中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

6 records (took 0.019 seconds)

    Gas turbine engine quench pattern for gas turbine engine combustor
    2.
    发明授权
    Gas turbine engine quench pattern for gas turbine engine combustor 有权

    公开(公告)号：US10816206B2

    公开(公告)日：2020-10-27

    申请号：US15025808

    申请日：2014-10-20

    Applicant: United Technologies Corporation

    Inventor： Dennis M. Moura, III ,  Reza Rezvani

    IPC: F23R3/14 ,  F23R3/50 ,  F23R3/06 ,  F02C3/00 ,  F23R3/28

    Abstract: A combustor for a turbine engine includes an inner liner panel with a multiple of inner dilution passages. The multiple of dilution passages includes a repeating pattern of a first major inner air passage, a minor inner air passage, and a second major inner air passage. A combustor for a turbine engine includes an outer liner panel with a multiple of outer dilution passages. The multiple of outer dilution passages includes a repeating pattern of a first major outer air passage, a first minor outer air passage, a second major outer air passage, and a second minor outer air passage.

    Combustor panel cooling arrangements
    3.
    发明授权
    Combustor panel cooling arrangements 有权

    公开(公告)号：US10605169B2

    公开(公告)日：2020-03-31

    申请号：US15490189

    申请日：2017-04-18

    Applicant: United Technologies Corporation

    Inventor： Dennis M. Moura ,  James B. Hoke ,  Reza Rezvani

    IPC: F02C7/12 ,  F23R3/00 ,  F23R3/16 ,  F23R3/06

    Abstract: Combustor panels for use in gas turbine engine combustors having a panel body having a peripheral rail around a periphery of the panel body, a first boss formed on the panel body and surrounding a first aperture that passes through the panel body, and a first webbing that extends from the peripheral rail toward the first boss. A first annular channel is formed between the first webbing and the first boss and surrounds the first boss and a first web pocket is formed within the first webbing between the peripheral rail and the first boss and defines a local extension of the first annular channel extending from the first boss to the peripheral rail.

    COMBUSTOR PANEL COOLING ARRANGEMENTS
    4.
    发明申请
    COMBUSTOR PANEL COOLING ARRANGEMENTS 审中-公开

    公开(公告)号：US20180298819A1

    公开(公告)日：2018-10-18

    申请号：US15490189

    申请日：2017-04-18

    Applicant: United Technologies Corporation

    Inventor： Dennis M. Moura ,  James B. Hoke ,  Reza Rezvani

    IPC: F02C7/12 ,  F23R3/00

    Abstract: Combustor panels for use in gas turbine engine combustors having a panel body having a peripheral rail around a periphery of the panel body, a first boss formed on the panel body and surrounding a first aperture that passes through the panel body, and a first webbing that extends from the peripheral rail toward the first boss. A first annular channel is formed between the first webbing and the first boss and surrounds the first boss and a first web pocket is formed within the first webbing between the peripheral rail and the first boss and defines a local extension of the first annular channel extending from the first boss to the peripheral rail.

    GAS TURBINE ENGINE QUENCH PATTERN FOR GAS TURBINE ENGINE COMBUSTOR
    5.
    发明申请
    GAS TURBINE ENGINE QUENCH PATTERN FOR GAS TURBINE ENGINE COMBUSTOR 审中-公开
    用于气体涡轮发动机燃油的燃气涡轮发动机

    公开(公告)号：US20160245521A1

    公开(公告)日：2016-08-25

    申请号：US15025808

    申请日：2014-10-20

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Dennis M. Moura, III ,  Reza Rezvani

    IPC: F23R3/14 ,  F23R3/28 ,  F02C3/00

    CPC classification number: F23R3/14 ,  F02C3/00 ,  F23R3/06 ,  F23R3/283 ,  F23R3/50 ,  Y02T50/675

    Abstract: A combustor for a turbine engine includes an inner liner panel with a multiple of inner dilution passages. The multiple of dilution passages includes a repeating pattern of a first major inner air passage, a minor inner air passage, and a second major inner air passage. A combustor for a turbine engine includes an outer liner panel with a multiple of outer dilution passages. The multiple of outer dilution passages includes a repeating pattern of a first major outer air passage, a first minor outer air passage, a second major outer air passage, and a second minor outer air passage.

    Abstract translation: 用于涡轮发动机的燃烧器包括具有多个内部稀释通道的内衬板。 多个稀释通道包括第一主要内部空气通道，次要内部空气通道和第二主要内部空气通道的重复图案。 用于涡轮发动机的燃烧器包括具有多个外部稀释通道的外衬板。 多个外部稀释通道包括第一主要外部空气通道，第一次要外部空气通道，第二主要外部空气通道和第二小型外部空气通道的重复图案。

Patent Agency Ranking