ATTITUDE CONTROL DEVICE FOR AIRSHIP,申请号JP20010064171-传众专利搜索

ATTITUDE CONTROL DEVICE FOR AIRSHIP

申请公布号：JP2002264898(A)

申请号：JP20010064171

申请日期：2001.03.08

申请公布日期：2002.09.18

申请人：

FUJI HEAVY IND LTD

发明人：MATSUMOTO TAKASHI

分类号：B64B1/38;(IPC1-7):B64B1/38

主分类号：B64B1/38

摘要：PROBLEM TO BE SOLVED: To provide an attitude control device for an airship capable of quickly providing a desired attitude even under the influence of a disturbance such as gust or the like. SOLUTION: Each electric motor 7 in a connecting point a11 , a21 , a31 , and a41 or the like shown in Fig. 2 (B) and (C) rewinds a rope 6 in a space ratio from its constrained point a1 , a2 , a3 , and a4 or the like according to an instruction from a microprocessor based on a signal from a sensor which detects the down inclination of a stem. while each electric motor 7 in other connecting points winds the rope 6 in the space ratio from the connecting point to the constrained point a1 , a2 , a3 , and a4 or the like. Each electric motor 7 in a connecting point d11 , d21 , d31 , and d41 or the like shown in Fig. 2 (D) and (E) winds the rope 6 in a space ratio from its constraint point d1 , d2 , d3 , and d4 or the like, while each electric motor 7 in other connecting points rewinds the rope 6 in the space ratio from the connecting point to the constraint point d1 , d2 , d3 , and d4 or the like. Then, a diaphragm 3 reacts to it to immediately raise the stem as shown in Fig. 2 (A).