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1. 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

2. 发明公开

EP3183172A1 ACTUATED OUTLET DOOR FOR AIRCRAFT HIGH-TEMPERATURE EXHAUST 有权
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。

3. 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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