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公开(公告)号:EP1706317A1
公开(公告)日:2006-10-04
申请号:EP04803021.7
申请日:2004-12-16
发明人: TVINGSHOLM, John
IPC分类号: B64F1/08 , B64C31/036 , B64C31/032
CPC分类号: B64C31/032 , B64C31/036 , B64D17/025 , B64F1/08
摘要: A towing winch apparatus for paragliders and hang-gliders (4,6) is provided which comprises a line (3) and a towing winch mechanism (5) adapted to apply tension to said line (3) during towing, where one end (15) of the line (3) is releaseably attached to the ground (16) during towing and the towing winch mechanism (5) is attached to the paraglider or hang-glider (4,6). In this way a towing winch apparatus is provided which is useable by a pilot (1) of a paraglider or hang-glider (4,6) without needing a helper on the ground (16). In addition, after the tow process, the pilot (1) of a paraglider or hang-glider (4,6) doesn't need to go back to the ground (16) in order to collect the towing winch mechanism (5).
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公开(公告)号:EP4313760A1
公开(公告)日:2024-02-07
申请号:EP22719390.1
申请日:2022-03-18
申请人: Lolatchy, Schain
发明人: Lolatchy, Schain
IPC分类号: B64C27/00 , B64C27/04 , B64C27/26 , B64C31/032
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公开(公告)号:EP1899220A1
公开(公告)日:2008-03-19
申请号:EP05769453.1
申请日:2005-07-07
申请人: Nimbus S.R.L.
发明人: CAPUANI, Alfredo
IPC分类号: B64B1/02 , B64C31/032
CPC分类号: B64C31/032 , B64B1/02 , B64B2201/00
摘要: The aircraft (10) comprises an elongated framework (26) provided with propelling means and direction-control planes. The framework is coupled to a pneumatic chamber (16) suited to be filled with lighter-than-air gas and comprising two tubular branches (12, 14) joined to form a V-shaped profile, with an aerodinamic-lift surface (22, 24) extending therebetween.
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公开(公告)号:EP3630600B1
公开(公告)日:2023-01-04
申请号:EP18810496.2
申请日:2018-06-01
IPC分类号: B64C17/00 , B64C13/30 , B64C3/38 , B64C31/032 , B64C39/02
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公开(公告)号:EP3630600A1
公开(公告)日:2020-04-08
申请号:EP18810496.2
申请日:2018-06-01
申请人: Romaeris Corporation
IPC分类号: B64C17/00 , B64C13/30 , B64C3/38 , B64C31/032 , B64C39/02
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公开(公告)号:EP1899220B1
公开(公告)日:2011-04-13
申请号:EP05769453.1
申请日:2005-07-07
申请人: Nimbus S.R.L.
发明人: CAPUANI, Alfredo
IPC分类号: B64B1/02 , B64C31/032
CPC分类号: B64C31/032 , B64B1/02 , B64B2201/00
摘要: The aircraft (10) comprises an elongated framework (26) provided with propelling means and direction-control planes. The framework is coupled to a pneumatic chamber (16) suited to be filled with lighter-than-air gas and comprising two tubular branches (12, 14) joined to form a V-shaped profile, with an aerodinamic-lift surface (22, 24) extending therebetween.
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