发明名称 CARRIER SYSTEM FOR CARRYING OUT INTERCEPTION MANEUVERS OF A LOADBEARING PARAGLIDER AND METHOD FOR ADJUSTING THE TRAILING EDGE OF A LOADBEARING PARAGLIDER
摘要 A carrier system for carrying out interception maneuvers of a loadbearing paraglider which has a glider having a trailing edge for carrying out the maneuver with at least one interception line is fixed to said edge includes at least one carried load unit, which is connected to the carrier system via a first, short load carrier belt and a second, longer load carrier belt. A carried load connected to the carried load unit is carried by way of the first, short load carrier belt. The trailing edge is adjusted to carry out the maneuver by the gravitational force of the carried load, in that the first, short load carrier belt is separated and the carried load is carried by way of the longer, second load carrier belt.
申请公布号 US2016176531(A1) 申请公布日期 2016.06.23
申请号 US201514966997 申请日期 2015.12.11
申请人 Airbus Defence and Space GmbH 发明人 Biehl Juka
分类号 B64D17/22 主分类号 B64D17/22
代理机构 代理人
主权项 1. A carrier system for carrying out interception maneuvers of a loadbearing paraglider which comprises a glider having a trailing edge for carrying out the maneuver, wherein at least one interception line is fixed to said edge, comprising: at least one carried load unit connected to the carrier system via a first, short load carrier belt and a second, longer load carrier belt; wherein a carried load connected to the at least one carried load unit is carried by way of the first, short load carrier belt; and wherein the trailing edge is adjusted to carry out the maneuver by the gravitational force of the carried load, in that the first, short load carrier belt is separated so as to no longer connect the carried load to the carried load unit and the carried load is subsequently carried by way of the longer, second load carrier belt.
地址 Ottobrunn DE