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    RADIO FREQUENCY SYSTEM SENSOR INTERFACE
    1.
    发明申请
    RADIO FREQUENCY SYSTEM SENSOR INTERFACE 有权

    公开(公告)号：US20210160593A1

    公开(公告)日：2021-05-27

    申请号：US16692128

    申请日：2019-11-22

    Applicant: United Technologies Corporation

    Inventor： Jonathan Gilson ,  Joseph V. Mantese ,  Goran Djuknic ,  Gurkan Gok ,  Brenda J. Lisitano ,  Coy Bruce Wood ,  Sanjay Bajekal

    IPC: H04Q9/00

    Abstract: A system of a machine includes a network of nodes distributed throughout the machine. Each of the nodes is operable to communicate through electromagnetic signals. The system also includes a radio frequency transceiver, a first antenna coupled to the radio frequency transceiver, a second antenna coupled to one or more sensor nodes, and a controller coupled to the radio frequency transceiver. The controller is configured to select at least one sensor node to interrogate, transmit one or more interrogation frequencies from the radio frequency transceiver through the first antenna to the second antenna, receive one or more sensor frequencies at the first antenna broadcast from the second antenna based on a frequency response of the at least one sensor node to the one or more interrogation frequencies, and determine one or more sensed values based on the sensor frequencies received at the radio frequency transceiver through the first antenna.

    RADIO FREQUENCY-BASED REPEATER IN A WAVEGUIDE SYSTEM
    2.
    发明申请
    RADIO FREQUENCY-BASED REPEATER IN A WAVEGUIDE SYSTEM 有权

    公开(公告)号：US20210159969A1

    公开(公告)日：2021-05-27

    申请号：US16692119

    申请日：2019-11-22

    Applicant: United Technologies Corporation

    Inventor： Jonathan Gilson ,  Joseph V. Mantese ,  Goran Djuknic ,  Gurkan Gok ,  Brenda J. Lisitano ,  Sanjay Bajekal ,  Coy Bruce Wood

    IPC: H04B7/155 ,  F02C9/00

    Abstract: A system of a machine includes a network of a plurality of nodes distributed throughout the machine. Each of the nodes is operable to communicate through a plurality of electromagnetic signals. A controller is operable to communicate with the network of nodes through the electromagnetic signals. The system also includes a plurality of waveguides configured to guide transmission of the electromagnetic signals between the controller and one or more of the nodes. A radio frequency-based repeater is coupled to at least two of the waveguides in the network between the controller and at least one of the nodes. The radio frequency-based repeater is configured to receive a portion of the electromagnetic signals in a first waveguide and boost a transmission characteristic of the portion of the electromagnetic signals in a second waveguide.

    Radio frequency system sensor interface
    5.
    发明授权
    Radio frequency system sensor interface 有权

    公开(公告)号：US11277676B2

    公开(公告)日：2022-03-15

    申请号：US16692128

    申请日：2019-11-22

    Applicant: United Technologies Corporation

    Inventor： Jonathan Gilson ,  Joseph V. Mantese ,  Goran Djuknic ,  Gurkan Gok ,  Brenda J. Lisitano ,  Coy Bruce Wood ,  Sanjay Bajekal

    IPC: H04Q9/00

    Abstract: A system of a machine includes a network of nodes distributed throughout the machine. Each of the nodes is operable to communicate through electromagnetic signals. The system also includes a radio frequency transceiver, a first antenna coupled to the radio frequency transceiver, a second antenna coupled to one or more sensor nodes, and a controller coupled to the radio frequency transceiver. The controller is configured to select at least one sensor node to interrogate, transmit one or more interrogation frequencies from the radio frequency transceiver through the first antenna to the second antenna, receive one or more sensor frequencies at the first antenna broadcast from the second antenna based on a frequency response of the at least one sensor node to the one or more interrogation frequencies, and determine one or more sensed values based on the sensor frequencies received at the radio frequency transceiver through the first antenna.

    Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
    6.
    发明授权
    Low pressure ratio fan engine having a dimensional relationship between inlet and fan size 有权

    公开(公告)号：US11015550B2

    公开(公告)日：2021-05-25

    申请号：US15887183

    申请日：2018-02-02

    Applicant: United Technologies Corporation

    Inventor： Wesley K. Lord ,  Robert E. Malecki ,  Yuan J. Qiu ,  Becky E. Rose ,  Jonathan Gilson

    IPC: F02K3/068 ,  F01D25/24 ,  F02C7/04

    Abstract: According to an example embodiment, a gas turbine engine assembly includes, among other things, a fan section including a fan, the fan including a plurality of fan blades, a diameter of the fan having a dimension D that is based on a dimension of the fan blades, each fan blade having a leading edge, and a forward most portion on the leading edges of the fan blades in a first reference plane, a turbine section including a high pressure turbine and a low pressure turbine, the low pressure turbine driving the fan, a nacelle including an inlet portion forward of the fan, a forward edge on the inlet portion in a second reference plane, and a length of the inlet portion having a dimension L measured along an engine axis between the first reference plane and the second reference plane. A dimensional relationship of L/D is no more than 0.45.

    LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BETWEEN INLET AND FAN SIZE
    8.
    发明申请
    LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BETWEEN INLET AND FAN SIZE 审中-公开

    公开(公告)号：US20200025036A1

    公开(公告)日：2020-01-23

    申请号：US16391476

    申请日：2019-04-23

    Applicant: United Technologies Corporation

    Inventor： Wesley K. Lord ,  Robert E. Malecki ,  Yuan J. Qiu ,  Becky E. Rose ,  Jonathan Gilson

    IPC: F01D25/24 ,  F02K3/06 ,  F01D5/14 ,  F02C7/04 ,  F01D5/02 ,  F01D15/12 ,  F01D17/10

    Abstract: According to an example embodiment, a gas turbine engine assembly includes, among other things, a fan section including a fan, the fan including a plurality of fan blades, a diameter of the fan having a dimension D that is based on a dimension of the fan blades, each fan blade having a leading edge, and a forward most portion on the leading edges of the fan blades in a first reference plane, a geared architecture, a turbine section including a high pressure turbine and a low pressure turbine, the low pressure turbine driving the fan through the geared architecture, a nacelle surrounding the fan, the nacelle including an inlet portion forward of the fan, a forward edge on the inlet portion in a second reference plane, and a length of the inlet portion having a dimension L measured along an engine axis between the first reference plane and the second reference plane. A dimensional relationship of L/D is between 0.20 and 0.40.

    LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BETWEEN INLET AND FAN SIZE
    10.
    发明申请
    LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BETWEEN INLET AND FAN SIZE 审中-公开
    低压风扇发动机在入口和风扇尺寸之间存在尺寸关系

    公开(公告)号：US20160108854A1

    公开(公告)日：2016-04-21

    申请号：US14882760

    申请日：2015-10-14

    Applicant: United Technologies Corporation

    Inventor： Wesley K. Lord ,  Robert E. Malecki ,  Yuan J. Qiu ,  Becky E. Rose ,  Jonathan Gilson

    IPC: F02K3/06 ,  F04D19/02 ,  F01D15/12 ,  F01D17/10 ,  F01D5/02 ,  F01D5/12

    CPC classification number: F02K3/06 ,  F01D5/02 ,  F01D5/141 ,  F01D15/12 ,  F01D17/105 ,  F02C7/04 ,  F02C7/045 ,  F04D29/522 ,  F04D29/547 ,  F05D2220/32 ,  F05D2250/00 ,  Y02T50/671 ,  Y02T50/673

    Abstract: A gas turbine engine assembly according to an example of the present disclosure includes, among other things, a fan including a plurality of fan blades, a diameter of the fan having a dimension D that is based on a dimension of the fan blades, each fan blade having a leading edge, a geared architecture configured to drive the fan, a turbine section configured to drive the geared architecture, a compressor section including a first compressor and a second compressor, and an inlet portion forward of the fan. A length of the inlet portion has a dimension L between a location of the leading edge of at least some of the fan blades and a forward edge on the inlet portion. A dimensional relationship of L/D is between about 0.2 and about 0.45.

    Abstract translation: 根据本公开的示例的燃气涡轮发动机组件包括除了别的以外的包括多个风扇叶片的风扇，具有基于风扇叶片的尺寸的尺寸D的风扇的直径，每个风扇 具有前缘的叶片，配置成驱动风扇的齿轮架构，构造成驱动齿轮架构的涡轮部分，包括第一压缩机和第二压缩机的压缩机部分以及风扇前部的入口部分。 入口部分的长度在至少一些风扇叶片的前缘的位置与入口部分的前边缘之间具有尺寸L。 L / D的尺寸关系为约0.2至约0.45。

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