发明名称 |
Rocket elevation angle measuring device - has pendulum positioning itself into firing direction by take-off acceleration |
摘要 |
<p>The measuring device determines and stores the angle of elevation on a launched rocket for evaluation and activation of certain switching and/or control functions. The rocket has a measuring system which determines the angle of elevation and stores the measured value for subsequent evaluation to take place after the firing. The measuring system consists of a housing contg. a potentiometer. The set spindle of the potentiometer carries a toothed wheel in mesh with an intermediary wheel only during the acceleration phase. The intermediary wheel is fitted on a shaft seated on a lateral bearing on the side which carries the intermediate wheel. The other side of the shaft carries out limited swinging movements around the bearing.</p> |
申请公布号 |
DE2557317(A1) |
申请公布日期 |
1977.06.30 |
申请号 |
DE19752557317 |
申请日期 |
1975.12.19 |
申请人 |
VEREINIGTE FLUGTECHNISCHE WERKE-FOKKER GMBH |
发明人 |
SEEGER,HANS-JOCHEN,DIPL.-ING. |
分类号 |
F41G3/12;F41G7/00;(IPC1-7):41G7/14 |
主分类号 |
F41G3/12 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|