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公开(公告)号：EP0714363A1
公开(公告)日：1996-06-05
申请号：EP95900354.0
申请日：1994-08-24
申请人： Gevers, David E.
发明人： Gevers, David E.
CPC分类号： B64D35/04 , B64C1/00 , B64C3/38 , B64C3/54 , B64C3/56 , B64C25/52 , B64C25/54 , B64C25/66 , B64C35/00 , B64C35/002 , B64C35/008 , B64C2001/0045 , B64D27/00 , B64D27/08 , B64D29/04 , Y02T50/12 , Y02T50/14 , Y02T50/44
摘要： Several innovative systems for an aircraft, and aircraft incorporating them, are disclosed. Features include inboard-mounted engine(s) (24,25) with a belt drive system (84,99) for turning wing-situated propellers (8,9); compound landing gear integrating ski (29,114), pontoon and wheel (18,19,21) subcomponents; pivotal mounting armatures (6,7) for landing gear and/or propellers which provide a plurality of possible landing gear and/or propeller configurations; and a compound wing structure (14,15) featuring extendable wing panels (4,5) that permit the wing span of the aircraft to be nearly doubled while in flight. Aircraft incorporating such features will enjoy several safety advantages over conventional multi-engine aircraft and will be capable of modifications during flight which permit landings on any of snow, hard surfaces (runways) and water.
摘要翻译： 披露了一些飞机的创新系统，以及包含它们的飞机。 特征包括内置发动机（24,25）和带驱动系统（84,99），用于转动机翼定位的螺旋桨（8,9）; 整合滑雪（29,114），浮桥和轮（18,19,21）子组件的复式起落架; 用于起落架和/或螺旋桨的枢转安装衔铁（6,7），其提供多个可能的起落架和/或螺旋桨结构; 以及具有可延伸的翼板（4,5）的复合翼结构（14,15），其允许飞行器的机翼跨度在飞行中几乎翻倍。 结合这样的特征的飞机将比常规的多引擎飞机具有几个安全优点，并且能够在飞行期间进行修改，这允许在雪，硬的表面（跑道）和水中的任一个上着陆。
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公开(公告)号：EP0714363B1
公开(公告)日：1998-01-07
申请号：EP95900354.2
申请日：1994-08-24
申请人： Gevers, David E.
发明人： Gevers, David E.
CPC分类号： B64D35/04 , B64C1/00 , B64C3/38 , B64C3/54 , B64C3/56 , B64C25/52 , B64C25/54 , B64C25/66 , B64C35/00 , B64C35/002 , B64C35/008 , B64C2001/0045 , B64D27/00 , B64D27/08 , B64D29/04 , Y02T50/12 , Y02T50/14 , Y02T50/44
摘要： Several innovative systems for an aircraft, and aircraft incorporating them, are disclosed. Features include inboard-mounted engine(s) (24,25) with a belt drive system (84,99) for turning wing-situated propellers (8,9); compound landing gear integrating ski (29,114), pontoon and wheel (18,19,21) subcomponents; pivotal mounting armatures (6,7) for landing gear and/or propellers which provide a plurality of possible landing gear and/or propeller configurations; and a compound wing structure (14,15) featuring extendable wing panels (4,5) that permit the wing span of the aircraft to be nearly doubled while in flight. Aircraft incorporating such features will enjoy several safety advantages over conventional multi-engine aircraft and will be capable of modifications during flight which permit landings on any of snow, hard surfaces (runways) and water.
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公开(公告)号：EP0798207A3
公开(公告)日：1998-04-08
申请号：EP97109971.8
申请日：1994-08-24
申请人： Gevers, David E.
发明人： Gevers, David E.
CPC分类号： B64D35/04 , B64C1/00 , B64C3/38 , B64C3/54 , B64C3/56 , B64C25/52 , B64C25/54 , B64C25/66 , B64C35/00 , B64C35/002 , B64C35/008 , B64C2001/0045 , B64D27/00 , B64D27/08 , B64D29/04 , Y02T50/12 , Y02T50/14 , Y02T50/44
摘要： Several innovative systems for an aircraft, and aircraft incorporating them, are disclosed. Features include inboard-mounted engine(s) (24,25) with a belt drive system (84,99) for turning wing-situated propellers (8,9); compound landing gear integrating ski (29,114), pontoon and wheel (18,19,21) subcomponents; pivotal mounting armatures (6,7) for landing gear and/or propellers which provide a plurality of possible landing gear and/or propeller configurations; and a compound wing structure (14,15) featuring extendable wing panels (4,5) that permit the wing span of the aircraft to be nearly doubled while in flight. Aircraft incorporating such features will enjoy several safety advantages over conventional multi-engine aircraft and will be capable of modifications during flight which permit landings on any of snow, hard surfaces (runways) and water.
摘要翻译： 披露了一些飞机的创新系统，以及包含它们的飞机。 特征包括内置发动机（24,25）和带驱动系统（84,99），用于转动机翼定位的螺旋桨（8,9）; 整合滑雪（29,114），浮桥和轮（18,19,21）子组件的复式起落架; 用于起落架和/或螺旋桨的枢转安装衔铁（6,7），其提供多个可能的起落架和/或螺旋桨结构; 以及具有可延伸的翼板（4,5）的复合翼结构（14,15），其允许飞行器的机翼跨度在飞行中几乎翻倍。 结合这样的特征的飞机将比常规的多引擎飞机具有几个安全优点，并且能够在飞行期间进行修改，这允许在雪，硬的表面（跑道）和水中的任一个上着陆。
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公开(公告)号：EP0798207A2
公开(公告)日：1997-10-01
申请号：EP97109971.8
申请日：1994-08-24
申请人： Gevers, David E.
发明人： Gevers, David E.
CPC分类号： B64D35/04 , B64C1/00 , B64C3/38 , B64C3/54 , B64C3/56 , B64C25/52 , B64C25/54 , B64C25/66 , B64C35/00 , B64C35/002 , B64C35/008 , B64C2001/0045 , B64D27/00 , B64D27/08 , B64D29/04 , Y02T50/12 , Y02T50/14 , Y02T50/44
摘要： Several innovative systems for an aircraft, and aircraft incorporating them, are disclosed. Features include inboard-mounted engine(s) (24,25) with a belt drive system (84,99) for turning wing-situated propellers (8,9); compound landing gear integrating ski (29,114), pontoon and wheel (18,19,21) subcomponents; pivotal mounting armatures (6,7) for landing gear and/or propellers which provide a plurality of possible landing gear and/or propeller configurations; and a compound wing structure (14,15) featuring extendable wing panels (4,5) that permit the wing span of the aircraft to be nearly doubled while in flight. Aircraft incorporating such features will enjoy several safety advantages over conventional multi-engine aircraft and will be capable of modifications during flight which permit landings on any of snow, hard surfaces (runways) and water.
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