resistance and a hub alloy having high tensile strength and good low cycle fatigue crack resistance is described. The dual alloy disk is designed for use as a disk in gas turbine engines operating as high as 1500.degree. F. The hub and rim are joined together at a substantially defect-free joint to form a turbine disk having improved properties in both the hub and rim regions.
摘要翻译：描述了由具有高应力断裂和抗蠕变性以及良好的保持时间疲劳抗开裂性的边缘合金制成的双合金圆盘，以及具有高拉伸强度和良好的低循环疲劳抗开裂性的轮毂合金。双合金盘被设计用作高达1500°F的燃气涡轮发动机中的盘。轮毂和轮辋在基本上无缺陷的接头处连接在一起以形成具有改进的轮毂和轮毂性能的涡轮盘边缘区域。

2. 发明授权

US5106012A Dual-alloy disk system 失效
标题翻译：双合金盘系统
公开(公告)号：US5106012A
公开(公告)日：1992-04-21
申请号：US225907
申请日：1988-07-29
申请人： John M. Hyzak , Timothy E. Howson , Wilford H. Couts, Jr. , Steven H. Reichman , Hugo E. Delgado , Daniel D. Kruger , Michael E. Sauby , Sulekh C. Jain , Bruce P. Bardes , Richard G. Menzies , Swami Ganesh
发明人： John M. Hyzak , Timothy E. Howson , Wilford H. Couts, Jr. , Steven H. Reichman , Hugo E. Delgado , Daniel D. Kruger , Michael E. Sauby , Sulekh C. Jain , Bruce P. Bardes , Richard G. Menzies , Swami Ganesh
IPC分类号： B21J5/00 , B21K1/32 , F01D5/02
CPC分类号： B21K1/32 , B21J5/00 , F01D5/02 , Y10S72/70 , Y10T29/49316 , Y10T29/4932
摘要： Two pieces of metal are bonded together at a surface by placing the two pieces into contact at the surface and forging the two pieces in a die which causes substantial displacement of the metal originally at the surface in a direction parallel to and outwardly from the edges of the surface. In this way, many of the defects which are potentially present at the original surface are displaced with moving metal away from the original contact between the two pieces of metal into sacrificial ribs and the remaining defects are exposed to significant strain. A portion of the displaced metal which contains many of the defects and which forms the sacrificial ribs is removed from the resulting bonded work piece as the sacrificial ribs are removed from the work piece. The result is a bond with superior properties and with a bond surface which can be located very precisely. This system is particularly appropriate for forming dual-alloy high-pressure turbine disks for gas turbines in which an annular peripheral ring of a second super-alloy is bonded to a central core of a first super-alloy. The system is particularly effective if, prior to forging, surfaces to be bonded are closely shape-conforming, are very clean, and are diffusion-bonded using hot isostatic pressing while the surfaces are gas-free. The sacrificial ribs are formed by vents in the impression of the forging dies. The vents are adjacent to the outer edges of the bond surface. The system may be accomplished by using one or more strikes of the same dies, or may include multiple strikes in which only one side of the bond is vented during each strike.
摘要翻译：两块金属在表面上通过将两个部件在表面上接触并且将两个部件锻造在模具中而在一个表面上结合在一起，该模具使原来在表面处的金属在平行于和向外从表面。以这种方式，可能存在于原始表面的许多缺陷被移动的金属从两块金属之间的原始接触件移开到牺牲肋中，并且剩余的缺陷暴露于显着的应变。当牺牲肋从工件上移除时，包含许多缺陷并形成牺牲肋的位移金属的一部分从所得到的粘合工件中被去除。结果是具有优异性能和可以非常精确地定位的粘结表面的粘结。该系统特别适用于形成用于燃气轮机的双合金高压涡轮盘，其中第二超合金的环形外围环结合到第一超级合金的中心芯。如果在锻造之前，要结合的表面紧密形状，非常干净，并且在表面无气体时使用热等静压进行扩散粘合，该系统是特别有效的。牺牲肋由锻造模具的印模形成。通风口与接合表面的外边缘相邻。该系统可以通过使用相同模具的一个或多个冲击来实现，或者可以包括多次冲击，其中在每次冲击期间仅释放粘结件的一侧。

3. 发明授权

US5100050A Method of manufacturing dual alloy turbine disks 失效
标题翻译：制造双合金涡轮盘的方法
公开(公告)号：US5100050A
公开(公告)日：1992-03-31
申请号：US417095
申请日：1989-10-04
申请人： Daniel D. Krueger , Michael E. Sauby , Sulekh C. Jain , Bruce P. Bardes
发明人： Daniel D. Krueger , Michael E. Sauby , Sulekh C. Jain , Bruce P. Bardes
IPC分类号： B21J5/00 , B21K1/32 , B22F3/00 , B23K20/00 , B23K20/02 , C22F1/00 , C22F1/10 , F01D5/02
CPC分类号： B23K20/02 , B21J5/00 , B21K1/32 , F01D5/02 , F05D2300/603 , Y02T50/672 , Y10S72/70
摘要： An article of manufacture having at least a first and a second part, each part having different mechanical properties, compositions, microstructures or combinations thereof, being joined together using a forging process to yield a substantially defect-free joint region. The article in the form of a turbine disk is particularly suited for use in a gas turbine engine in which the hub or inner portion must be resistant to low cycle fatigue and have high strength, while the rim or outer portion must be resistant to stress rupture failure and creep failure.
摘要翻译：具有至少第一部分和第二部分的制品，每个部分具有不同的机械性能，组成，微观结构或其组合，使用锻造方法连接在一起以产生基本上无缺陷的接合区域。涡轮盘形式的物品特别适用于燃气轮机发动机，其中轮毂或内部部分必须抵抗低循环疲劳并具有高强度，而轮辋或外部必须抵抗应力破裂故障和蠕变故障。

4. 发明授权

US5413752A Method for making fatigue crack growth-resistant nickel-base article 失效
标题翻译：疲劳裂纹生长耐蚀镍基制品的制备方法
公开(公告)号：US5413752A
公开(公告)日：1995-05-09
申请号：US957113
申请日：1992-10-07
申请人： Robert D. Kissinger , Michael E. Sauby , Richard G. Menzies , Allen J. Paxson
发明人： Robert D. Kissinger , Michael E. Sauby , Richard G. Menzies , Allen J. Paxson
IPC分类号： B22F3/24 , C22C1/04 , C22F1/10 , B22F3/00
CPC分类号： C22C1/0433 , B22F3/24 , C22F1/10
摘要： Fatigue crack growth-resistant articles are made from powder metal or cast and wrought gamma prime precipitation strengthened nickel-base superalloy material, wherein a relatively high predetermined minimum strain rate, .epsilon..sub.min, is employed during hot working at or near the alloy's recrystallization temperature; or alternatively a relatively high strain level, .epsilon..sub.min, is employed during cold or warm working at temperatures below the alloy's recrystallization temperature. The worked articles are characterized by a uniform fine grain size, and grains which coarsen uniformly after heating at the supersolvus solutioning temperature, thereby alleviating non-uniform grain growth within the material.
摘要翻译：疲劳裂纹生长抗性制品由粉末金属或铸造和锻造的γ析出强化的镍基超合金材料制成，其中在合金的再结晶温度或接近合金的热加工期间采用相对较高的预定最小应变速率εmin; 或者在低于合金的再结晶温度的温度下，在冷或热加工期间采用相对高的应变水平，εmin。加工制品的特征在于均匀的细粒度，以及在超溶解温度下加热后均匀地粗化的晶粒，从而减轻材料内不均匀的晶粒生长。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式