-
公开(公告)号：US20160258323A1
公开(公告)日：2016-09-08
申请号：US15031585
申请日：2014-05-23
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Gary L. Grogg , Garth J. Vdoviak, JR. , Berci Cherpician
CPC classification number: F01D25/162 , F01D25/164 , F05D2230/70 , F05D2260/37 , F16C19/06 , F16C19/26 , F16C27/045 , F16C35/045 , F16C35/062 , F16C35/067 , F16C35/077 , F16C43/04 , F16C2226/12 , F16C2226/50 , F16C2360/23
Abstract: A bearing housing may include a main body integrated with a bearing receiving portion. A bearing retention stop may extend from the main body and include a plurality of access cutouts for facilitating the removal of a bearing from the bearing housing without causing damage to the bearing.
Abstract translation: 轴承壳体可以包括与轴承接收部分一体化的主体。 轴承保持止动件可以从主体延伸并且包括多个通路切口，用于便于从轴承壳体移除轴承而不会损坏轴承。
-
公开(公告)号：US20140260321A1
公开(公告)日：2014-09-18
申请号：US14208255
申请日：2014-03-13
Applicant: United Technologies Corporation
Inventor： James L. McClellan, IV , Gary L. Grogg , Garth J. Vdoviak, JR.
IPC: F02C7/20
CPC classification number: F01D25/162 , F01D25/30 , F02C7/06 , F05D2250/29 , F05D2260/30
Abstract: A gas turbine engine static structure has a joint that includes at least two flanges. The first flange includes a face extending axially proud between radially spaced apart undercuts. The second flange abuts the face. Fasteners secure the flanges to one another through the face.
Abstract translation: 燃气涡轮发动机静态结构具有包括至少两个凸缘的接头。 第一凸缘包括在径向间隔开的底切部之间轴向凸起的面。 第二个法兰靠在脸上。 紧固件通过面部将法兰固定在一起。
-
公开(公告)号：US20190017414A1
公开(公告)日：2019-01-17
申请号：US16127524
申请日：2018-09-11
Applicant: United Technologies Corporation
Inventor： Garth J. Vdoviak, JR. , Gary L. Grogg
IPC: F01D25/18 , F02C7/06 , F02C7/28 , F01D25/12 , F16J15/16 , F04D29/12 , F16C33/66 , F04D29/059 , F04D29/063 , F04D29/32
Abstract: A component for a gas turbine engine includes a compartment housing that redirects oil from at least one passage in a rotational component onto a backside of a seal land.
-
公开(公告)号：US20160032771A1
公开(公告)日：2016-02-04
申请号：US14771867
申请日：2014-03-07
Applicant: United Technologies Corporation
Inventor： Garth J. Vdoviak, JR. , Gary L. Grogg
CPC classification number: F01D25/183 , F01D25/12 , F02C7/06 , F02C7/28 , F04D29/059 , F04D29/063 , F04D29/124 , F04D29/321 , F05D2220/32 , F05D2240/50 , F05D2240/55 , F05D2260/20 , F16C19/26 , F16C33/6677 , F16C2360/23 , F16J15/162
Abstract: A component for a gas turbine engine includes a compartment housing that redirects oil from at least one passage in a rotational component onto a backside of a seal land.
Abstract translation: 用于燃气涡轮发动机的部件包括隔室壳体，其将来自旋转部件中的至少一个通道的油重定向到密封件的背面。
-
-
-
Search Results
4
records
(took 0.037 seconds)
