| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 混合式飞机 | CN96198541.0 | 1996-10-24 | CN1094453C | 2002-11-20 | 汉斯·J·伯恩 |
| 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 | 混合式飞机 | CN02105234.4 | 1996-10-24 | CN1378952A | 2002-11-13 | 汉斯·J·伯恩 |
| 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 | 混合式飞机 | CN02105234.4 | 1996-10-24 | CN1190345C | 2005-02-23 | 汉斯·J·伯恩 |
| 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 | 混合式飞机 | CN96198541.0 | 1996-10-24 | CN1202861A | 1998-12-23 | 汉斯·J·伯恩 |
| 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。 | ||||||
| 5 | Hybrid aircraft | JP51615697 | 1996-10-24 | JPH11513635A | 1999-11-24 | ボセ ハンス−ユーゲン |
| 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. <IMAGE> | ||||||
| 6 | Hybrid aircraft | EP02075573.2 | 1996-10-24 | EP1211172A3 | 2002-11-27 | Bothe, Hans-Jurgen |
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. |
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| 7 | Hybrid aircraft | EP02075630.0 | 1996-10-24 | EP1211173A2 | 2002-06-05 | Bothe, Hans-Jurgen |
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. |
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| 8 | Hybrid aircraft | EP02075573.2 | 1996-10-24 | EP1211172A2 | 2002-06-05 | Bothe, Hans-Jurgen |
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. |
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| 9 | Hybrid aircraft | EP02075631.8 | 1996-10-24 | EP1209076A2 | 2002-05-29 | Bothe, Hans-Jurgen |
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. |
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| 10 | Hybrid aircraft | EP02075630.0 | 1996-10-24 | EP1211173A3 | 2002-11-27 | Bothe, Hans-Jurgen |
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. |
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| 11 | Hybrid aircraft | EP02075631.8 | 1996-10-24 | EP1209076A3 | 2002-11-27 | Bothe, Hans-Jurgen |
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. |
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| 12 | HYBRID AIRCRAFT | EP96934255.9 | 1996-10-24 | EP0854821B1 | 2002-05-02 | Bothe, Hans-Jurgen |
| 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. |
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| 13 | HYBRID AIRCRAFT | EP96934255.0 | 1996-10-24 | EP0854821A2 | 1998-07-29 | Bothe, Hans-Jurgen |
| 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. |
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| 14 | Hybrid aircraft | US547574 | 1995-10-24 | US5823468A | 1998-10-20 | Hans-Jurgen Bothe |
| A hybrid aircraft is taught having VTOL, R-VTOL and S-STOL capabilities. The aircraft has a lifting body hull and four wing sections arranged in tandem which are pivotally moveable about their neutral axis. Each wing section has mounted thereon a pivotal propeller-rotor 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. | ||||||
| 15 | Barrel-curved, wreck-resistant cabin | US3718295D | 1970-12-29 | US3718295A | 1973-02-27 | MOORE A |
| A light-weight, shock-resistant vehicular cabin or other insulated, barrel-curved container, mainly constructed of elongated, stave-like members, each of which comprises: a pair of spaced side pieces (of wood, sheet metal or metallic mesh), having outer edges that curvingly slope from the greatest bulge of the container toward the forward and rearward ends of the cabin; firm, molded filler material (plastic - preferably foamed - or light-weight concrete or the like) between the side pieces; and a hollow element or elements in the filler, containing gaseous material (air or other gas, optionally pressurized, or gas-cell-containing foam plastic). The hollow elements may be: single, sealed, bent tubes, each being nearly the length of the cabin; cans in end-to-end relation; bent bamboo or straight bamboo sections; slender, plastic tubes; or small balloons. The gaseous material in the hollow elements may be: air or non-aerial gas at or above atmospheric pressure; or gas-cell-containing foam plastic, which optionally may be under internal, aboveatmospheric pressure. Bonding material is between adjacent faces of the stave-like members, and preferably the assembled members are tautly encompassed by hoops or equivalent looped means - for example, tautly applied metallic mesh. The outer skin means may comprise rubber sheeting or other rubber coating. In the preferred vehicular form, windowed doors or hatches are provided.
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| 16 | Filament reinforced structure and method of making | US3579411D | 1967-09-27 | US3579411A | 1971-05-18 | MACKIE WILLIAM L; WILSON EDGAR D |
| A LIGHTWEIGHT, HIGH STRENGTH STRUCTURE AND METHOD OF MAKING SAME. SPACED PANELS ARE INTERCONNECTED BY HIGH TENSILE STRENGTH FLEXIBLE FILMAENTS OF GLASS FIBER OR METAL WHICH FILAMENTS PENETRATE THROUGH THE PANELS, AND ARE WOVEN BACK AND FORTH. THE PORTIONS OF THE FILAMENTS EXTENDING BETWEEN THE PANELS ARE SUBSEQUENTLY RIGIDIZED BY THE ADDITION OF A COATING WHICH, WHEN SOLIDIFED, IMPARTS SUBSTANTIAL COMPRESSIVE STRENGTH. TO COUNTER SHEAR FORCES CERTAIN FILAMENTS MAY BE ARRANGED TO SLANT IN THE DIRECTION OF ANTICIPATED STRESS. SINCE THE FILAMENTS PASS THROUGH AND OVERLIE PORTIONS OF THE PANELS THEY EFFECTIVELY COUNTER DELAMINATION OR PEELING.
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| 17 | Method of making reinforced honeycomb sandwich | US3578526D | 1968-01-22 | US3578526A | 1971-05-11 | HARDING HOWARD H |
| A LIGHTWEIGHT, SANDWHICH CONSTRUCTION COMPRISING A HONEYCOMB CORE MEMBER WITH END-GRAIN BALSA WOOD IMPRESSED THEREINTO TO FILL THE CELL THEREOF AT SELECTED POSITIONS FOR THE PURPOSE OF STRENGTHENING THE HONEYCOMB FOR MACHINING OR LOAD CARRYING SUCH AS BOLT RETENTION AND PREFERABLY INCLUDING PLASTIC IMPREGNATED FIBER GLASS SHEETS ADHESIVELY BONDED TO THE OPPPOSITE SIDES OF THE END-GRAIN
BALSA WOOD IMPRESSED HONEYCOMB CORE TO FORM A SANDWICH CONTRUCTION THEREOF AND THE METHOD OF SO FABRICATING SUCH SANDWICH CONSTRUCTION. |
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| 18 | Self-supporting shell for flying body | US40295954 | 1954-01-08 | US2817484A | 1957-12-24 | STENZEL FRITZ MIRKO B |
| 19 | Rotary stud fastener and installation thereof | US46303542 | 1942-10-23 | US2330169A | 1943-09-21 | CHURCHILL WILMER H |
| 20 | Structural element | US33219440 | 1940-04-29 | US2329366A | 1943-09-14 | WEILL MELVILLE K; ETIENNE MAUTNER |
