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1. 发明公开

CN1378952A 混合式飞机失效
公开(公告)号：CN1378952A
公开(公告)日：2002-11-13
申请号：CN02105234.4
申请日：1996-10-24
申请人：汉斯·J·伯恩
发明人：汉斯·J·伯恩
IPC分类号： B64C39/00 , B64C29/00 , B64C1/00
CPC分类号： B64C39/00 , B64B1/06 , B64B1/08 , B64B1/18 , B64B1/32 , B64B1/34 , B64B2201/00 , B64C27/52 , B64C29/00 , B64C29/0033 , B64C39/10 , B64C2001/0063 , B64C2001/0072 , B64C2001/0081 , Y02T50/12 , Y02T50/43
摘要：一种混合式飞机有VTOL、R－VTOL和S－STOL功能。飞机有产生升力的机身(1)和四个前后排列的翼段(20),它们前后排列并可绕其中性轴回转。每个翼段有安装在它上面可回转的旋翼螺旋桨(21)组件,用于提供基本上在水平与垂直之间范围内的推力。机翼和螺旋桨通过外伸架组合在机身上,外伸架设计成有很大的刚度并能将来自机翼和螺旋桨的力分配给机身。机身的形状设计为在气流中产生气动升力并可使构成它所需要的不同弯度的壁板数量减到最少程度。机身设计为由覆盖以半刚性壁板的增压张力框架、有覆盖的下部框架和包覆有头锥的机头构成。覆盖构架的半刚性壁板由气密和耐腐的层压材料制造并借助于连接肋和锁销装置与框架连接。框架由多个弯曲细长串排的分段构成,垂直于机身纵轴线并借助于承扭件连接。电涡轮传动系统可用于驱动飞机。还介绍了一种高级混合式飞机,它有约8至12个高速风扇的替代旋翼螺旋桨。

2. 发明授权

CN1094453C 混合式飞机失效
公开(公告)号：CN1094453C
公开(公告)日：2002-11-20
申请号：CN96198541.0
申请日：1996-10-24
申请人：汉斯·J·伯恩
发明人：汉斯·J·伯恩
IPC分类号： B64C29/00 , B64C1/00 , B64C39/00
CPC分类号： B64C39/00 , B64B1/06 , B64B1/08 , B64B1/18 , B64B1/32 , B64B1/34 , B64B2201/00 , B64C27/52 , B64C29/00 , B64C29/0033 , B64C39/10 , B64C2001/0063 , B64C2001/0072 , B64C2001/0081 , Y02T50/12 , Y02T50/43
摘要：一种混合式飞机有VTOL、R-VTOL和S-STOL功能。飞机有产生升力的机身(1)和四个前后排列的翼段(20)，它们前后排列并可绕其中性轴回转。每个翼段有安装在它上面可回转的旋翼螺旋桨(21)组件，用于提供基本上在水平与垂直之间范围内的推力。机翼和螺旋桨通过外伸架组合在机身上，外伸架设计成有很大的刚度并能将来自机翼和螺旋桨的力分配给机身。机身的形状设计为在气流中产生气动升力并可使构成它所需要的不同弯度的壁板数量减到最少程度。机身设计为由覆盖以半刚性壁板的增压张力框架、有覆盖的下部框架和包覆有头锥的机头构成。覆盖构架的半刚性壁板由气密和耐腐的层压材料制造并借助于连接肋和锁销装置与框架连接。框架由多个弯曲细长串排的分段构成，垂直于机身纵轴线并借助于承扭件连接。电涡轮传动系统可用于驱动飞机。还介绍了一种高级混合式飞机，它有约8至12个高速风扇的替代旋翼螺旋桨。

3. 发明公开

CN1202861A 混合式飞机失效
公开(公告)号：CN1202861A
公开(公告)日：1998-12-23
申请号：CN96198541.0
申请日：1996-10-24
申请人：汉斯·J·伯恩
发明人：汉斯·J·伯恩
IPC分类号： B64C29/00 , B64C1/00 , B64C39/00
CPC分类号： B64C39/00 , B64B1/06 , B64B1/08 , B64B1/18 , B64B1/32 , B64B1/34 , B64B2201/00 , B64C27/52 , B64C29/00 , B64C29/0033 , B64C39/10 , B64C2001/0063 , B64C2001/0072 , B64C2001/0081 , Y02T50/12 , Y02T50/43
摘要：一种混合式飞机有VTOL、R－VTOL和S－STOL功能。飞机有产生升力的机身(1)和四个前后排列的翼段(20),它们前后排列并可绕其中性轴回转。每个翼段有安装在它上面可回转的旋翼螺旋桨(21)组件,用于提供基本上在水平与垂直之间范围内的推力。机翼和螺旋桨通过外伸架组合在机身上,外伸架设计成有很大的刚度并能将来自机翼和螺旋桨的力分配给机身。机身的形状设计为在气流中产生气动升力并可使构成它所需要的不同弯度的壁板数量减到最少程度。机身设计为由覆盖以半刚性壁板的增压张力框架、有覆盖的下部框架和包覆有头锥的机头构成。覆盖构架的半刚性壁板由气密和耐腐的层压材料制造并借助于连接肋和锁销装置与框架连接。框架由多个弯曲细长串排的分段构成,垂直于机身纵轴线并借助于承扭件连接。电涡轮传动系统可用于驱动飞机。还介绍了一种高级混合式飞机,它有约8至12个高速风扇的替代旋翼螺旋桨。

4. 发明公开

CN107776892A 轻型可折叠察打一体无人机有权
公开(公告)号：CN107776892A
公开(公告)日：2018-03-09
申请号：CN201711223016.9
申请日：2017-11-29
申请人：哈尔滨模豆科技有限责任公司
发明人：吴春来
IPC分类号： B64C39/02 , B64C3/56 , B64C1/06 , B64C1/30 , B64D47/08 , B64D1/12
CPC分类号： B64C39/02 , B64C1/068 , B64C1/30 , B64C3/56 , B64C2001/0063 , B64C2001/0072 , B64C2201/12 , B64D1/12 , B64D47/08
摘要：本发明涉及无人机领域，特别是涉及一种轻型可折叠察打一体无人机，包括机身、机翼、折叠机构、平垂尾、侦察云台和投放机构，所述机身包括前段机身、后段机身、中央翼盒、机翼主梁、机身连接盒和机尾连接盒；所述机翼包括内段机翼和外段机翼；所述机翼设置有左右两副，两副机翼对称设置在机身的两侧；所述折叠机构包括机翼折叠机构和机身折叠机构；所述机翼折叠机构设置有两副。本发明提供了一种可快速折叠展开，成本低廉，结构简单易修复，具有优异的机动性和一定投放载荷的察打一体无人机，可用于实施军事侦察行动，执行快速精确打击任务，亦可应用于民用科研领域，如大气探测，地表测绘等。

5. 发明授权

CN1190345C 混合式飞机失效
公开(公告)号：CN1190345C
公开(公告)日：2005-02-23
申请号：CN02105234.4
申请日：1996-10-24
申请人：汉斯·J·伯恩
发明人：汉斯·J·伯恩
IPC分类号： B64C29/00 , B64C1/00 , B64C39/00
CPC分类号： B64C39/00 , B64B1/06 , B64B1/08 , B64B1/18 , B64B1/32 , B64B1/34 , B64B2201/00 , B64C27/52 , B64C29/00 , B64C29/0033 , B64C39/10 , B64C2001/0063 , B64C2001/0072 , B64C2001/0081 , Y02T50/12 , Y02T50/43
摘要：一种混合式飞机有VTOL、R-VTOL和S-STOL功能。飞机有产生升力的机身(1)和四个前后排列的翼段(20)，它们前后排列并可绕其中性轴回转。每个翼段有安装在它上面可回转的旋翼螺旋桨(21)组件，用于提供基本上在水平与垂直之间范围内的推力。机翼和螺旋桨通过外伸架组合在机身上，外伸架设计成有很大的刚度并能将来自机翼和螺旋桨的力分配给机身。机身的形状设计为在气流中产生气动升力并可使构成它所需要的不同弯度的壁板数量减到最少程度。机身设计为由覆盖以半刚性壁板的增压张力框架、有覆盖的下部框架和包覆有头锥的机头构成。覆盖构架的半刚性壁板由气密和耐腐的层压材料制造并借助于连接肋和锁销装置与框架连接。框架由多个弯曲细长串排的分段构成，垂直于机身纵轴线并借助于承扭件连接。电涡轮传动系统可用于驱动飞机。还介绍了一种高级混合式飞机，它有约8至12个高速风扇的替代旋翼螺旋桨。

6. 发明公开

EP1209076A3 Hybrid aircraft 失效
标题翻译：混合型飞机
公开(公告)号：EP1209076A3
公开(公告)日：2002-11-27
申请号：EP02075631.8
申请日：1996-10-24
申请人： Bothe, Hans-Jurgen
发明人： Bothe, Hans-Jurgen
IPC分类号： B64C29/00 , B64C1/00 , B64C39/00
CPC分类号： B64C39/00 , B64B1/06 , B64B1/08 , B64B1/18 , B64B1/32 , B64B1/34 , B64B2201/00 , B64C27/52 , B64C29/00 , B64C29/0033 , B64C39/10 , B64C2001/0063 , B64C2001/0072 , B64C2001/0081 , Y02T50/12 , Y02T50/43
摘要： A hybrid aircraft having VTOL R-VTOL and S-STOL capabilities having a lifting body hull (1) and four wing sections (20) arranged in tandem which are pivotally moveable about their neutral axis. Each wing section has mounted thereon a pivotal propeller-rotor (21) assembly for providing thrust substantially in a range between horizontal and vertical. The wings and propellers are integrated to the hull by an outrigger designed to be very stiff and to distribute forces from the wings and propellers from the hull. The hull is shaped to provide aerodynamic lift in an airstream and to facilitate construction by minimizing the number of panels of differing curvature required. The hull is formed of a pressure tensioned frame covered with semi-rigid panels, a lower cladding frame and bow and stem cladding nose cones. The semi-rigid panels covering the frame are formed of gas-tight and abrasion resistant laminate material and are connected to the frame by means of an interface rib and latch system. The frame is formed of a plurality of curved elongate segments arranged in series orthogonal to the long axis of the hull and connected by means of torsion members. A turbo-electric drive system can be used to drive the aircraft. An advanced hybrid aircraft is also described having about 8 to 12 high speed fans in place of the propeller-rotors.

7. 发明申请

WO2002092928A1 MODULAR BUILDING STRUCTURE 审中-公开
标题翻译：模块化建筑结构
公开(公告)号：WO2002092928A1
公开(公告)日：2002-11-21
申请号：PCT/US2001/010904
申请日：2001-04-04
申请人： ZORNES, David
发明人： ZORNES, David
IPC分类号： E04B1/14
CPC分类号： B64C1/06 , B29C44/348 , B64C2001/0063 , B64C2001/0072 , B64C2001/0081 , E04B1/14 , E04B1/6104 , E04B2/12 , E04B2001/0069 , E04B2001/6191 , F16B5/02 , F16B35/00 , F24S20/66 , F24S2020/10 , F28D7/0041 , F28F21/02 , Y02B10/20 , Y02E10/44 , Y02T50/43
摘要： A hexagon building structure offset layering system uses hexagon structures assembled in an offset layering architecture to construct building walls, floors, roofs, and other structures. Hexagon building structures (7) include interior panels (1) and (2) that are adhered to both sides of a foam core (3). The structures (7) also include radial cutouts (6) at each corner for offset layering assembly with another structure (7). Peg retainers (5) selectively secure the hexagon building structures (7) to one another. Six alignments fastening holes (4) are equidistantly spaced and located on interior panels (1) and (2). The holes (4) provide fastener locations for screwing or bolting through the layers of the hexagon. The holes (4) align with an offset layer of hexagons when assembled in the axial direction. Conduct holes (12) are selectively located depending on the fastening technique selected. The hexagon system includes five derivatives of hexagon building structures (7) and a door or window header, providing square, triangular, and curved geometries when assembled. Since hexagon buildings are built from hexagon building structures (7) without customization, hexagon buildings can be rebuilt, modified, or recycled onto a like building using the same materials.
摘要翻译：六角建筑结构偏移分层系统使用在偏移分层结构中组装的六边形结构来构建建筑物墙壁，地板，屋顶和其他结构。六边形建筑结构（7）包括粘附在泡沫芯（3）两侧的内部面板（1）和（2）。结构（7）还包括在每个拐角处的用于具有另一结构（7）的偏移层叠组件的径向切口（6）。栓保持器（5）选择性地将六边形建筑结构（7）彼此固定。六个对准紧固孔（4）等距间隔开并位于内板（1）和（2）上。孔（4）提供用于螺纹连接或螺栓穿过六边形层的紧固件位置。当沿轴向组装时，孔（4）与六边形偏移层对准。导孔（12）根据所选的紧固技术选择性地定位。六边形系统包括五角形六角形建筑结构（7）和门或窗头，当组装时提供方形，三角形和弯曲几何形状。由于六边形建筑物是由六边形建筑结构（7）建造的，不需要定制，因此六边形建筑物可以使用相同的材料重建，修改或回收到类似建筑物上。

8. 发明申请

WO02092928A8 MODULAR BUILDING STRUCTURE 审中-公开
标题翻译：模块化建筑结构
公开(公告)号：WO02092928A8
公开(公告)日：2003-04-10
申请号：PCT/US0110904
申请日：2001-04-03
申请人： ZORNES DAVID
发明人： ZORNES DAVID
IPC分类号： B29C44/34 , B64C1/00 , E04B1/00 , E04B1/14 , E04B1/61 , E04B2/12 , F16B5/02 , F16B35/00 , F24J2/04 , F28D7/00 , F28F21/02 , E04B2/22
CPC分类号： B64C1/06 , B29C44/348 , B64C2001/0063 , B64C2001/0072 , B64C2001/0081 , E04B1/14 , E04B1/6104 , E04B2/12 , E04B2001/0069 , E04B2001/6191 , F16B5/02 , F16B35/00 , F24J2/0444 , F24J2002/0038 , F28D7/0041 , F28F21/02 , Y02B10/20 , Y02E10/44 , Y02T50/433
摘要： A hexagon building structure offset layering system uses hexagon structures assembled in an offset layering architecture to construct building walls, floors, roofs, and other structures. Hexagon building structures (7) include interior panels (1) and (2) that are adhered to both sides of a foam core (3). The structures (7) also include radial cutouts (6) at each corner for offset layering assembly with another structure (7). Peg retainers (5) selectively secure the hexagon building structures (7) to one another. Six alignments fastening holes (4) are equidistantly spaced and located on interior panels (1) and (2). The holes (4) provide fastener locations for screwing or bolting through the layers of the hexagon. The holes (4) align with an offset layer of hexagons when assembled in the axial direction. Conduct holes (12) are selectively located depending on the fastening technique selected. The hexagon system includes five derivatives of hexagon building structures (7) and a door or window header, providing square, triangular, and curved geometries when assembled. Since hexagon buildings are built from hexagon building structures (7) without customization, hexagon buildings can be rebuilt, modified, or recycled onto a like building using the same materials.
摘要翻译：六角建筑结构偏移分层系统使用在偏移分层结构中组装的六边形结构来构建建筑物墙壁，地板，屋顶和其他结构。六边形建筑结构（7）包括粘附在泡沫芯（3）两侧的内部面板（1）和（2）。结构（7）还包括在每个拐角处的用于具有另一结构（7）的偏移层叠组件的径向切口（6）。栓保持器（5）选择性地将六边形建筑结构（7）彼此固定。六个对准紧固孔（4）等距间隔开并位于内板（1）和（2）上。孔（4）提供用于螺纹连接或螺栓穿过六边形层的紧固件位置。当沿轴向组装时，孔（4）与六边形偏移层对准。导孔（12）根据所选的紧固技术选择性地定位。六边形系统包括五角形六角形建筑结构（7）和门或窗头，当组装时提供方形，三角形和弯曲几何形状。由于六边形建筑物是由六边形建筑结构（7）建造的，不需要定制，因此六边形建筑物可以使用相同的材料重建，修改或回收到类似建筑物上。

9. 发明申请

WO9715492A2 HYBRID AIRCRAFT 审中-公开
标题翻译：混合飞机
公开(公告)号：WO9715492A2
公开(公告)日：1997-05-01
申请号：PCT/CA9600705
申请日：1996-10-24
申请人： BOTHE HANS JURGEN
发明人： BOTHE HANS-JURGEN
IPC分类号： B64B1/06 , B64B1/08 , B64B1/18 , B64B1/32 , B64B1/34 , B64C1/00 , B64C1/26 , B64C27/52 , B64C29/00 , B64C39/00 , B64C39/10
CPC分类号： B64C39/00 , B64B1/06 , B64B1/08 , B64B1/18 , B64B1/32 , B64B1/34 , B64B2201/00 , B64C27/52 , B64C29/00 , B64C29/0033 , B64C39/10 , B64C2001/0063 , B64C2001/0072 , B64C2001/0081 , Y02T50/12 , Y02T50/433
摘要： A hybrid aircraft is taught having VTOL, R-VTOL and S-STOL capabilities. The aircraft has a lifting body hull (1) and four wing sections (20) arranged in tandem which are pivotally moveable about their neutral axis. Each wing section has mounted thereon a pivotal propeller-rotor (21) assembly for providing thrust substantially in a range between horizontal and vertical. The wings and propellers are integrated to the hull by an outrigger designed to be very stiff and to distribute forces from the wings and propellers to the hull. The hull is shaped to provide aerodynamic lift in an airstream and to facilitate construction by minimizing the number of panels of differing curvature required. The hull is formed of a pressure tensioned frame covered with semi-rigid panels, a lower cladding frame and bow and stem cladding nose cones. The semi-rigid panels covering the frame are formed of gas-tight and abrasion resistant laminate material and are connected to the frame by means of an interface rib and latch system. The frame is formed of a plurality of curved elongate segments arranged in series orthogonal to the long axis of the hull and connected by means of torsion members. A turbo-electric drive system can be used to drive the aircraft. An advanced hybrid aircraft is also described having about 8 to 12 high speed fans in place of the propeller-rotors.
摘要翻译：混合飞机被教导有VTOL，R-VTOL和S-STOL功能。飞行器具有提升体体（1）和四个翼形部分（20），它们串联布置，其可绕其中性轴线枢转运动。每个翼部分安装有枢转的螺旋桨 - 转子（21）组件，用于提供基本上在水平和垂直之间的范围内的推力。机翼和螺旋桨通过设计成非常坚固的外伸支架并将力从翼和螺旋桨分配到船体而与船体结合在一起。船体被成形为在空气流中提供空气动力提升，并且通过最小化所需曲率不同的面板的数量来促进构造。船体由覆盖有半刚性板，下包层框架和弓和茎包覆鼻锥的压力张紧框架形成。覆盖框架的半刚性面板由气密且耐磨的层压材料形成，并且通过界面肋和闩锁系统连接到框架。框架由多个弯曲的细长段形成，该多个弯曲细长段与船体的长轴正交并且通过扭转构件连接。涡轮增压驱动系统可用于驱动飞机。还描述了一种先进的混合动力飞机，具有大约8到12个高速风扇代替螺旋桨转子。

10. 发明公开

EP1209076A2 Hybrid aircraft 失效
标题翻译：混合飞机
公开(公告)号：EP1209076A2
公开(公告)日：2002-05-29
申请号：EP02075631.8
申请日：1996-10-24
申请人： Bothe, Hans-Jurgen
发明人： Bothe, Hans-Jurgen
IPC分类号： B64C29/00 , B64C1/00 , B64C39/00
CPC分类号： B64C39/00 , B64B1/06 , B64B1/08 , B64B1/18 , B64B1/32 , B64B1/34 , B64B2201/00 , B64C27/52 , B64C29/00 , B64C29/0033 , B64C39/10 , B64C2001/0063 , B64C2001/0072 , B64C2001/0081 , Y02T50/12 , Y02T50/43
摘要： A hybrid aircraft having VTOL R-VTOL and S-STOL capabilities having a lifting body hull (1) and four wing sections (20) arranged in tandem which are pivotally moveable about their neutral axis. Each wing section has mounted thereon a pivotal propeller-rotor (21) assembly for providing thrust substantially in a range between horizontal and vertical. The wings and propellers are integrated to the hull by an outrigger designed to be very stiff and to distribute forces from the wings and propellers from the hull. The hull is shaped to provide aerodynamic lift in an airstream and to facilitate construction by minimizing the number of panels of differing curvature required. The hull is formed of a pressure tensioned frame covered with semi-rigid panels, a lower cladding frame and bow and stem cladding nose cones. The semi-rigid panels covering the frame are formed of gas-tight and abrasion resistant laminate material and are connected to the frame by means of an interface rib and latch system. The frame is formed of a plurality of curved elongate segments arranged in series orthogonal to the long axis of the hull and connected by means of torsion members. A turbo-electric drive system can be used to drive the aircraft. An advanced hybrid aircraft is also described having about 8 to 12 high speed fans in place of the propeller-rotors.
摘要翻译：具有VTOL R-VTOL和S-STOL能力的混合动力飞机具有提升体壳体（1）和四个前后布置的机翼部分（20），所述机翼部分（20）可围绕其中性轴线枢转地移动。每个翼段在其上安装有枢转螺旋桨 - 转子（21）组件，用于提供基本上在水平和垂直之间范围内的推力。机翼和螺旋桨通过设计成非常坚硬的支腿与船体相结合，并从机身和螺旋桨上分配来自船体的力。船体成形为在气流中提供气动升力，并通过最小化所需曲率不同的面板的数量来促进施工。船体由压力张紧框架形成，覆盖有半刚性面板，下覆层框架以及弓形和杆状覆层鼻锥体。覆盖框架的半刚性面板由气密和耐磨层压材料形成，并通过接口肋和闩锁系统连接到框架。该框架由多个弯曲的细长段形成，该多个弯曲的细长段与船体的长轴线正交地排列并通过扭转构件连接。可以使用涡轮驱动系统来驱动飞机。还描述了一种高级混合动力飞机，其具有大约8至12个高速风扇来代替螺旋桨转子。

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