发明名称 AIR PRESSURE TRANSDUCER
摘要 FIELD: devices for detection of aircraft flight characteristics or other liquid or gas flow investigation equipment. SUBSTANCE: device has rod, which carries multiple ribs oriented along it with groups of holes between ribs which are connected to connecting pipes via pneumatic circuits. Ribs are continuous in longitudinal direction, there number n is greater than 3. Groups of holes are located between ribs on smooth side surfaces of rod and are spaced from ribs by <EMI ID=0.339 HE=3 WI=15 TI=CHI>, where b is distance between ribs in arbitrary cross section of rod. Angle between side surfaces in arbitrary cross section of rod gamma. Sharp ribs may be rounded or blunted by roots, they may be also designed as projections. Side surfaces of rod may be convex, cylindrical, cone, and so on. Number of ribs on rod of air pressure transducer depends on goal and may be equal to four, five and six. EFFECT: simplified design, increased precision, decreased weight of device and flow measuring equipment. 9 cl, 13 dwg
申请公布号 RU2135971(C1) 申请公布日期 1999.08.27
申请号 RU19980112519 申请日期 1998.07.06
申请人 TSENTRAL'NYJ AEHROGIDRODINAMICHESKIJ INSTITUT IM.P;TSENTRAL NYJ AEHROGIDRODINAMIC 发明人 VOZHDAEV E.S.;GOLOVKIN M.A.;GOLOVKIN V.A.;EFREMOV A.A.;GORBAN' V.P.
分类号 G01P5/14;G01L19/00;G01P5/16;G01P5/165;G01P13/02;(IPC1-7):G01L19/00 主分类号 G01P5/14
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