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1. 发明授权

EP3366586B1 A THRUST PRODUCING UNIT WITH AT LEAST TWO ROTOR ASSEMBLIES AND A SHROUDING 有权
公开(公告)号：EP3366586B1
公开(公告)日：2020-08-19
申请号：EP17400008.3
申请日：2017-02-27
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Kiesewetter, Uwe , Bebesel, Marius , Mores, Sebastian , Pfaller, Rupert
IPC分类号： B64C39/02 , B64C11/00 , B64C11/48 , B64C27/20

2. 发明公开

EP3354559A1 A THRUST PRODUCING UNIT WITH AT LEAST TWO ROTOR ASSEMBLIES AND A SHROUDING 有权
公开(公告)号：EP3354559A1
公开(公告)日：2018-08-01
申请号：EP17400003.4
申请日：2017-01-26
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Mores, Sebastian , Kiesewetter, Uwe , Bebesel, Marius
IPC分类号： B64C11/00 , B64C29/00 , B64C27/20
CPC分类号： B64C11/46 , B64C11/001 , B64C27/08 , B64C27/20 , B64C29/0033
摘要： The invention is related to a thrust producing unit 3d for producing thrust in a predetermined direction 23, comprising a shrouding 6d and at least two rotor assemblies 7d, 8d, wherein the shrouding 6d defines an internal volume 20c, and wherein a first rotor assembly 7d of the at least two rotor assemblies 7d, 8d defines a first rotor axis and a second rotor assembly 8d of the at least two rotor assemblies 8d defines a second rotor axis, the first and second rotor axes 12d being one of: (i) coaxially arranged, and (ii) inclined by associated inclination angles 21a, 22a with respect to the predetermined direction 23, the associated inclination angles 21a, 22a being comprised in a range between -60° and +60°, and preferably amounting to 0°, and wherein the first rotor assembly 7d is arranged outside of the internal volume 20c of the shrouding 6d.

3. 发明授权

EP2878536B1 Advanced pitch stabilizer 有权
标题翻译：高级音调稳定器
公开(公告)号：EP2878536B1
公开(公告)日：2017-05-24
申请号：EP13400035.5
申请日：2013-11-29
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Mores, Sebastian , D'Alascio, Alessandro , Kiesewetter, Uwe , Probst, Stefan , Wehle, Christian , Bebesel, Marius
IPC分类号： B64C27/82
CPC分类号： B64C5/10 , B64C9/06 , B64C27/82 , B64C2027/8254 , B64C2027/8272 , B64C2027/8281

4. 发明公开

EP3050794A1 AIRCRAFT WITH INWARDLY FOLDABLE REAR DOOR 有权
标题翻译：里面折返门平面
公开(公告)号：EP3050794A1
公开(公告)日：2016-08-03
申请号：EP15400004.6
申请日：2015-01-28
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Probst, Stefan , Hünecke, Wolfgang , Löser, Frank , Frese, Johannes , Mores, Sebastian , Matt, Michael
IPC分类号： B64C1/14
CPC分类号： B64C1/1415 , B64C1/24 , B64D11/00
摘要： An aircraft comprising a rear opening (4) and a rear door (11) to close such rear opening (4), wherein the rear door is attached to the fuselage (3) of the aircraft by means of an arrangement having two links (26, 27) due to which the rear door (11) can be displaced longitudinally and in elevation up to a position at the interior of the fuselage (3).

5. 发明授权

EP3333072B1 AN AIRCRAFT WITH AN AIRFRAME THAT COMPRISES A LOAD CARRYING FRAMEWORK 有权
公开(公告)号：EP3333072B1
公开(公告)日：2020-02-05
申请号：EP16400059.8
申请日：2016-12-07
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Mores, Sebastian , Blacha, Martin , Reichensperger, Christian , Rittel, Klaus , Schneeberger, Marco , Geiss, Michael , Paschek, Markus , Bebesel, Marius
IPC分类号： B64C27/04 , B64C27/08 , B64D27/24 , B64C1/06 , B64C1/16

6. 发明授权

EP3354559B1 A THRUST PRODUCING UNIT WITH AT LEAST TWO ROTOR ASSEMBLIES AND A SHROUDING 有权
公开(公告)号：EP3354559B1
公开(公告)日：2019-04-03
申请号：EP17400003.4
申请日：2017-01-26
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Mores, Sebastian , Kiesewetter, Uwe , Bebesel, Marius
IPC分类号： B64C11/00 , B64C29/00 , B64C27/20

7. 发明公开

EP3354566A1 A THRUST PRODUCING UNIT WITH AT LEAST TWO ROTOR ASSEMBLIES AND A SHROUDING 有权
公开(公告)号：EP3354566A1
公开(公告)日：2018-08-01
申请号：EP17400002.6
申请日：2017-01-26
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Mores, Sebastian , D'Alascio, Alessandro , Kneisch, Thomas , Kicker, Klaus , Link, Stefanie , Kiesewetter, Uwe , Bebesel, Marius
IPC分类号： B64C27/20 , B64C11/00 , B64C11/48 , B64D25/00
CPC分类号： B64C11/001 , B64C11/48 , B64C27/08 , B64C27/20 , B64C2201/027 , B64C2201/162 , B64D25/00
摘要： The invention is related to a thrust producing unit 3d for producing thrust in a predetermined direction 23, comprising at least two rotor assemblies 7d, 8d and a shrouding 6d, each one of the at least two rotor assemblies 7d, 8d defining an associated rotor plane 21, 22, wherein a first rotor assembly 7d of the at least two rotor assemblies 7d, 8d is provided for operating in a failure-free operating mode of the thrust producing unit 3d and a second rotor assembly 8d of the at least two rotor assemblies 7d, 8d is provided for operating at least in case of a failure of the first rotor assembly 7d, and wherein the shrouding 6d accommodates at most one of the at least two rotor assemblies 7d, 8d.

8. 发明公开

EP3184425A1 MULTIROTOR AIRCRAFT 有权
标题翻译：多旋翼飞机
公开(公告)号：EP3184425A1
公开(公告)日：2017-06-28
申请号：EP15400058.2
申请日：2015-12-21
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Mores, Sebastian , Geyer, Christoph , Haisch, Stefan , Bebesel, Marius
IPC分类号： B64C27/20 , B64C27/10
CPC分类号： B64C27/20 , B64C27/10
摘要： The invention is related to a multirotor aircraft (1) with at least two thrust producing units (3a, 3b, 3c, 3d), the multirotor aircraft (1) being adapted for transportation of passengers and comprising an aircraft operating structure (7a, 7b, 7c, 7d) that is adapted for operation of the multirotor aircraft (1) in failure-free operating mode, and a redundant security architecture (8a, 8b, 8c, 8d) that is at least adapted for operation of the multirotor aircraft (1) in case of a failure of the aircraft operating structure (7a, 7b, 7c, 7d) in operation, the redundant security architecture (8a, 8b, 8c, 8d) being provided to comply with applicable authority regulations and certification requirements regarding passenger transportation.
摘要翻译：本发明涉及一种具有至少两个推力产生单元（3a，3b，3c，3d）的多旋翼飞机（1），所述多旋翼飞行器（1）适于乘客的运输并且包括飞机操作结构（7a，7b ，适于在无故障运行模式下操作多旋翼飞行器（1）的多旋翼飞行器（7c，7d，7c，7d）以及至少适用于多旋翼飞行器（1）的操作的冗余安全架构（8a，8b，8c， 1）在运行中的飞机操作结构（7a，7b，7c，7d）发生故障的情况下，提供冗余安全结构（8a，8b，8c，8d）以符合适用的权限规定和关于乘客的认证要求运输。

9. 发明公开

EP2878536A1 Advanced pitch stabilizer 有权
标题翻译：扩展斜坡稳定
公开(公告)号：EP2878536A1
公开(公告)日：2015-06-03
申请号：EP13400035.5
申请日：2013-11-29
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Mores, Sebastian , D'Alascio, Alessandro , Kiesewetter, Uwe , Probst, Stefan , Wehle, Christian , Bebesel, Marius
IPC分类号： B64C27/82
CPC分类号： B64C5/10 , B64C9/06 , B64C27/82 , B64C2027/8254 , B64C2027/8272 , B64C2027/8281
摘要： A pitch stabilizer (10) with box configuration suitable for providing stability to a rotorcraft comprising a vertical mid-plane (15) and a fuselage (14); the pitch stabilizer (10) comprising one or two pitch stabilizing assemblies, with no more than one pitch stabilizing assembly on each side of the vertical mid-plane (15), wherein each pitch stabilizing assembly comprises upper pitch stabilizing means (11), lower pitch stabilizing means (12) and a wing tip element (13).

10. 发明授权

EP3333064B1 AN AIRCRAFT WITH AN AIRFRAME AND AT LEAST ONE ELECTRICALLY POWERED THRUST PRODUCING UNIT 有权
公开(公告)号：EP3333064B1
公开(公告)日：2020-04-22
申请号：EP16400060.6
申请日：2016-12-07
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Mores, Sebastian , Blacha, Martin , Reichensperger, Christian , Rittel, Klaus , Schneeberger, Marco , Geiss, Michael , Paschek, Markus , Bebesel, Marius
IPC分类号： B64C1/06 , B64C27/04 , B64D27/24

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