HEAT MANAGEMENT SYSTEM FOR AIRCRAFT
    1.
    发明公开

    公开(公告)号:US20240110512A1

    公开(公告)日:2024-04-04

    申请号:US18463641

    申请日:2023-09-08

    Inventor: Mark P. Reid

    CPC classification number: F02C7/14 B64D27/10 F02C7/06 F02C7/224

    Abstract: A heat management system includes a fuel tank storing a fuel; a first heat exchanger thermally coupled to the fuel tank; a hydraulic pump for circulating a hydraulic fluid; a hydraulic circuit including first and second hydraulic lines fluidly coupled to the first heat exchanger and the hydraulic pump, such that the first heat exchanger brings the hydraulic fluid and the fuel into a heat exchange relationship; an oil circuit; and a second heat exchanger thermally coupled to the oil circuit and at least one of the first and second hydraulic lines, such that the second heat exchanger brings the hydraulic fluid and the oil into a heat exchange relationship, thereby allowing heat transfer between the fuel and the oil via the hydraulic fluid.

    OIL TANK SYSTEM
    2.
    发明申请
    OIL TANK SYSTEM 审中-公开

    公开(公告)号:US20190338670A1

    公开(公告)日:2019-11-07

    申请号:US16389107

    申请日:2019-04-19

    Inventor: Mark P. Reid

    Abstract: An oil tank system (100) for a gas turbine engine is provided. The oil tank system (100) includes an oil tank (102) having an upper tank portion (112) and a lower tank portion (114), a waisted section (118) being provided between the upper tank portion (112) and the lower tank portion (114). Oil is received by a de-aerator (104) of the system (100) which supplies de-aerated oil to the upper tank portion (112). The waisted section (118) includes an upper face (119) configured to catch oil drips from above the waisted section (118) and to guide oil to a lower face (121) of the waisted section (118).

    Oil tank system
    3.
    发明授权

    公开(公告)号:US11492927B2

    公开(公告)日:2022-11-08

    申请号:US16389107

    申请日:2019-04-19

    Inventor: Mark P. Reid

    Abstract: An oil tank system (100) for a gas turbine engine is provided. The oil tank system (100) includes an oil tank (102) having an upper tank portion (112) and a lower tank portion (114), a waisted section (118) being provided between the upper tank portion (112) and the lower tank portion (114). Oil is received by a de-aerator (104) of the system (100) which supplies de-aerated oil to the upper tank portion (112). The waisted section (118) includes an upper face (119) configured to catch oil drips from above the waisted section (118) and to guide oil to a lower face (121) of the waisted section (118).

    Heat management system for aircraft

    公开(公告)号:US12129797B2

    公开(公告)日:2024-10-29

    申请号:US18463641

    申请日:2023-09-08

    Inventor: Mark P. Reid

    CPC classification number: F02C7/14 B64D27/10 F02C7/06 F02C7/224

    Abstract: A heat management system includes a fuel tank storing a fuel; a first heat exchanger thermally coupled to the fuel tank; a hydraulic pump for circulating a hydraulic fluid; a hydraulic circuit including first and second hydraulic lines fluidly coupled to the first heat exchanger and the hydraulic pump, such that the first heat exchanger brings the hydraulic fluid and the fuel into a heat exchange relationship; an oil circuit; and a second heat exchanger thermally coupled to the oil circuit and at least one of the first and second hydraulic lines, such that the second heat exchanger brings the hydraulic fluid and the oil into a heat exchange relationship, thereby allowing heat transfer between the fuel and the oil via the hydraulic fluid.

    Oil tank
    5.
    发明授权
    Oil tank 有权

    公开(公告)号:US11174787B2

    公开(公告)日:2021-11-16

    申请号:US16389190

    申请日:2019-04-19

    Inventor: Mark P. Reid

    Abstract: An oil tank (100) for a gas turbine engine is provided. The oil tank (100) comprises an oil inlet (102), an oil outlet (104), and a body including a coiled portion (106) interposed between the oil inlet (102) and the oil outlet (104). Oil is received by the coiled portion (106). The coiled portion (106) acts to at least partially de-aerate oil received from the oil inlet (104).

    Oil Tank
    6.
    发明申请
    Oil Tank 审中-公开

    公开(公告)号:US20190338705A1

    公开(公告)日:2019-11-07

    申请号:US16389190

    申请日:2019-04-19

    Inventor: Mark P. Reid

    Abstract: An oil tank (100) for a gas turbine engine is provided. The oil tank (100) comprises an oil inlet (102), an oil outlet (104), and a body including a coiled portion (106) interposed between the oil inlet (102) and the oil outlet (104). Oil is received by the coiled portion (106). The coiled portion (106) acts to at least partially de-aerate oil received from the oil inlet (104).

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