发明名称 |
Torsion sensor for detecting torsional stiffness of rotor blade used in helicopter rotor, has surface elements that are aligned and distributed radially around torque shaft, while connectors are provided in inter-connected state |
摘要 |
<p>The torsion sensor (1) has a strain gauge (6) that is arranged on several surface elements (5). The surface elements are aligned and distributed radially around the torque shaft (4). A primary connector (2) is inter-connected to secondary connector (3).</p> |
申请公布号 |
DE102011000054(A1) |
申请公布日期 |
2012.07.12 |
申请号 |
DE20111000054 |
申请日期 |
2011.01.07 |
申请人 |
DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V. |
发明人 |
OPITZ, STEFFEN |
分类号 |
G01L3/10;G01L3/14 |
主分类号 |
G01L3/10 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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