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公开(公告)号：US4220551A
公开(公告)日：1980-09-02
申请号：US56344
申请日：1979-07-10
IPC分类号： C09K11/00 , C01B33/12 , C09K11/08 , C09K11/77 , G03C1/815 , G21K4/00 , H01J29/20 , H01J61/44 , C09K11/46
CPC分类号： C09K11/7734
摘要： Luminophors which luminesce in the blue region of the spectrum have the formula:M.sub.5 (1-.alpha.)Eu.sub.5.alpha..sup.2+ SiO.sub.4 X.sub.6wherein M represents Ba.sub.1-.beta. Sr.sub..beta. or Ba.sub.1-.beta. Ca.sub.62, with 0.ltoreq..beta..ltoreq.0.1 and 0.ltoreq..alpha..ltoreq.0.2, and X is Cl.sub.1-.gamma. Br.sub..gamma., with 0.ltoreq..gamma..ltoreq.1.
摘要翻译： 在光谱的蓝色区域发光的发光体具有下式：M5（1-α）Eu5α2+ SiO4X6，其中M表示Ba1-β4b或Ba1-βCa62，其中0≤β≤0.1和 0
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公开(公告)号：US4920744A
公开(公告)日：1990-05-01
申请号：US267458
申请日：1988-11-04
CPC分类号： B64D29/08
摘要： Inside a ducted fan turbine engine, especially one with a high or very high bypass dilution ratio, access to the gas generator compartment of the engine is effected by means of two articulated caps (34) with a C-shaped section. The upper edge of each cap (34) is connected to the fixed structure of the jet engine by means of a series of articulated arms (36) and a telescopic link (54) is inserted between the housing of the engine and the bottom of each cap. In a first stage (arrow F1), this mechanism enables the caps (34) to be brought beyond the rear edge of the outer ring (12) of the jet engine, the links (54) being locked in a compressed position. In a second stage, the caps (34) uncoupled from the ring (12) are able to pivot from the desired angle (arrow F2) around an axis (y-y') parallel to the axis (x-x') of the ducted fan turbine engine.
摘要翻译： 在管道风扇涡轮发动机内，特别是具有高或非常高的旁路稀释比的风机涡轮发动机内，通过具有C形截面的两个铰接盖（34）进入发动机的气体发生器舱。 每个盖（34）的上边缘通过一系列铰接臂（36）连接到喷气发动机的固定结构，并且伸缩连杆（54）插入在发动机的壳体和每个的底部 帽。 在第一阶段（箭头F1）中，该机构使得帽（34）能够超出喷气发动机的外圈（12）的后边缘，链节（54）被锁定在压缩位置。 在第二阶段中，与环（12）脱离联接的盖（34）能够围绕平行于所述轴（x-x'）的轴线（y-y'）从所需角度（箭头F2）枢转 风机涡轮发动机。
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