SEALING CONFIGURATION TO REDUCE AIR LEAKAGE
    1.
    发明申请

    公开(公告)号:US20200025005A1

    公开(公告)日:2020-01-23

    申请号:US16037470

    申请日:2018-07-17

    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.

    Heat exchanger supply plenum
    2.
    发明授权

    公开(公告)号:US11519368B2

    公开(公告)日:2022-12-06

    申请号:US16736342

    申请日:2020-01-07

    Abstract: A cooling system for a gas turbine engine may comprise a plenum extending circumferentially around an outer engine case structure. The plenum may comprise a supply conduit and a return conduit. The supply conduit and the return conduit may be in fluid communication with a heat exchanger. The heat exchanger may be disposed between the outer engine case structure and an inner engine case structure. The plenum may be configured to provide enhance heat transfer for the cooling system.

    Airflow deflector and assembly
    3.
    发明授权

    公开(公告)号:US10738637B2

    公开(公告)日:2020-08-11

    申请号:US15852483

    申请日:2017-12-22

    Abstract: An airflow deflector is provided that includes at least one liner attachment flange, a deflector panel, and at least one deflector leg. The at least one liner attachment flange has a liner side surface and an opposing outer surface. The at least one deflector leg extends between and is attached to the at least one liner attachment flange. The at least one deflector leg extends a distance between the deflector panel and the liner attachment flange to maintain the deflector panel a separation distance from the liner attachment flange. The airflow deflector is configured for insertion of the at least one deflector leg and the deflector panel within a liner aperture.

    Sealing configuration to reduce air leakage

    公开(公告)号:US10830077B2

    公开(公告)日:2020-11-10

    申请号:US16037379

    申请日:2018-07-17

    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.

    SEALING CONFIGURATION TO REDUCE AIR LEAKAGE
    5.
    发明申请

    公开(公告)号:US20200025004A1

    公开(公告)日:2020-01-23

    申请号:US16037379

    申请日:2018-07-17

    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.

    HEAT EXCHANGER SUPPLY PLENUM
    6.
    发明申请

    公开(公告)号:US20210207564A1

    公开(公告)日:2021-07-08

    申请号:US16736342

    申请日:2020-01-07

    Abstract: A cooling system for a gas turbine engine may comprise a plenum extending circumferentially around an outer engine case structure. The plenum may comprise a supply conduit and a return conduit. The supply conduit and the return conduit may be in fluid communication with a heat exchanger. The heat exchanger may be disposed between the outer engine case structure and an inner engine case structure. The plenum may be configured to provide enhance heat transfer for the cooling system.

    Sealing configuration to reduce air leakage

    公开(公告)号:US10781710B2

    公开(公告)日:2020-09-22

    申请号:US16037470

    申请日:2018-07-17

    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.

Patent Agency Ranking