中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

135 records (took 0.032 seconds)

    Baffle with impingement holes
    1.
    发明授权
    Baffle with impingement holes 有权

    公开(公告)号：US11415002B2

    公开(公告)日：2022-08-16

    申请号：US16657135

    申请日：2019-10-18

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Adam P. Generale ,  Lucas Dvorozniak ,  San Quach

    IPC: F01D5/18 ,  F01D25/12

    Abstract: An airfoil includes an vane airfoil, which has a ceramic matrix composite airfoil section including an outer wall that defines an internal cavity. The vane airfoil has an associated temperature profile which defines at least one high temperature area and at least one low temperature area. The vane airfoil includes a first zone which is defined in a first radial extent and corresponds to the high temperature area of the temperature profile and a second zone defined in a second radial extent and corresponds to the low temperature area of the temperature profile. An insert is situated in the internal cavity. The insert includes a first zone defined in a first radial extent that is aligned with the first zone of the vane airfoil. The first zone includes a first plurality of cooling holes which are configured to provide a first cooling density. A second zone is defined in a second radial extent that is aligned with the second zone of the vane airfoil. The second zone includes a second plurality of cooling holes that provide a second cooling density that is lower than the first cooling density such that the high temperature area and the low temperature area are balanced to lower a thermal gradient across the first and second zones of the vane airfoil. An vane airfoil and a method of assembling a ceramic matrix composite vane airfoil are also disclosed.

    Internal cooling cavity with trip strips
    3.
    发明授权
    Internal cooling cavity with trip strips 有权

    公开(公告)号：US10947854B2

    公开(公告)日：2021-03-16

    申请号：US16793575

    申请日：2020-02-18

    Applicant: United Technologies Corporation

    Inventor： San Quach ,  Atul Kohli ,  Matthew A. Devore ,  Steven Bruce Gautschi

    IPC: F01D5/18

    Abstract: An airfoil is provided. The airfoil may comprise a cross over, an impingement chamber in fluid communication with the cross over, and a first trip strip disposed on a first surface of the impingement chamber. A cooling system is also provided. The cooling system may comprise an impingement chamber, a first trip strip on a first surface of the impingement chamber, and a second trip strip on a second surface of the impingement chamber. An internally cooled engine part is further provided. The internally cooled part may comprise a cross over and an impingement chamber in fluid communication with the cross over. The cross over may be configured to direct air towards a first surface of the impingement chamber. A first trip strip may be disposed on the first surface of the impingement chamber.

    Woven skin cores for turbine airfoils
    4.
    发明授权
    Woven skin cores for turbine airfoils 有权

    公开(公告)号：US10731477B2

    公开(公告)日：2020-08-04

    申请号：US15700990

    申请日：2017-09-11

    Applicant: United Technologies Corporation

    Inventor： San Quach ,  Jeffrey T. Morton

    IPC: F01D5/18

    Abstract: An airfoil includes an airfoil body having a pressure side and a suction side that each radially extend between a first radial boundary end and a second radial boundary end and each axially extend between a leading edge and a trailing edge. The airfoil body defines a plurality of first skin core passages disposed proximate the suction side and radially extend from the first radial boundary end towards the second radial boundary end, and a plurality of second skin core passages that radially extend toward the second radial boundary end and circumferentially extend towards the suction side proximate the second radial boundary end.

    INTERNAL COOLING CAVITY WITH TRIP STRIPS
    5.
    发明申请
    INTERNAL COOLING CAVITY WITH TRIP STRIPS 审中-公开

    公开(公告)号：US20200182070A1

    公开(公告)日：2020-06-11

    申请号：US16793575

    申请日：2020-02-18

    Applicant: United Technologies Corporation

    Inventor： San Quach ,  Atul Kohli ,  Matthew A. Devore ,  Steven Bruce Gautschi

    IPC: F01D5/18

    Abstract: An airfoil is provided. The airfoil may comprise a cross over, an impingement chamber in fluid communication with the cross over, and a first trip strip disposed on a first surface of the impingement chamber. A cooling system is also provided. The cooling system may comprise an impingement chamber, a first trip strip on a first surface of the impingement chamber, and a second trip strip on a second surface of the impingement chamber. An internally cooled engine part is further provided. The internally cooled part may comprise a cross over and an impingement chamber in fluid communication with the cross over. The cross over may be configured to direct air towards a first surface of the impingement chamber. A first trip strip may be disposed on the first surface of the impingement chamber.

    Float wall combustor panels having airflow distribution features
    6.
    发明授权
    Float wall combustor panels having airflow distribution features 有权

    公开(公告)号：US10563584B2

    公开(公告)日：2020-02-18

    申请号：US15795301

    申请日：2017-10-27

    Applicant: United Technologies Corporation

    Inventor： Jason Shenny ,  John J. Rup, Jr. ,  Robert M. Sonntag ,  James B. Hoke ,  San Quach ,  Richard G. Ullrich

    IPC: F23R3/00 ,  F02C7/18 ,  F23R3/04

    Abstract: Combustor panels including panel bodies with first and second sides, a pin array extending from the first side, wherein each pin extends a first height, has a pin diameter, and is separated from adjacent pins by a pin array separation distance. A structural protrusion extends from the first side. No pins of the pin array are located within a flashing distance that is equal to a protrusion separation distance plus half of the pin diameter, wherein a location of the pin is measured from a center point of the pin to a closest point on the exterior surface of the structural protrusion. At least one pin array extension is integrally formed with the structural protrusion, the pin array extension extending along the first side to a position that replaces a pin of the pin array that would be within the flashing distance.

    Airfoil cooling circuits
    8.
    发明授权
    Airfoil cooling circuits 有权

    公开(公告)号：US10400609B2

    公开(公告)日：2019-09-03

    申请号：US15866134

    申请日：2018-01-09

    Applicant: United Technologies Corporation

    Inventor： Eric A. Hudson ,  Tracy A. Propheter-Hinckley ,  San Quach ,  Matthew A. Devore

    IPC: B22C9/10 ,  B22C9/24 ,  F01D5/18

    Abstract: An airfoil includes leading and trailing edges; first and second sides extending from the leading edge to the trailing edge, each side having an exterior surface; a core passage located between the first and second sides and the leading and trailing edges; and a wall structure located between the core passage and the exterior surface of the first side. The wall structure includes a plurality of cooling fluid inlets communicating with the core passage for receiving cooling fluid from the core passage, a plurality of cooling fluid outlets on the exterior surface of the first side for expelling cooling fluid and forming a cooling film along the exterior surface of the first side, and a plurality of cooling passages communicating with the plurality of cooling fluid inlets and the plurality of cooling fluid outlets. At least a portion of one cooling passage extends between adjacent cooling fluid outlets.

Patent Agency Ranking