专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 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.

2. 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。

3. 发明授权

EP0854821B1 HYBRID AIRCRAFT 失效
标题翻译： HYBRID飞机
公开(公告)号：EP0854821B1
公开(公告)日：2002-05-02
申请号：EP96934255.9
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.

4. 发明公开

EP0854821A2 HYBRID AIRCRAFT 失效
标题翻译： HYBRID飞机
公开(公告)号：EP0854821A2
公开(公告)日：1998-07-29
申请号：EP96934255.0
申请日：1996-10-24
申请人： Bothe, Hans-Jurgen
发明人： Bothe, Hans-Jurgen
IPC分类号： B64B1 , B64C1 , B64C27 , B64C29 , B64C39
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.

5. 发明公开

EP1211173A3 Hybrid aircraft 失效
标题翻译：混合型飞机
公开(公告)号：EP1211173A3
公开(公告)日：2002-11-27
申请号：EP02075630.0
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 , B64B1/00 , B64B1/08
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.

6. 发明公开

EP1211172A3 Hybrid aircraft 失效
公开(公告)号：EP1211172A3
公开(公告)日：2002-11-27
申请号：EP02075573.2
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. 发明公开

EP1211173A2 Hybrid aircraft 失效
公开(公告)号：EP1211173A2
公开(公告)日：2002-06-05
申请号：EP02075630.0
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 , B64B1/00
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.

8. 发明公开

EP1211172A2 Hybrid aircraft 失效
公开(公告)号：EP1211172A2
公开(公告)日：2002-06-05
申请号：EP02075573.2
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.

9. 发明申请

WO1997015492A3 HYBRID AIRCRAFT 审中-公开
公开(公告)号：WO1997015492A3
公开(公告)日：1997-05-01
申请号：PCT/CA1996000705
申请日：1996-10-24
申请人： BOTHE, Hans-Jurgen
IPC分类号： B64C29/00

10. 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。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式