欢迎来到麦多课文档分享! | 帮助中心 海量文档,免费浏览,给你所需,享你所想!
麦多课文档分享
全部分类
  • 标准规范>
  • 教学课件>
  • 考试资料>
  • 办公文档>
  • 学术论文>
  • 行业资料>
  • 易语言源码>
  • ImageVerifierCode 换一换
    首页 麦多课文档分享 > 资源分类 > PDF文档下载
    分享到微信 分享到微博 分享到QQ空间

    NAVY MIL-I-81683 A-1979 INDICATOR ATTITUDE REFERENCE SELF-CONTAINED 3-INCH ID-1791 A《ID-1791 A型3英尺 自包含型姿态参考指示器》.pdf

    • 资源ID:980000       资源大小:2.72MB        全文页数:62页
    • 资源格式: PDF        下载积分:10000积分
    快捷下载 游客一键下载
    账号登录下载
    微信登录下载
    二维码
    微信扫一扫登录
    下载资源需要10000积分(如需开发票,请勿充值!)
    邮箱/手机:
    温馨提示:
    如需开发票,请勿充值!快捷下载时,用户名和密码都是您填写的邮箱或者手机号,方便查询和重复下载(系统自动生成)。
    如需开发票,请勿充值!如填写123,账号就是123,密码也是123。
    支付方式: 支付宝扫码支付    微信扫码支付   
    验证码:   换一换

    加入VIP,交流精品资源
     
    账号:
    密码:
    验证码:   换一换
      忘记密码?
        
    友情提示
    2、PDF文件下载后,可能会被浏览器默认打开,此种情况可以点击浏览器菜单,保存网页到桌面,就可以正常下载了。
    3、本站不支持迅雷下载,请使用电脑自带的IE浏览器,或者360浏览器、谷歌浏览器下载即可。
    4、本站资源下载后的文档和图纸-无水印,预览文档经过压缩,下载后原文更清晰。
    5、试题试卷类文档,如果标题没有明确说明有答案则都视为没有答案,请知晓。

    NAVY MIL-I-81683 A-1979 INDICATOR ATTITUDE REFERENCE SELF-CONTAINED 3-INCH ID-1791 A《ID-1791 A型3英尺 自包含型姿态参考指示器》.pdf

    1、a ?. MIL-I-81683A 66 W 9999906 0343585 b W j5=9/-)3 SCOPE 1. - MIL- 1-81 683R(AS) +i.3-.5.5.3 1: . .1 .i 9- 3.5.5.4 3.5.5.5 -. 3.5.6 . _. 3.5.6.1 - -* I *. .= . 5 . :. -1 . . ;: - .i -. I:. - . :-Damping Liquid- The -dampini. :iiqujd .shall be sufficiently . colorless under- all. specified condi.ti.

    2、ons to preclude interference .with visibi.l.ity. of. thebll. The viscosity shall be such that with the ball in motion at the zero mark, and the case tilted 12,-the time required for the ball to roll. from the zero mark to -the end of the tube shall be not.less than 0.5 second. . Sensitivity - The se

    3、nsitivity shall .be such that the ball reaches its limit of travel when the indicator is rotated right or left 10 5 2 about the roll axis. Inclinometer Filling - No part of the air bubble shall be visible when the indicator is viewed from the posi- tion specified in 3.5.5.2. Rate-of-Turn - The rate-

    4、of-turn display shall be in accordance with Figures 1 and 7. The design shall be such that the pointey is stable as practicable under rough air conditions and 1/29 vibration. normal operating position, the index shall move left or right in agreement with the polarity of the direct current received f

    5、rom the remote rate-of-turn sensor. The scale shall conform to the path of the index so that there is a minimum of parallax. to either side of the center zero position shall be limited to 1/2 inch. At each of the fully deflected positions, a minimum of one-half of the index shall be in view when vie

    6、wed at a horizontal distance of 2 feet from the center point of the display. Fixed mechanical stops shall be provided at the extreme deflection points to prevent pointer hangup on the case or mechanisms. Sensitivity Element - The sensitive element of the turn indicators shall be operated on 1 vdc (2

    7、 vdc maximum input) applied to pins 26 and 27. The element shall be so mounted that it reacts only to turns about the vertical axis. Within The index deflection 16 Licensed by Information Handling Services. MIL-I-Lb3A bb 7977906 OLLi3bOL O I 3.5.6.2 *3.5.6.3 c *3.5.6.4 Pointer - The pointer shall be

    8、 as shown on Figure 7. Scale - The turn rate scale shall conform to Figure 7. The colors shall be as specified in Table II. The distance between the indicator dial and the inside of the cover glass shall be held to a minimum and shall not exceed 1/4 inch at the zero position. TABLE I. Inclinometer T

    9、ube Color. Marking Col or Visible Part of Two Wires on Black No. 37038 Front and Top Inclinometer Wire on each side of Inclinometer Black No. 37038 Incl inometer Background . White No. 37875 Al 1 Other Background Black 140. 37038 TABLE II. Turn Rate Scale Color. Color Marking Center Mark White No. 3

    10、7875 Two Needle-width Deflection Marks White No. 37875 Pointer White No. 37875 Deflection (Pointer) - The deflection for a given input shall be as specified in the following table. The maximum voltage supplied to pins 26 and 27 shall be limited to 2 vdc. For left turns (cw deflection), the voltage p

    11、olarity shall be positive (+) on pin 26 and negative (-) on pin 27. the voltage polarity shall be negative (-) on pin 26 and positive (+) on pin 27. needle width minimum. For right turns (ccw deflection), Oyer travel shall be 1/2 17 Licensed by Information Handling ServicesMIL-I-Lb3A 66 7779706 OLLi

    12、3b02 2 .- .- 3.5.7 . .- i -“ - : :- *3.5.6.5 I . rate-of-turnindex shall be a maximum of .45 sec. Response Time f The response time (see 6.5.1) of the Flight Director Display - The flight director display shall consist of a vertical pointer and a horizontal . . .- I. - - : . .-. -. . . . j ., . . .(

    13、31) Pitch Trim Test :i . . . (73) Rotor Coast Time . . (1-4) Inclinometer:,Tests . -(15) Rate-of-Turn TesFS Tests .t. - (1 2) Poher Consumption .L . 3. . +. . . . - (16) Vertical Category 4, Upper Test MTBF O - 2000 hours Lower Test MTBF 1 - 1000 hours Test Plan - Fix length test plan 20-6, Appendix Cy page 115, Figure C-19 of MIL-STD-781 Environmental temperature extreme shall be +55C and -44C. *4.4.3.1 The fol lowing conditions apply: MI L-STD- 781 The vibration level shall be .5g. 30 . .I Licensed by Information Handling Services


    注意事项

    本文(NAVY MIL-I-81683 A-1979 INDICATOR ATTITUDE REFERENCE SELF-CONTAINED 3-INCH ID-1791 A《ID-1791 A型3英尺 自包含型姿态参考指示器》.pdf)为本站会员(ownview251)主动上传,麦多课文档分享仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文档分享(点击联系客服),我们立即给予删除!




    关于我们 - 网站声明 - 网站地图 - 资源地图 - 友情链接 - 网站客服 - 联系我们

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1 

    收起
    展开