发明名称 Multiple function generator for aircraft flight instruments
摘要 A multiple function generator is described in the environment of an airspeed indicator for controlling the maximum allowable airspeed needle in accordance with a plurality of selectable functions of altitude and comprises a cam having a plurality of surface segments shaped in accordance with the functions positioning a cam follower coupled to the maximum allowable airspeed needle. A null-seeking electro-mechanical feedback servo mechanism having an altitude signal applied to its input synchro drives the cam, thereby positioning the needle in accordance with the function of altitude represented by the cam surface segment in contact with the follower. Means are included for altering the null index of the servo thereby selectively engaging the desired cam functionsurface segment with the cam follower in accordance with the function desired. A selection knob is coupled with the indexing means for selecting the function.
申请公布号 US4081730(A) 申请公布日期 1978.03.28
申请号 US19760696457 申请日期 1976.06.16
申请人 SPERRY RAND CORPORATION 发明人 MURTLAND, WILLIAM H.
分类号 G01C5/00;G01C23/00 主分类号 G01C5/00
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