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1. 发明申请

WO2014177591A1 AIRCRAFT FOR VERTICAL TAKE-OFF AND LANDING WITH AN ENGINE AND A PROPELLER UNIT 审中-公开
标题翻译：用于垂直起落架和发动机和螺旋桨单元的飞机
公开(公告)号：WO2014177591A1
公开(公告)日：2014-11-06
申请号：PCT/EP2014/058767
申请日：2014-04-29
申请人： REITER, Johannes
发明人： REITER, Johannes
IPC分类号： B64C29/00 , B64C29/02
CPC分类号： B64C29/0033 , B64C29/02 , B64C39/024 , B64C2201/088 , B64C2201/108
摘要： The present invention relates to an aircraft (100) for vertical take-off and landing. A wing arrangement (110) is coupled to a fuselage (101) such that the wing arrangement (110) is tiltable around a longitudinal wing axis of the wing arrangement (110) and such that the wing arrangement (110) is rotatable around the fuselage (101). The wing arrangement (110) is adapted in such a way that, in a fixed-wing flight mode, the wing arrangement (110) does not rotate around the fuselage (101). The wing arrangement (110) is further adapted in such a way that, in a hover flight mode, the wing arrangement (110) is tilted around the longitudinal wing axis with respect to its orientations in the fixed-wing flight mode and that the wing arrangement (110) rotates around the fuselage (101). An engine (120) comprising a drive shaft (121) with an engine rotary axis (122), wherein the engine (120) is coupled to the wing arrangement (110) in such a way that in the hover flight mode the engine rotary axis (122) comprise at least one component which is parallel to a rotary axis (102) of the wing arrangement (110) around the fuselage (101).
摘要翻译：本发明涉及用于垂直起飞和着陆的飞行器（100）。机翼装置（110）联接到机身（101），使得机翼装置（110）围绕机翼装置（110）的纵向翼轴可倾斜，并且使得机翼装置（110）可围绕机身旋转（101）。机翼装置（110）适于使得在固定翼飞行模式中，机翼装置（110）不围绕机身（101）旋转。机翼装置（110）进一步适应于使得在悬停飞行模式中，机翼装置（110）相对于其在固定翼飞行模式中的定向围绕纵向翼轴线倾斜，并且机翼装置（110）绕机身（101）旋转。一种发动机（120），包括具有发动机旋转轴线（122）的驱动轴（121），其中所述发动机（120）以这种方式联接到所述机翼装置（110），使得在所述悬停飞行模式下，所述发动机旋转轴（122）包括平行于机身布置（110）围绕机身（101）的旋转轴线（102）的至少一个部件。

2. 发明申请

WO2014177589A1 AIRCRAFT FOR VERTICAL TAKE-OFF AND LANDING WITH HINGED AND BENDABLE WINGS 审中-公开
标题翻译：用于垂直起落架和带有铰链和可弯曲的机翼的飞机
公开(公告)号：WO2014177589A1
公开(公告)日：2014-11-06
申请号：PCT/EP2014/058765
申请日：2014-04-29
申请人： REITER, Johannes
发明人： REITER, Johannes
IPC分类号： B64C29/02
CPC分类号： B64C29/02 , B64C2201/088
摘要： The present invention describes an aircraft (100) for vertical take-off and landing. The aircraft (100) comprises a fuselage (101) comprising a fuselage nose (103) and a fuselage tail (104), a wing arrangement (110) comprising a longitudinal wing axis and a coupling device (120) which couples the wing arrangement (110) to the fuselage (101), such that the wing arrangement (110), in a fixed-wing flight mode, does not rotate around the fuselage (101), and such that the wing arrangement (110), in a hover flight mode, is tilted around the longitudinal wing axis with respect to its orientation in the fixed-wing flight mode and that the wing arrangement (110) rotates around the fuselage (101). The wing arrangement (110) is coupled to the coupling device (120) such that in the hover flight mode a wing tip of the wing arrangement (110) is movable in a direction to the fuselage nose (103) or to the fuselage tail (104).
摘要翻译：本发明描述了用于垂直起飞和着陆的飞行器（100）。飞机（100）包括机身（101），其包括机身前端（103）和机身尾部（104），机翼装置（110）包括纵向翼轴线和联接装置（120） 110），使得机翼装置（110）以固定翼飞行模式不围绕机身（101）旋转，并且使得在悬停飞行中的机翼装置（110）相对于其在固定翼飞行模式中的定向而围绕纵向翼轴线倾斜，并且机翼装置（110）围绕机身（101）旋转。机翼装置（110）联接到联接装置（120），使得在悬停飞行模式中，机翼装置（110）的翼尖可沿机身鼻部（103）或机身尾部（103）的方向移动 104）。

3. 发明申请

WO2014118299A1 AIRCRAFT AND METHOD FOR CONTROLLING AN AIRCRAFT FOR VERTICAL TAKE-OFF AND LANDING WITH A WIN ARRANGEMENT COMPRISING AN EXTENDIBLE LIFT INCREASING SYSTEM 审中-公开
标题翻译：用于控制垂直起落架的飞机的飞行器和方法，其中包括具有可扩展提升系统的绕组
公开(公告)号：WO2014118299A1
公开(公告)日：2014-08-07
申请号：PCT/EP2014/051847
申请日：2014-01-30
申请人： REITER, Johannes
发明人： REITER, Johannes
IPC分类号： B64C29/02 , B64C39/02
CPC分类号： B64C29/02 , B64C39/024 , B64C2201/021 , B64C2201/048 , B64C2201/088 , B64C2201/102
摘要： The present invention relates to an aircraft comprising a fuselage (100) comprising a fuselage axis (101), a first wing arrangement (110) and a second wing arrangement (120). The first wing arrangement (110) is mounted to the fuselage (100) such that the first wing arrangement (110) is tiltable around a first rotary wing axis (111) of the first wing arrangement (110) and such that the first wing arrangement (110) is rotatable around the fuselage axis (101). The first wing arrangement (110) is adapted in such a way that, in a fixed-wing flight mode, the first wing arrangement (110) do not rotate around the fuselage axis (101). The first wing arrangement (110) is further adapted in such a way that, in a hover flight mode, the first wing arrangement (110) is tilted around the respective first rotary wing axis (111) with respect to its orientation in the fixed-wing flight mode and that the first wing arrangement (110) rotates around the fuselage axis (101). The aircraft further comprises an extendible lift increasing system which is arranged to the first wing arrangement (110) for selectively amending a lift area of the first wing arrangement (110) in the fixed-wing flight mode and the hover flight mode.
摘要翻译：本发明涉及一种飞行器，其包括机身（100），其包括机身轴线（101），第一机翼装置（110）和第二机翼装置（120）。第一机翼装置（110）被安装到机身（100），使得第一机翼装置（110）围绕第一机翼装置（110）的第一旋转翼轴线（111）可倾斜，并且使得第一机翼装置（110）能够围绕机身轴线（101）旋转。第一机翼装置（110）以这种方式适配，使得在固定翼飞行模式中，第一机翼装置（110）不围绕机身轴线（101）旋转。第一机翼装置（110）进一步适应于在悬停飞行模式中，第一机翼装置（110）围绕其相应的第一旋转翼轴线（111）相对于其固定方向的取向倾斜，机翼飞行模式，并且第一机翼装置（110）围绕机身轴线（101）旋转。该飞机还包括可伸缩提升增加系统，该系统布置在第一机翼装置（110）上，用于以固定翼飞行模式和悬停飞行模式选择性地修理第一机翼装置（110）的提升区域。

4. 发明申请

WO2013120918A1 WING ADJUSTING MECHANISM 审中-公开
标题翻译： WING调整机制
公开(公告)号：WO2013120918A1
公开(公告)日：2013-08-22
申请号：PCT/EP2013/052911
申请日：2013-02-13
申请人： REITER, Johannes
发明人： REITER, Johannes
IPC分类号： B64C29/02 , B64C39/02 , B64C29/00 , B64C39/00 , B64C27/16 , B64C27/18
CPC分类号： B64C27/00 , B64C3/385 , B64C27/001 , B64C27/16 , B64C27/18 , B64C29/00 , B64C29/0033 , B64C29/0075 , B64C29/02 , B64C39/008 , B64C39/024 , B64C2201/088 , B64C2201/102 , B64C2201/104 , B64C2201/108 , B64C2201/165
摘要： The present invention relates to a device for generating aerodynamic lift and in particular an aircraft (100) for vertical take-off and landing. A wing arrangement (110) comprises at least one propulsion unit (111), wherein the propulsion unit (111) comprises a rotating mass which is rotatable around a rotary axis (117). The wing arrangement (110) is mounted to a fuselage (101) such that the wing arrangement (110) is tiltable around a longitudinal wing axis (112) of the wing arrangement (110) and such that the wing arrangement (110) is rotatable with respect to the fuselage (101) around a further rotary axis that differs to the longitudinal wing axis (112). An adjusting mechanism adjusts a tilting angle of the wing arrangement (110) around the longitudinal wing axis (112) under influence of a precession force (Fp) which forces the wing arrangement (110) to tilt around the longitudinal wing axis (112).
摘要翻译：本发明涉及一种用于产生空气动力升降装置，特别涉及用于垂直起飞和着陆的飞机（100）。机翼装置（110）包括至少一个推进单元（111），其中推进单元（111）包括围绕旋转轴线（117）旋转的旋转块。机翼装置（110）被安装到机身（101），使得机翼装置（110）围绕机翼装置（110）的纵向翼轴线（112）可倾斜，并且使得机翼装置（110）可旋转相对于机身（101）围绕与纵向翼轴（112）不同的另一旋转轴线。调节机构在促使机翼装置（110）围绕纵向机翼轴线（112）倾斜的进动力（Fp）的影响下调节机翼装置（110）围绕纵向翼轴线（112）的倾斜角度。

5. 发明申请

WO2013120912A1 AIRCRAFT FOR VERTICAL TAKE-OFF AND LANDING WITH TWO WING ARRANGEMENTS 审中-公开
标题翻译：用于双向安装的垂直起落架的飞机
公开(公告)号：WO2013120912A1
公开(公告)日：2013-08-22
申请号：PCT/EP2013/052903
申请日：2013-02-13
申请人： REITER, Johannes
发明人： REITER, Johannes
IPC分类号： B64C29/02 , B64C39/02 , B64C29/00
CPC分类号： B64C27/00 , B64C3/385 , B64C27/001 , B64C27/16 , B64C27/18 , B64C29/00 , B64C29/0033 , B64C29/0075 , B64C29/02 , B64C39/008 , B64C39/024 , B64C2201/088 , B64C2201/102 , B64C2201/104 , B64C2201/108 , B64C2201/165
摘要： The present invention relates to an aircraft comprising a fuselage (100) comprising a fuselage axis (101), a first wing arrangement (110) and a second wing arrangement (120). The first wing arrangement (110) is mounted to the fuselage (100) such that the first wing arrangement (110) is tiltable around a first longitudinal wing axis (111) of the first wing arrangement (110) and such that the first wing arrangement (110) is rotatable around the fuselage axis (101). The second wing arrangement (120) comprises at least one propulsion unit (122), wherein the second wing arrangement (120) is mounted to the fuselage (100) such that the second wing arrangement (120) is tiltable around a second longitudinal wing axis (121) of the second wing arrangement (120) and such that the second wing arrangement (120) is rotatable around the fuselage axis (101). The first wing arrangement (110) and the second wing arrangement (120) are adapted in such a way that, in a fixed-wing flight mode, the first wing arrangement (110) and the second wing arrangement (120) do not rotate around the fuselage axis (101). The first wing arrangement (110) and the second wing arrangement (120) are further adapted in such a way that, in a hover flight mode, the first wing arrangement (110) and the second wing arrangement (120) are tilted around the respective first longitudinal wing axis (111) and the respective second longitudinal wing axis (121) with respect to its orientations in the fixed-wing flight mode and that the first wing arrangement (110) and the second wing arrangement (120) rotate around the fuselage axis (101).
摘要翻译：本发明涉及一种飞行器，其包括机身（100），其包括机身轴线（101），第一机翼装置（110）和第二机翼装置（120）。第一机翼装置（110）安装到机身（100），使得第一机翼装置（110）能围绕第一机翼装置（110）的第一纵向机翼轴线（111）倾斜，并且使得第一机翼装置（110）能够围绕机身轴线（101）旋转。第二机翼装置（120）包括至少一个推进单元（122），其中第二机翼装置（120）安装到机身（100）上，使得第二机翼装置（120）可围绕第二纵向机翼轴线（121），并且使得所述第二机翼装置（120）能够围绕所述机身轴线（101）旋转。第一机翼装置（110）和第二机翼装置（120）以这样的方式适配，使得在固定翼飞行模式中，第一机翼装置（110）和第二机翼装置（120）不围绕机身轴（101）。第一机翼装置（110）和第二机翼装置（120）进一步适于以悬停飞行模式，第一机翼装置（110）和第二机翼装置（120）围绕相应的第一纵向翼片轴线（111）和相应的第二纵向翼片轴线（121）相对于其在固定翼飞行模式中的定向，并且第一翼形装置（110）和第二翼形装置（120）围绕机身旋转轴（101）。

6. 发明申请

WO2012035153A1 TILT WING ROTOR VTOL 审中-公开
标题翻译：倾斜转子垂直起落架
公开(公告)号：WO2012035153A1
公开(公告)日：2012-03-22
申请号：PCT/EP2011/066143
申请日：2011-09-16
申请人： REITER, Johannes
发明人： REITER, Johannes
IPC分类号： B64C29/00 , B64C29/02 , B64C39/02
CPC分类号： B64C29/00 , B64C29/02 , B64C39/024 , B64C2201/021 , B64C2201/088 , B64C2201/104 , B64C2201/165
摘要： The present invention relates to an aircraft (110) for vertical take-off and landing. The aircraft comprises a first wing (101), a second wing (102) and a fuselage (103). The first wing (101) comprises a first longitudinal wing axis (104) and the second wing (102) comprises a second longitudinal wing axis (104). The first wing (101) extends along the first longitudinal wing axis (104) and the second wing (102) extends along the second longitudinal wing axis (104) from the fuselage (103). The first wing (101) is tiltable with a first rotational direction around the first longitudinal wing axis (104) and the second wing (102) is tiltable with a second rotational direction around the second longitudinal wing axis (104). The wings (101, 102) are adapted in such a way that, in a fixed- wing flight mode, the wings (101, 102) do not rotate around a second axis (105). The wings (101, 102) are further adapted in such a way that, in a hover flight mode, the wings (101, 102) are tilted around the longitudinal wing axis (104) with respect to its orientation in the fixed- wing flight mode and that the wing (100) rotates around the second axis (105).
摘要翻译：本发明涉及用于垂直起飞和着陆的飞行器（110）。飞机包括第一翼（101），第二翼（102）和机身（103）。第一翼（101）包括第一纵向翼轴线（104），第二翼片（102）包括第二纵向翼轴线（104）。第一翼（101）沿着第一纵向翼轴（104）延伸，第二翼（102）从机身（103）沿着第二纵向翼轴（104）延伸。第一翼（101）可围绕第一纵向翼轴线（104）以第一旋转方向倾斜，并且第二翼（102）可围绕第二纵向翼轴线（104）以第二旋转方向倾斜。翼（101,102）适于以固定翼飞行模式，翼（101,102）不围绕第二轴（105）旋转。翼（101,102）进一步适于使得在悬停飞行模式中，翼（101,102）相对于其在固定翼飞行中的定向围绕纵向翼轴线（104）倾斜并且机翼（100）围绕第二轴线（105）旋转。

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