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公开(公告)号：US10781710B2
公开(公告)日：2020-09-22
申请号：US16037470
申请日：2018-07-17
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Rebecca R. Dunnigan , Billie W. Bunting , Ted Guevel , Randall Lee Greenberg
Abstract: A seal assembly for a fluid transfer tube in a gas turbine engine is disclosed. In various embodiments, the seal assembly includes a base member having a first side configured to mate with a casing and a second side opposite the first side, a housing configured to mate with the second side of the base member and to surround a portion of the fluid transfer tube, a bellows surrounding the fluid transfer tube and positioned between the housing and the casing, and a wear ring disposed between the housing and the bellows.
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公开(公告)号：US20140312611A1
公开(公告)日：2014-10-23
申请号：US14200649
申请日：2014-03-07
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Billie W. Bunting , Robert J. DeRosa , Craig Michael Callaghan , Mark W. Colebrook , Ranganath Santosh
IPC: F16L15/08
CPC classification number: F16L15/006 , F02C7/222 , F16L15/00 , Y10T29/49895
Abstract: A fluid conduit for a gas turbine engine includes a first fluid conduit attachable to a second fluid conduit and securable together with a lockable connector. The connector includes a first portion including external threads and a second portion receiving the first portion and including internal threads mating to the external threads of the first portion. The internal threads include lead threads defining a first thread interface with the external threads for starting attachment of the first portion to the second portion and locking threads defining a second thread interface for locking the first portion to the second portion.
Abstract translation: 用于燃气涡轮发动机的流体导管包括可连接到第二流体导管并与可锁定连接器一起固定的第一流体导管。 连接器包括包括外螺纹的第一部分和接收第一部分并包括与第一部分的外螺纹配合的内螺纹的第二部分。 内螺纹包括限定与外螺纹的第一螺纹接口的引导螺纹，用于开始将第一部分附接到第二部分，并且锁定螺纹限定用于将第一部分锁定到第二部分的第二螺纹接口。
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Patent Agency Ranking
公开(公告)号：US20200025038A1
公开(公告)日：2020-01-23
申请号：US16037270
申请日：2018-07-17
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Rebecca R Dunnigan , Billie W. Bunting , Ted Guevel , Randall Lee Greenberg
Abstract: A seal assembly for a fluid transfer tube in a gas turbine engine is disclosed. In various embodiments, the seal assembly includes a boot seal configured to surround a length of the fluid transfer tube, the boot seal having a first end and a second end and a seal ring disposed at the first end, an attachment ring configured to mate with the seal ring and to secure the seal ring against a casing, an annular ring configured to mate with an interior surface of the boot seal at the second end and to surround a portion of the fluid transfer tube, and a clamp ring configured to surround the second end of the boot seal proximate the annular ring.
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公开(公告)号：US20200025005A1
公开(公告)日：2020-01-23
申请号：US16037470
申请日：2018-07-17
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Rebecca R. Dunnigan , Billie W. Bunting , Ted Guevel , Randall Lee Greenberg
Abstract: A seal assembly for a fluid transfer tube in a gas turbine engine is disclosed. In various embodiments, the seal assembly includes a base member having a first side configured to mate with a casing and a second side opposite the first side, a housing configured to mate with the second side of the base member and to surround a portion of the fluid transfer tube, a bellows surrounding the fluid transfer tube and positioned between the housing and the casing, and a wear ring disposed between the housing and the bellows.
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公开(公告)号：US10830077B2
公开(公告)日：2020-11-10
申请号：US16037379
申请日：2018-07-17
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Rebecca R. Dunnigan , Billie W. Bunting , Ted Guevel , Randall Lee Greenberg
Abstract: A seal assembly for a fluid transfer tube in a gas turbine engine is disclosed. In various embodiments, the seal assembly includes a base member having a first side configured to mate with a casing and a second side opposite the first side, an annular ring configured to mate with the second side of the base member and to surround a portion of the fluid transfer tube, a first O-ring disposed between the annular ring and the fluid transfer tube, a second O-ring disposed between the base member and the annular ring, and an attachment ring configured to secure the annular ring and the base member to the casing.
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公开(公告)号：US20200025004A1
公开(公告)日：2020-01-23
申请号：US16037379
申请日：2018-07-17
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Rebecca R. Dunnigan , Billie W. Bunting , Ted Guevel , Randall Lee Greenberg
Abstract: A seal assembly for a fluid transfer tube in a gas turbine engine is disclosed. In various embodiments, the seal assembly includes a base member having a first side configured to mate with a casing and a second side opposite the first side, an annular ring configured to mate with the second side of the base member and to surround a portion of the fluid transfer tube, a first O-ring disposed between the annular ring and the fluid transfer tube, a second O-ring disposed between the base member and the annular ring, and an attachment ring configured to secure the annular ring and the base member to the casing.
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公开(公告)号：US10119635B2
公开(公告)日：2018-11-06
申请号：US14200649
申请日：2014-03-07
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Billie W. Bunting , Robert J. DeRosa , Craig Michael Callaghan , Mark W. Colebrook , Ranganath Santosh
Abstract: A fluid conduit for a gas turbine engine includes a first fluid conduit attachable to a second fluid conduit and securable together with a lockable connector. The connector includes a first portion including external threads and a second portion receiving the first portion and including internal threads mating to the external threads of the first portion. The internal threads include lead threads defining a first thread interface with the external threads for starting attachment of the first portion to the second portion and locking threads defining a second thread interface for locking the first portion to the second portion.
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