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公开(公告)号：US20250067514A1
公开(公告)日：2025-02-27
申请号：US18236614
申请日：2023-08-22
Applicant: Hamilton Sundstrand Corporation
Inventor： David Saltzman , Grum T. Ngatu , Stephen Patrick Adamakis , Patrick McCord , Zachary Valente
IPC: F28D1/053
Abstract: A fluid circuit of a heat exchanger includes a core and a first header. The core is configured to receive a fluid and includes a plurality of conduits. Each of the plurality of conduits extends along a longitudinal axis from a first end portion to a second end portion. The first header is integrally formed with and fluidly connecting the plurality of conduits. Outer walls of the plurality of conduits taper outward relative to the longitudinal axes to join the first header.
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公开(公告)号：US12084188B2
公开(公告)日：2024-09-10
申请号：US17538203
申请日：2021-11-30
Applicant: Hamilton Sundstrand Corporation
Inventor： Patrick McCord , Donald E. Army , Liana Frangioni
CPC classification number: B64D13/06 , B64D2013/0662
Abstract: A water extractor for use in an environmental control system, the water extractor comprising a housing having an inlet end and an outlet end, a swirling mechanism mounted within the housing, and a fog harvester assembly mounted within the housing at a location between the inlet end and the outlet end.
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公开(公告)号：US20160195004A1
公开(公告)日：2016-07-07
申请号：US14590558
申请日：2015-01-06
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor： Donald E. Army, Jr. , Patrick McCord
CPC classification number: F02B29/0462 , B05B1/02 , B05B15/40 , B05B15/62 , B64D13/08 , F24F2006/146 , H05K7/20345 , H05K7/20881
Abstract: A water injector for an aviation cooling system includes a body having a first end, a second end, and an intermediate portion extending therebetween. A conduit extends through the body from the first end to the second end. A spray nozzle is fluidically connected to the conduit and arranged at one of the first end and the second end. A mounting plate is arranged at the other of the first end and the second end. The mounting plate is configured and disposed to secure the body to an aviation cooling component. A filter is supported at the body and is fluidically exposed to the conduit. The filter is configured and disposed to capture particulate flowing into the water injector towards the spray nozzle.
Abstract translation: 用于航空冷却系统的喷水器包括具有第一端，第二端和在其间延伸的中间部的主体。 导管从第一端延伸穿过主体到第二端。 喷嘴流体地连接到管道并且布置在第一端和第二端中的一个处。 在第一端和第二端的另一端设置安装板。 安装板被构造和布置成将主体固定到航空冷却部件上。 过滤器在主体处被支撑并且流体地暴露于导管。 过滤器被配置和设置成捕获流向喷水器的颗粒流向喷嘴。
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公开(公告)号：US20220411073A1
公开(公告)日：2022-12-29
申请号：US17362195
申请日：2021-06-29
Applicant: Hamilton Sundstrand Corporation
Inventor： Donald E. Army , Patrick McCord
Abstract: A water extractor for an environmental control system of an aircraft includes a separation mechanism configured to divide an airflow into a first airflow and a second airflow. The separation mechanism includes an inlet conduit, a body in fluid communication with the inlet conduit, and at least one coalescing feature arranged within an interior of the body. A water extraction vessel is arranged in fluid communication with the separation mechanism. The water extraction vessel includes a first portion for receiving the first airflow and a second portion for receiving the second airflow. The first portion is configured to collect and remove water from the first airflow.
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公开(公告)号：US10077951B2
公开(公告)日：2018-09-18
申请号：US14947447
申请日：2015-11-20
Applicant: Hamilton Sundstrand Corporation
Inventor： Luke J. Mayo , Patrick McCord , Donald E. Army
CPC classification number: F28F9/0075 , B64D13/00 , B64D2013/0688 , F28D9/00 , F28D9/0043 , F28D2021/0021 , F28F9/001 , F28F2009/029 , F28F2280/00
Abstract: A mount configured for use with a recirculation heat exchanger of an aircraft environmental control is provided including a rectangular base having a length of about 14 inches (35.56 cm) and a width of about 6 inches (15.24 cm). A support extends vertically from the base. A top surface of the support is arranged at a 10° angle below a horizontal plane.
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Patent Agency Ranking
公开(公告)号：US20180258837A1
公开(公告)日：2018-09-13
申请号：US15975445
申请日：2018-05-09
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor： Donald E. Army, JR. , Patrick McCord
CPC classification number: F02B29/0462 , B05B1/02 , B05B15/40 , B05B15/62 , B64D13/08 , B64D2013/0614 , B64D2013/0674 , F24F2006/146 , H05K7/20345 , H05K7/20881 , Y02T10/146
Abstract: A water injector for an aviation cooling system includes a body having a first end, a second end, and an intermediate portion extending therebetween. A conduit extends through the body from the first end to the second end. A spray nozzle is fluidically connected to the conduit and arranged at one of the first end and the second end. A mounting plate is arranged at the other of the first end and the second end. The mounting plate is configured and disposed to secure the body to an aviation cooling component. A filter is supported at the body and is fluidically exposed to the conduit. The filter is configured and disposed to capture particulate flowing into the water injector towards the spray nozzle.
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公开(公告)号：US11156233B2
公开(公告)日：2021-10-26
申请号：US16157147
申请日：2018-10-11
Applicant: Hamilton Sundstrand Corporation
Inventor： Donald E. Army , Patrick McCord , Dominique P. Sautron , Thomas M. Zywiak
IPC: F04F5/14 , F04F5/18 , F04F7/00 , B64D13/06 , B60K11/06 , F16K11/052 , F16K11/044 , F04F5/46
Abstract: An Environmental Control System (ECS) for an aircraft includes a ram air system having a ram inlet and a ram outlet. The ECS includes a cabin air compressor motor, a diverter valve, and a dedicated outlet. The cabin air compressor motor has a motor inlet passage and a motor outlet passage with the motor inlet passage being coupled to the ram inlet. The diverter valve includes a first diverter inlet, a first diverter outlet, and a second diverter outlet. The first diverter inlet is coupled to the motor outlet passage. The dedicated outlet is connected to the first diverter outlet in a flight mode of operation of the aircraft and the ram outlet is connected to the second diverter outlet in a ground mode of operation of the aircraft.
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公开(公告)号：US10697355B2
公开(公告)日：2020-06-30
申请号：US15975445
申请日：2018-05-09
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor： Donald E. Army, Jr. , Patrick McCord
IPC: B05B1/32 , F02B29/04 , H05K7/20 , B05B1/02 , B64D13/08 , F24F6/14 , B05B15/40 , B05B15/62 , B64D13/06
Abstract: A water injector for an aviation cooling system includes a body having a first end, a second end, and an intermediate portion extending therebetween. A conduit extends through the body from the first end to the second end. A spray nozzle is fluidically connected to the conduit and arranged at one of the first end and the second end. A mounting plate is arranged at the other of the first end and the second end. The mounting plate is configured and disposed to secure the body to an aviation cooling component. A filter is supported at the body and is fluidically exposed to the conduit. The filter is configured and disposed to capture particulate flowing into the water injector towards the spray nozzle.
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公开(公告)号：US20200041212A1
公开(公告)日：2020-02-06
申请号：US16054253
申请日：2018-08-03
Applicant: Hamilton Sundstrand Corporation
Inventor： Nigel Palmer , Ahmet Becene , Patrick McCord , James Streeter , Feng Feng , Luke Martin , Gabriel Ruiz , Joseph Turney
Abstract: A counter-flow heat exchanger including: a primary flow passageway comprising a primary flow inlet, a primary flow outlet, and a plurality of primary flow subset passageways therebetween; a secondary flow passageway comprising a secondary flow inlet, a secondary flow outlet, and a plurality of secondary flow subset passageways therebetween; and a heat exchanger core comprising portions of the plurality of primary flow subset passageways and the plurality of secondary flow subset passageways, the secondary flow passageway being in thermal communication with the primary flow passageway in the heat exchanger core, wherein the primary flow subset passageways in the heat exchanger core and the secondary flow subset passageways in the heat exchanger core are oriented such that primary fluid flow through the primary flow subset passageways flows opposite secondary fluid flow through the secondary flow subset passageways.
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公开(公告)号：US10184494B2
公开(公告)日：2019-01-22
申请号：US13930549
申请日：2013-06-28
Applicant: Hamilton Sundstrand Corporation
Inventor： Donald E. Army , Patrick McCord , Dominique P. Sautron , Thomas M. Zywiak
Abstract: An Environmental Control System (ECS) for an aircraft includes a ram air system having a ram inlet and a ram outlet. The ECS includes a cabin air compressor motor, a diverter valve, and a dedicated outlet. The cabin air compressor motor has a motor inlet passage and a motor outlet passage with the motor inlet passage being coupled to the ram inlet. The diverter valve includes a first diverter inlet, a first diverter outlet, and a second diverter outlet. The first diverter inlet is coupled to the motor outlet passage. The dedicated outlet is connected to the first diverter outlet in a flight mode of operation of the aircraft and the ram outlet is connected to the second diverter outlet in a ground mode of operation of the aircraft.
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