发明名称 |
MODULE OF LANDING SYSTEM OF FLYING VEHICLE |
摘要 |
FIELD: landing systems of flying vehicles. SUBSTANCE: module includes pressure accumulator with float secured on it, fairing, drive of diaphragm opening mechanism of pressure accumulator and fairing unlocking; fairing is secured on assembling area by means of clamping bands. Assembling area is made in form of ellipse and is provided with edge former and flexible ring located between edge former and inner surface of fairing. Tightness of module and synchronization of inflation of float at simultaneous release of fairing enhances reliability of module. EFFECT: enhanced operational reliability. 5 dwg øøø1
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申请公布号 |
RU2120886(C1) |
申请公布日期 |
1998.10.27 |
申请号 |
RU19960122707 |
申请日期 |
1996.11.26 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO NAUCHNO-PROIZVOD;STVENNOE OB EDINENIE ISKRA |
发明人 |
SMOL'NIKOV V.V.;SOKOLOVSKIJ M.I.;IL'ICHEV B.N.;PESTOV V.M.;MAKAREVICH JU.L. |
分类号 |
B64C25/56;(IPC1-7):B64C25/56 |
主分类号 |
B64C25/56 |
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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