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公开(公告)号：EP3162702B1
公开(公告)日：2019-05-15
申请号：EP16192580.5
申请日：2016-10-06
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2.发明公开REDUCED COMPLEXITY RING MOTOR DESIGN FOR PROPELLER DRIVEN VEHICLES 审中-公开RINGMOTORKONSTRUKTION麻省理工学院研究所KOMPLEXITÄTFÜRPROPELLERGETRIEBENE FAHRZEUGE
公开(公告)号：EP3162702A2
公开(公告)日：2017-05-03
申请号：EP16192580.5
申请日：2016-10-06
CPC分类号： H02K5/26 , B63G2008/002 , B63H1/16 , B63H3/06 , B64C11/001 , B64C11/04 , B64C11/12 , B64C11/44 , B64C39/02 , H02K1/06
摘要： A motor (200) includes a stator (210) and a rotor (250) coupled via the center hub (270) of the rotor. The stator includes a support ring, the support ring (220) comprising a plurality of windings (230) arranged circumferentially. The rotor is configured to operate as a rotating propeller and includes a center hub, a rotor support ring, and a plurality of blades (260). The rotor support ring comprises a plurality of magnetic poles arranged circumferentially. Each particular blade is individually coupled to the rotor support ring.
摘要翻译： 电动机（200）包括通过转子的中心毂（270）联接的定子（210）和转子（250）。 定子包括支撑环，支撑环（220）包括周向布置的多个绕组（230）。 转子被构造成作为旋转螺旋桨操作并且包括中心毂，转子支撑环和多个叶片（260）。 转子支撑环包括沿圆周布置的多个磁极。 每个特定的叶片分别联接到转子支撑环。
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公开(公告)号：EP2440454A4
公开(公告)日：2013-10-30
申请号：EP09845904
申请日：2009-06-10
申请人： SAAB AB
发明人： CARDELL PER-ERIK , STENBOM KJELL
CPC分类号： B64C27/43 , B64C2201/024 , Y10S416/50
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公开(公告)号：EP2440454B1
公开(公告)日：2014-11-12
申请号：EP09845904.3
申请日：2009-06-10
申请人： Saab AB
发明人： CARDELL, Per-Erik , STENBOM, Kjell
CPC分类号： B64C27/43 , B64C2201/024 , Y10S416/50
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5.发明公开VARIABLE PITCH COUNTERWEIGHTED PROPELLER SYSTEM WITH RELEASABLE HYDRAULIC PITCHLOCK 审中-公开变桨距平衡式松脱的水力坡降固定术
公开(公告)号：EP1023219A4
公开(公告)日：2002-11-13
申请号：EP98953841
申请日：1998-10-21
发明人： CARVALHO PAUL A , PRUDEN ROBERT W
IPC分类号： B64C11/38 , B63H1/06 , B63H3/08 , B63H5/125 , B64C11/06 , B64C11/12 , B64C11/28 , B64C27/50 , B64C27/64 , F01D7/00 , F03B3/14 , F04D29/36
CPC分类号： B64C11/385
摘要： The hydraulic propeller system of the present invention has a central hub (14) including a stationary portion (28), and a rotatable portion (30). A plurality of propeller blades (12) are connected with the rotatable portion (30), wherein each of the plurality of propeller blades (12) has an adjustable pitch, and a counterweight (26) biasing the blades (12) in a first pitch direction . An actuating mechanism (16) is used for adjusting the pitch of each of the plurality of blades (12). A valve (56) for locking the propeller blades (12) at a last commanded pitch is further provided. At least the valve (56), the actuating mechanism (16) are located on, and rotatable with, the rotatable portion (30).
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公开(公告)号：EP2437979A4
公开(公告)日：2015-04-22
申请号：EP09845603
申请日：2009-06-02
申请人： SAAB AB
CPC分类号： B64C27/82 , B64C27/51 , B64C2027/003 , Y10S416/50
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公开(公告)号：EP2437979A1
公开(公告)日：2012-04-11
申请号：EP09845603.1
申请日：2009-06-02
申请人： Saab AB
CPC分类号： B64C27/82 , B64C27/51 , B64C2027/003 , Y10S416/50
摘要： The invention relates to a rotor damper for a tail rotor (1) of a helicopter (4), comprising a main body (30) of a resilient material to be arranged between a drive shaft (6) for the tail rotor (1) and a hub (12) on which rotor blades (14) for the tail rotor (1) is coupled. A flange (38) is connected to the main body (30) of the rotor damper (2), which flange (38) is provided with an abutment surface (39) for abutting an outer surface (50) of the hub (12). The invention also relates to a tail rotor (1) provided with such a rotor damper (2).
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8.发明公开VARIABLE PITCH COUNTERWEIGHTED PROPELLER SYSTEM WITH RELEASABLE HYDRAULIC PITCHLOCK 审中-公开变桨距平衡式松脱的水力坡降固定术
公开(公告)号：EP1023219A1
公开(公告)日：2000-08-02
申请号：EP98953841.8
申请日：1998-10-21
IPC分类号： B63H1/06 , B63H3/08 , B63H5/125 , B64C11/06 , B64C11/12 , B64C11/28 , B64C11/38 , B64C27/50 , B64C27/64 , F01D7/00 , F03B3/14 , F04D29/36
CPC分类号： B64C11/385
摘要： The hydraulic propeller system of the present invention has a central hub (14) including a stationary portion (28), and a rotatable portion (30). A plurality of propeller blades (12) are connected with the rotatable portion (30), wherein each of the plurality of propeller blades (12) has an adjustable pitch, and a counterweight (26) biasing the blades (12) in a first pitch direction . An actuating mechanism (16) is used for adjusting the pitch of each of the plurality of blades (12). A valve (56) for locking the propeller blades (12) at a last commanded pitch is further provided. At least the valve (56), the actuating mechanism (16) are located on, and rotatable with, the rotatable portion (30).
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公开(公告)号：EP3162702A3
公开(公告)日：2017-07-12
申请号：EP16192580.5
申请日：2016-10-06
CPC分类号： H02K5/26 , B63G2008/002 , B63H1/16 , B63H3/06 , B64C11/001 , B64C11/04 , B64C11/12 , B64C11/44 , B64C39/02 , H02K1/06
摘要： A motor (200) includes a stator (210) and a rotor (250) coupled via the center hub (270) of the rotor. The stator includes a support ring, the support ring (220) comprising a plurality of windings (230) arranged circumferentially. The rotor is configured to operate as a rotating propeller and includes a center hub, a rotor support ring, and a plurality of blades (260). The rotor support ring comprises a plurality of magnetic poles arranged circumferentially. Each particular blade is individually coupled to the rotor support ring.
摘要翻译： 电机（200）包括经由转子的中心毂（270）联接的定子（210）和转子（250）。 定子包括支撑环，支撑环（220）包括周向布置的多个绕组（230）。 转子构造成作为旋转推进器运行并且包括中心毂，转子支撑环和多个叶片（260）。 转子支撑环包括沿圆周布置的多个磁极。 每个特定的叶片单独连接到转子支撑环。
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公开(公告)号：EP2437979B1
公开(公告)日：2016-10-26
申请号：EP09845603.1
申请日：2009-06-02
CPC分类号： B64C27/82 , B64C27/51 , B64C2027/003 , Y10S416/50
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