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Improvements relating to rate of climb indicators for aircraft and like rate of change of fluid pressure responsive instruments

机译:与飞机爬升率指标以及类似流体压力响应仪器的变化率有关的改进

摘要

507,990. Pressure gauges. BENDIX AVIATION CORPORATION. Sept. 17, 1937, No. 25327. Convention date, Sept. 17, 1936. [Class 106 (ii)] A rate of climb indicator for aircraft comprises a pressure iespoiisive element operating through mechanism to indicate a pressure differential on opposite sides of the element due to rate of change of altitude as a result of the retarded rate at which the pressures on opposite sides of the element tend to equalize through restricted flow communication between the fluids on opposite sides of the element, characterized in that the restricted communication is constituted by a diffuser of a porous nature so chosen that the rate of pressure equalization is independent of the altitude. Two intercommunicating aneroid capsules 6 communicate by a pipe 9 with a vessel 10 and are connected by a link 7 and quadrant and pinion 4, 3 to a needle 1. The walls 11 of the chamber 10 are made of porous material. If the pressure on the outside of the chamber formed by vessels 10, 6 decreases due to ascent into higher altitudes, the vessels 6 expand and move the pointer to the left. If the instrument descends the pointer moves to the right. In another form of diffuser the walls are made of concentric tubes, each two adjacent walls at one end being connected together and the two adjacent pairs are connected together at the other end. Another form comprises capsule-like members made of porous material in communication at the central portions to form a closed chamber. Fig. 4 shows a form in which the diffuser is formed by a number of thin washers 22 preferably of metal clamped tightly between upper and lower clamping members 23, 24 by a bolt 25 and nuts 26. The member 23 has an extension 27 provided with parallel grooves 28 to permit passage of air from the stack of washers to the chamber 29 and thence through tube 30 to the pressure responsive element. The surfaces of the washers are etched or corrugated to give the desired porosity, and they may be of such material as to provide a bimetallic temperature control as described in Specification 508,059. The bolt 25 may be of copper and thus cause pressure to decrease as temperature increases. In a modification of this form a spacing member of selected material is used which coacts with the bolt to give the necessary compensation. Fig. 7 shows a rate of climb indicator. A case 37 is closed at one end by a plate 38 and at the other by a glass 39. A standard 41 secured to the base supports a post 42 to which the capsules 44 are connected by a resilient arm 43, a screw 58 affording zero adjustment. The capsules are connected to a pivoted lever 52 by a bimetallic strip 50 the lever operating a pointer 56 by means of a chain 54. The capsules are connected by a pipe 62 to a closed vessel 60 the walls of which are of porous material. The casing is vented to outside atmosphere through a suitable dehumidifying medium 64 such as silica gell and holes 68. The Specification as open to inspection under Sect. 91 comprises also a form in which a pointer shaft is journalled in a stationary block to which one end of a spiral metal strip is connected. The other end engages the pointer. The strip is faced with porous material or is of such a cross-section that a space is left between the strip and the porous facing to form a chamber. This strip behaves after the manner of a Bourdon tube, straightening out when the pressure in the porous material is greater than outside. This subjectmatter does not appear in the Specification as accepted. Reference has been directed by the Comptroller to Specification 141,244, [Class 106 (ii)]
机译:507,990。压力表。本迪克斯航空公司。 1937年9月17日,第25327号。会议日期,1936年9月17日。[等级106(ii)]飞机爬升率指示器包括通过机构运行的压力隐含元件,以指示在飞机相对两侧的压差。由于高度变化率而导致的元件受阻速率的降低,在该速率下,元件相对两侧的压力趋于通过元件相对两侧的流体之间的受限流动连通而趋于平衡,其特征在于,受限连通为由具有多孔性质的扩散器构成,因此选择的压力均衡率与海拔高度无关。两个相互连通的无液胶囊6通过导管9与容器10连通,并通过连接件7和象限和小齿轮4、3连接到针头1。腔室10的壁11由多孔材料制成。如果由容器10、6形成的腔室外部的压力由于上升到更高的高度而减小,则容器6膨胀并使指针向左移动。如果仪器下降,指针将向右移动。在扩散器的另一种形式中,壁由同心管制成,在一端的每两个相邻壁连接在一起,而在另一端的两对相邻壁连接在一起。另一种形式包括由多孔材料制成的胶囊状构件,该胶囊状构件在中央部分处连通以形成封闭室。图4示出了一种形式,其中,扩散器由多个薄垫圈22形成,该薄垫圈优选地由金属制成,该薄垫圈22通过螺栓25和螺母26紧密地夹持在上下夹持构件23、24之间。构件23具有延伸部27,该延伸部27设置有平行的凹槽28允许空气从垫圈堆流到腔室29,并由此通过管子30到达压力响应元件。垫圈的表面被蚀刻或形成波纹状以提供所需的孔隙度,并且垫圈的材料可以提供规范508,059中所述的双金属温度控制。螺栓25可以是铜的,因此导致压力随着温度升高而降低。在这种形式的变型中,使用选定材料的间隔构件,该间隔构件与螺栓共同作用以提供必要的补偿。图7示出了爬升率指示器。壳体37的一端通过板38封闭,而另一端通过玻璃39封闭。固定在基座上的标准件41支撑柱42,通过弹性臂43将胶囊44连接至柱42,螺钉58提供零值。调整。胶囊通过双金属条50连接到枢转的杠杆52,杠杆通过链条54操作指针56。胶囊通过管62连接到封闭的容器60,该容器的壁是多孔材料。外壳通过合适的除湿介质64(例如硅胶)和孔68排放到外部大气中。图91还包括一种形式,其中指针轴被固定在固定块中,螺旋金属带的一端连接到该固定块。另一端与指针啮合。条带面对多孔材料或具有这样的横截面,使得条带与多孔表面之间留有空间以形成腔室。该条带按照波登管的方式工作,当多孔材料中的压力大于外部压力时,其拉直。该主题未在接受的规范中出现。主计长已指导参考规范141,244,[106(ii)类]

著录项

  • 公开/公告号GB507990A

    专利类型

  • 公开/公告日1939-06-19

    原文格式PDF

  • 申请/专利权人 BENDIX AVIATION CORPORATION;

    申请/专利号GB19370025327

  • 发明设计人

    申请日1937-09-17

  • 分类号G01L7/10;G01P3/62;

  • 国家 GB

  • 入库时间 2022-08-24 04:59:24

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