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1. 发明申请

WO2019075555A1 AIRCRAFT PYLON FAIRING 审中-公开
公开(公告)号：WO2019075555A1
公开(公告)日：2019-04-25
申请号：PCT/CA2018/051293
申请日：2018-10-15
申请人： BOMBARDIER INC.
发明人： SADRI, Reza , DUSSAULT, Kathleen , BOILEAU, Edmond
IPC分类号： B64D29/02 , B64C7/00 , B64D27/12
CPC分类号： B64D27/18 , B64D29/02
摘要： An assembly comprises a wing and a pylon fairing extending from the wing at a pylon location. The pylon fairing has an aerodynamic profile defining a fairing trailing edge. The pylon fairing has an upper section extending from the wing and a lower section including a shelf. The aerodynamic profile of the upper section is cambered toward the root of the wing. The aerodynamic profile of at least part of the lower section is symmetrical. The fairing trailing edge in the upper section extends axially rearward of a trailing edge of the wing at the pylon location. In addition or alternately, a distance between the fairing trailing edge in the upper section and a trailing edge of the wing at the pylon location has a value corresponding to at most 30% of a local chord of the wing at the pylon location.

2. 发明申请

WO2016027187A1 ACTUATED OUTLET DOOR FOR AIRCRAFT HIGH-TEMPERATURE EXHAUST 审中-公开
标题翻译：用于飞机高温排气的启动门
公开(公告)号：WO2016027187A1
公开(公告)日：2016-02-25
申请号：PCT/IB2015/055735
申请日：2015-07-29
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： IAROCCI, Nick , SADRI, Reza , POIRIER, Vincent , DUSSAULT, Kathleen , BOILEAU, Edmond
IPC分类号： B64D33/04 , B64D33/08
CPC分类号： B64D33/04 , B64D15/04 , B64D33/08
摘要： An outlet door is provided for covering an outlet defining an outlet area in a skin (24) of an aircraft component to exhaust a flow of heated air to an outside of the aircraft. The outlet door includes a body defining a door area and extending between a leading edge and a trailing edge and a linkage (38) connecting the body to the aircraft, permitting the body to transition between at least one of an open position and a closed position. In the closed position, the body at least partially occupies the outlet area. In the open position, the body forms an angle with the skin of the aircraft. The leading edge of the body and the skin of the aircraft define a separation (202) therebetween when the body is in the open position. The separation defines and air flow for mixing cold air with the flow of heated air.
摘要翻译：出口门被设置用于覆盖限定飞行器部件的皮肤（24）中的出口区域的出口，以将热空气流排出到飞行器的外部。出口门包括限定门区域并在前缘和后缘之间延伸的主体以及将主体连接到飞行器的连接件（38），允许主体在打开位置和关闭位置中的至少一个之间转换。在关闭位置，身体至少部分地占据出口区域。在打开位置，身体与飞机的皮肤形成一个角度。当身体处于打开位置时，身体的前缘和飞行器的皮肤在其间限定了间隔（202）。分离限定和用于将冷空气与加热空气流混合的空气流。

3. 发明公开

EP3697691A1 AIRCRAFT PYLON FAIRING 审中-公开
公开(公告)号：EP3697691A1
公开(公告)日：2020-08-26
申请号：EP18867996.3
申请日：2018-10-15
申请人： Bombardier Inc.
发明人： SADRI, Reza , DUSSAULT, Kathleen , BOILEAU, Edmond
IPC分类号： B64D29/02 , B64C7/00 , B64D27/12

4. 发明公开

EP3183172A1 ACTUATED OUTLET DOOR FOR AIRCRAFT HIGH-TEMPERATURE EXHAUST 审中-公开
标题翻译：用于飞机高温排气的致动出口门
公开(公告)号：EP3183172A1
公开(公告)日：2017-06-28
申请号：EP15749890.8
申请日：2015-07-29
申请人： Bombardier Inc. , Short Brothers Plc
发明人： IAROCCI, Nick , SADRI, Reza , POIRIER, Vincent , DUSSAULT, Kathleen , BOILEAU, Edmond
IPC分类号： B64D33/04 , B64D33/08
CPC分类号： B64D33/04 , B64D15/04 , B64D33/08
摘要： An outlet door is provided for covering an outlet defining an outlet area in a skin (24) of an aircraft component to exhaust a flow of heated air to an outside of the aircraft. The outlet door includes a body defining a door area and extending between a leading edge and a trailing edge and a linkage (38) connecting the body to the aircraft, permitting the body to transition between at least one of an open position and a closed position. In the closed position, the body at least partially occupies the outlet area. In the open position, the body forms an angle with the skin of the aircraft. The leading edge of the body and the skin of the aircraft define a separation (202) therebetween when the body is in the open position. The separation defines and air flow for mixing cold air with the flow of heated air.
摘要翻译：提供出口门以覆盖限定飞机部件的外壳（24）中的出口区域的出口，以将经加热的空气流排出到飞机外部。出口门包括限定门区域并在前缘和后缘之间延伸的主体以及将主体连接到飞机的连杆（38），从而允许主体在打开位置和关闭位置中的至少一个之间转换。在关闭位置，主体至少部分地占据出口区域。在打开的位置，身体与飞机的皮肤形成一个角度。当主体处于打开位置时，主体的前缘和飞机的表皮在它们之间限定了分隔202。分离限定了用于将冷空气与热空气流混合的空气流动。

5. 发明授权

EP3183172B1 ACTUATED OUTLET DOOR FOR AIRCRAFT HIGH-TEMPERATURE EXHAUST 有权
公开(公告)号：EP3183172B1
公开(公告)日：2018-10-31
申请号：EP15749890.8
申请日：2015-07-29
申请人： Bombardier Inc. , Short Brothers Plc
发明人： IAROCCI, Nick , SADRI, Reza , POIRIER, Vincent , DUSSAULT, Kathleen , BOILEAU, Edmond
IPC分类号： B64D33/04 , B64D33/08
CPC分类号： B64D33/04 , B64D15/04 , B64D33/08
摘要： An outlet door is provided for covering an outlet defining an outlet area in a skin (24) of an aircraft component to exhaust a flow of heated air to an outside of the aircraft. The outlet door includes a body defining a door area and extending between a leading edge and a trailing edge and a linkage (38) connecting the body to the aircraft, permitting the body to transition between at least one of an open position and a closed position. In the closed position, the body at least partially occupies the outlet area. In the open position, the body forms an angle with the skin of the aircraft. The leading edge of the body and the skin of the aircraft define a separation (202) therebetween when the body is in the open position. The separation defines and air flow for mixing cold air with the flow of heated air.

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