中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

14 records (took 0.022 seconds)

    GAS TURBINE ENGINE SYSTEMS WITH FAIRING
    1.
    发明申请
    GAS TURBINE ENGINE SYSTEMS WITH FAIRING 审中-公开
    燃气涡轮发动机系统

    公开(公告)号：WO2009151701A3

    公开(公告)日：2010-11-18

    申请号：PCT/US2009037531

    申请日：2009-03-18

    Applicant: UNITED TECHNOLOGIES CORP ,  LYDERS DAVID ,  KLINETOB CARL BRIAN ,  ALEXANDER PHILLIP

    Inventor： LYDERS DAVID ,  KLINETOB CARL BRIAN ,  ALEXANDER PHILLIP

    IPC: F01D25/28 ,  F02C7/20

    CPC classification number: F01D25/28 ,  F01D9/041 ,  F02C7/20 ,  F05D2240/12 ,  F05D2240/121 ,  F05D2240/303 ,  F05D2260/36

    Abstract: Gas turbine engine systems involving fairings with locating data are provided. In this regard, a representative a fairing assembly for a gas turbine engine includes: a first locating component having a leading edge, first and second sides extending from the leading edge, and a recess oriented parallel to the leading edge, the recess having a first datum surface, the first locating component being operative to be positioned between a portion of a strut and a portion of an interior surface of a fairing sheath such that the first datum surface establishes a desired orientation of the fairing sheath relative to the strut.

    Abstract translation: 提供了涉及具有定位数据的整流罩的燃气涡轮发动机系统。 在这方面，用于燃气涡轮发动机的代表性整流罩组件包括：第一定位部件，其具有前缘，从前缘延伸的第一和第二侧以及平行于前缘定向的凹部，所述凹部具有第一 基准表面，第一定位部件可操作地定位在支柱的一部分和整流罩的内表面的一部分之间，使得第一基准表面相对于支柱建立整流罩的期望取向。

    2.
    发明专利
    未知

    公开(公告)号：BRPI0603516A

    公开(公告)日：2007-08-14

    申请号：BRPI0603516

    申请日：2006-08-23

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： CARROLL CHRISTIAN A ,  ELEY JAMES ALLEN ,  KLINETOB CARL BRIAN

    IPC: F02C7/00

    Abstract: An inlet guide vane (30) provides improved, smooth airflow and avoids separation of flow even at high incidence angles. The inlet guide vane (30) includes a strut (32) having opposite side surfaces (46,48) that are continuously curved to provide a controlled velocity distribution at the trailing edge (44) of the strut (32). The inlet guide vane (30) further includes a flap (34) having a leading edge (52) aligned behind the trailing edge (44) of the strut (32). Generally, the strut (32) and the flap (34) are designed together so that low momentum air in the gap (59) between the strut (32) and the flap (34) will be energized and entrained in the boundary layer of the flap (34). The airflow from the gap (59) will remain attached to the flap (34) to improve the flow from the flap (34).

    Variable Geometry Inlet Guide Vane
    3.
    发明专利
    Variable Geometry Inlet Guide Vane 未知

    公开(公告)号：AU2006230736A1

    公开(公告)日：2007-05-10

    申请号：AU2006230736

    申请日：2006-10-20

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： ELEY JAMES ALLEN ,  CARROLL CHRISTIAN A ,  KLINETOB CARL BRIAN

    IPC: F02C7/042 ,  B64D33/02 ,  F02C7/04

    Abstract: An inlet guide vane (30) provides improved, smooth airflow and avoids separation of flow even at high incidence angles. The inlet guide vane (30) includes a strut (32) having opposite side surfaces (46,48) that are continuously curved to provide a controlled velocity distribution at the trailing edge (44) of the strut (32). The inlet guide vane (30) further includes a flap (34) having a leading edge (52) aligned behind the trailing edge (44) of the strut (32). Generally, the strut (32) and the flap (34) are designed together so that low momentum air in the gap (59) between the strut (32) and the flap (34) will be energized and entrained in the boundary layer of the flap (34). The airflow from the gap (59) will remain attached to the flap (34) to improve the flow from the flap (34).

    VARIABLE GEOMETRY INLET GUIDE VANE
    4.
    发明专利
    VARIABLE GEOMETRY INLET GUIDE VANE 未知

    公开(公告)号：SG131832A1

    公开(公告)日：2007-05-28

    申请号：SG2006057905

    申请日：2006-08-23

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： CARROLL CHRISTIAN A ,  ELEY JAMES ALLEN ,  KLINETOB CARL BRIAN

    Abstract: An inlet guide vane (30) provides improved, smooth airflow and avoids separation of flow even at high incidence angles. The inlet guide vane (30) includes a strut (32) having opposite side surfaces (46,48) that are continuously curved to provide a controlled velocity distribution at the trailing edge (44) of the strut (32). The inlet guide vane (30) further includes a flap (34) having a leading edge (52) aligned behind the trailing edge (44) of the strut (32). Generally, the strut (32) and the flap (34) are designed together so that low momentum air in the gap (59) between the strut (32) and the flap (34) will be energized and entrained in the boundary layer of the flap (34). The airflow from the gap (59) will remain attached to the flap (34) to improve the flow from the flap (34).

    VARIABLE GEOMETRY INLET GUIDE VANE
    5.
    发明专利
    VARIABLE GEOMETRY INLET GUIDE VANE 未知

    公开(公告)号：CA2555074A1

    公开(公告)日：2007-04-25

    申请号：CA2555074

    申请日：2006-08-02

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： ELEY JAMES ALLEN ,  KLINETOB CARL BRIAN ,  CARROLL CHRISTIAN A

    IPC: F01D9/02

    Abstract: An inlet guide vane provides improved, smooth airflow and avoids separation of flow even at high incidence angles. The inlet guide vane includes a strut having opposite side surfaces that are continuously curved to provide a controlled velocity distribution at the trailing edge of the strut. The inle t guide vane further includes a flap having a leading edge aligned behind the trailing ed ge of the strut. Generally, the strut and the flap are designed together so that low momentum air in the gap between the strut and the flap will be energized and entraine d in the boundary layer of the flap. The airflow from the gap will remain attached to the flap to improve the flow from the flap.

    SELECTIVE COATING REMOVAL OR MASKING FOR GROUND PATH
    10.
    发明公开
    SELECTIVE COATING REMOVAL OR MASKING FOR GROUND PATH 审中-公开
    选择性涂层去除或支持地板路径

    公开(公告)号：EP2971610A4

    公开(公告)日：2016-05-04

    申请号：EP14768728

    申请日：2014-03-14

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： HYATT THOMAS B ,  KLINETOB CARL BRIAN

    IPC: F01D25/00 ,  B64D45/02 ,  H01R4/00

    CPC classification number: F01D9/042 ,  B64D45/02 ,  F01D5/288 ,  F01D25/005 ,  F01D25/243 ,  F05D2220/327 ,  F05D2260/31 ,  F05D2300/17 ,  F05D2300/173 ,  F05D2300/174 ,  F05D2300/50

    Abstract: A device for providing a grounding path between an outer surface of a gas turbine aircraft engine and an inner surface of a gas turbine aircraft engine uses a structural guide vane (SGV) with a nonconductive coating on the surface. Bolts are put in bolt holes that have a bolt receiving cavity without the nonconductive coating. A washer and bolt are used so that attachment of the SGV to a surface provides a ground path from the SGV through the bolt, washer and nut for electrical engagement with a surface to which the bolt attaches the SGV.

    Abstract translation: 用于在燃气涡轮机飞行器发动机的外表面和燃气涡轮机飞机发动机的内表面之间提供接地路径的装置使用在表面上具有非导电涂层的结构导叶（SGV）。 螺栓被放入螺栓孔中，螺栓孔具有不带非导电涂层的螺栓接收腔。 使用垫圈和螺栓，使得SGV附接到表面提供了从SGV通过螺栓，垫圈和螺母的接地路径，用于与螺栓连接到SGV的表面电接合。

Patent Agency Ranking