公开(公告)号：US09457531B2

公开(公告)日：2016-10-04

申请号：US14326819

申请日：2014-07-09

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Milton Ortiz

IPC: B29D99/00 ,  F01D5/34 ,  B22C9/02 ,  B22D19/00 ,  F01D5/30

CPC classification number: B29D99/0025 ,  B22C9/02 ,  B22D19/00 ,  F01D5/30 ,  F01D5/34 ,  F05D2230/21 ,  F05D2230/236 ,  F05D2300/175 ,  F05D2300/6033 ,  Y02T50/672 ,  Y02T50/673

Abstract: A bi-cast turbine rotor disk and method of forming the same are provided. The disk includes a ring and a blade. The ring comprises a superalloy that includes a plurality of elements, and the blade extends from the ring. The blade comprises a non-metallic ceramic matrix composite, and at least one element from the superalloy of the ring is diffused into the non-metallic ceramic matrix composite of the blade.

Abstract translation: 提供了一种双流型涡轮转子盘及其制造方法。 盘包括一个环和一个叶片。 该环包括包括多个元件的超级合金，并且该刀片从该环延伸。 叶片包括非金属陶瓷基复合材料，并且来自环的超合金的至少一种元素被扩散到叶片的非金属陶瓷基复合材料中。

公开(公告)号：US20140318729A1

公开(公告)日：2014-10-30

申请号：US14326819

申请日：2014-07-09

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Milton Ortiz

IPC: B29D99/00 ,  B22C9/02 ,  B22D19/00

CPC classification number: B29D99/0025 ,  B22C9/02 ,  B22D19/00 ,  F01D5/30 ,  F01D5/34 ,  F05D2230/21 ,  F05D2230/236 ,  F05D2300/175 ,  F05D2300/6033 ,  Y02T50/672 ,  Y02T50/673

Abstract: A bi-cast turbine rotor disk and method of forming the same are provided. The disk includes a ring and a blade. The ring comprises a superalloy that includes a plurality of elements, and the blade extends from the ring. The blade comprises a non-metallic ceramic matrix composite, and at least one element from the superalloy of the ring is diffused into the non-metallic ceramic matrix composite of the blade.

Abstract translation: 提供了一种双流型涡轮转子盘及其制造方法。 盘包括一个环和一个叶片。 该环包括包括多个元件的超级合金，并且该刀片从该环延伸。 叶片包括非金属陶瓷基复合材料，并且来自环的超合金的至少一种元素被扩散到叶片的非金属陶瓷基复合材料中。

公开(公告)号：US10605086B2

公开(公告)日：2020-03-31

申请号：US13681675

申请日：2012-11-20

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： George E. Zurmehly ,  Milton Ortiz ,  Kin Poon ,  Michael Vinup ,  Ardeshir Riahi

IPC: F01D5/12 ,  F01D5/14 ,  F01D5/28

Abstract: A vane assembly includes first and second annular metal rings configured to accept a compressed gas flow therebetween. The first and second annular rings each include a cutout portion. The assembly further includes a ceramic matrix composite vane configured as an airfoil having a blunt rounded nose and a flattened and tapered tail. A first radial end of the vane is rigidly disposed on the first annular ring and a second radial end of the vane is slidably disposed within the cutout portion of the second annular ring such that the vane is encompassed by the first and second annular rings. The vane includes a hollow through opening portion extending radially therethrough. Still further, the assembly includes a metallic elongated member disposed within and extending through the hollow portion of vane and through the cutout portion of the first annular ring.

公开(公告)号：US20160146024A1

公开(公告)日：2016-05-26

申请号：US14551293

申请日：2014-11-24

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Mark C. Morris ,  Daira Legzdina ,  Don Mittendorf ,  Milton Ortiz ,  Ardeshir Riahi ,  Michael Vinup

IPC: F01D5/30 ,  F01D5/28 ,  B23K20/12 ,  C22F1/18 ,  B23K31/02 ,  B23K20/00 ,  C22F1/10 ,  F01D5/18 ,  B23K31/12

CPC classification number: F01D5/3061 ,  B23K20/002 ,  B23K20/1205 ,  B23K31/02 ,  B23K31/12 ,  B23P15/006 ,  C22F1/10 ,  C22F1/183 ,  F01D5/187 ,  F01D5/28 ,  F01D5/288 ,  F05D2220/32 ,  F05D2230/10 ,  F05D2230/239 ,  F05D2230/411 ,  F05D2230/90 ,  F05D2240/30 ,  F05D2260/20 ,  F05D2260/941 ,  F05D2300/17 ,  F05D2300/174

Abstract: Hybrid bonded turbine rotors and methods for manufacturing the same are provided. A hybrid bonded turbine rotor comprises a turbine disk and a plurality of turbine blades each metallurgically bonded to a corresponding raised blade attachment surface of a plurality of raised blade attachment surfaces of the turbine disk to define a bond plane located at a selected radial position. Turbine disk has a rim portion comprising a live rim of circumferentially continuous material and a plurality of live rim notches in an outer periphery of the turbine disk alternating with the plurality of raised blade attachment surfaces defining the outer periphery. The selected radial position is outboard of the live rim. Each pair of adjacent turbine blades defines a shank cavity therebetween. The shank cavity extends radially outwardly from the live rim and includes a live rim notch disposed below the bond plane and above the live rim.

Abstract translation: 提供混合式涡轮转子及其制造方法。 混合结合的涡轮机转子包括涡轮盘和多个涡轮机叶片，每个涡轮机叶片各自冶金地结合到涡轮盘的多个凸起的叶片附接表面的对应的凸起的叶片附接表面，以限定位于选定径向位置处的接合平面。 涡轮盘具有边缘部分，其包括周向连续材料的活边缘和在涡轮盘的外周中的多个带状轮缘切口，与限定外周的多个凸起刀片附接表面交替。 所选的径向位置是活动边缘的外侧。 每对相邻的涡轮叶片在它们之间限定一个柄腔。 柄腔从活边缘径向向外延伸，并且包括设置在接合平面下方和活边缘上方的活边缘凹口。

公开(公告)号：US20140161623A1

公开(公告)日：2014-06-12

申请号：US13681675

申请日：2012-11-20

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： George E. Zurmehly ,  Milton Ortiz ,  Kin Poon ,  Michael Vinup ,  Ardeshir Riahi

IPC: F01D5/12

CPC classification number: F01D5/12 ,  F01D5/147 ,  F01D5/284 ,  F05D2300/6033 ,  Y02T50/672 ,  Y02T50/673 ,  Y10T29/49316

Abstract: A vane assembly includes first and second annular metal rings configured to accept a compressed gas flow therebetween. The first and second annular rings each include a cutout portion. The assembly further includes a ceramic matrix composite vane configured as an airfoil having a blunt rounded nose and a flattened and tapered tail. A first radial end of the vane is rigidly disposed on the first annular ring and a second radial end of the vane is slidably disposed within the cutout portion of the second annular ring such that the vane is encompassed by the first and second annular rings. The vane includes a hollow through opening portion extending radially therethrough. Still further, the assembly includes a metallic elongated member disposed within and extending through the hollow portion of vane and through the cutout portion of the first annular ring.

Abstract translation: 叶片组件包括构造成接受其间的压缩气体流动的第一和第二环形金属环。 第一和第二环形圈各自包括切口部分。 该组件还包括一个陶瓷基体复合叶片，其被构造成具有钝的圆形鼻部和扁平和渐缩的尾部的翼型件。 叶片的第一径向端刚性地设置在第一环形环上，并且叶片的第二径向端部可滑动地设置在第二环形环的切口部分内，使得叶片被第一和第二环形圈包围。 叶片包括径向延伸穿过的中空的通孔部分。 此外，组件包括设置在叶片的中空部分内并穿过叶片的中空部分并穿过第一环形圈的切口部分的金属细长构件。