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公开(公告)号：US11708166B2
公开(公告)日：2023-07-25
申请号：US17196803
申请日：2021-03-09
申请人： ROHR, INC.
发明人： Daniel J. Shetzer
摘要： An aircraft anti-icing system is disclosed. A tube having a plurality of outlet ports is disposed within an interior of an outer housing in spaced relation to a closed end of this outer housing. The exterior of the outer housing includes a leading edge at its closed end. The tube is anchored relative to the outer housing by one or more brackets that extend from the tube to the outer housing. An open end of the outer housing may be closed by an aft wall that encloses the tube within an interior compartment of the outer housing.
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2.发明申请公开(公告)号：US20160047274A1
公开(公告)日：2016-02-18
申请号：US14462106
申请日：2014-08-18
申请人： Rohr, Inc.
IPC分类号： F01D25/24
CPC分类号： F01D25/24 , F01D25/14 , F02C6/08 , F02C7/18 , F02C9/18 , F02K1/06 , F02K1/10 , F02K1/1207 , F02K1/30 , F02K1/32 , F02K1/34 , F02K1/70 , F02K1/72 , F02K1/76 , F02K1/763 , F02K1/766 , F02K1/805 , Y02T50/675
摘要： An assembly is provided for a turbofan engine. This turbofan engine assembly includes a cowling, a door and an actuation mechanism configured to actuate movement of the door in response to receiving a control signal. The cowling is configured to form a compartment at least partially around a case of the turbofan engine. The cowling includes an exhaust port that is fluidly coupled with the compartment. The door is configured to at least partially open and close the exhaust port. This variable exhaust port may be opened in case increased airflow is needed through the compartment, such as when increased cooling airflow is needed through an environmental air precooler that cools compressed air for the aircraft cabin and the precooler exhausts its cooling air into the compartment.
摘要翻译： 为涡扇发动机提供组件。 该涡轮风扇发动机组件包括整流罩，门和致动机构，其构造成响应于接收控制信号致动门的运动。 整流罩配置成至少部分地围绕涡轮风扇发动机的壳体形成隔间。 整流罩包括与隔室流体耦合的排气口。 门构造成至少部分地打开和关闭排气口。 例如当需要通过冷却用于飞行器机舱的压缩空气的预冷器的环境空气预冷器来增加冷却气流时，可以打开该可变排气口以防止需要增加气流，并且预冷器将其冷却空气排出到隔间内。
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公开(公告)号：US20210309374A1
公开(公告)日：2021-10-07
申请号：US17196803
申请日：2021-03-09
申请人： ROHR, INC.
发明人： Daniel J. Shetzer
摘要： An aircraft anti-icing system is disclosed. A tube having a plurality of outlet ports is disposed within an interior of an outer housing in spaced relation to a closed end of this outer housing. The exterior of the outer housing includes a leading edge at its closed end. The tube is anchored relative to the outer housing by one or more brackets that extend from the tube to the outer housing. An open end of the outer housing may be closed by an aft wall that encloses the tube within an interior compartment of the outer housing.
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公开(公告)号：US10906661B2
公开(公告)日：2021-02-02
申请号：US16180747
申请日：2018-11-05
申请人： Rohr, Inc.
发明人： Daniel J. Shetzer
摘要： A nacelle for a gas turbine engine includes at least one hinge axis extending along the nacelle. At least one cowl is mounted to the nacelle, along the at least one hinge axis, by a plurality of hinges. The plurality of hinges includes at least one latch. The at least one latch includes a clevis and a tang. The clevis and the tang of the at least one latch are configured to receive a hinge pin, through a pin aperture, when the at least one cowl is in a closed condition.
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