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

    DLA MIL-J-26149 E-1988 JACK HYDRAULIC AIRCRAFT MAINTENANCE GENERAL SPECIFICATION FOR《飞行器维护液压支撑物的常规》.pdf

    • 资源ID:691452       资源大小:1.16MB        全文页数:29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。

    DLA MIL-J-26149 E-1988 JACK HYDRAULIC AIRCRAFT MAINTENANCE GENERAL SPECIFICATION FOR《飞行器维护液压支撑物的常规》.pdf

    1、I NCH-POUND I MI L-J-261 49E 30 December 1988 SUPERSEDING MI L-J-261 49D 12 June 1987 (See 6.6) * MILITARY SPECIfICATION GENERAL SPECIFICATION FOR JACK, HYDRAULIC, AIRCRAFT MAINTENANCE, This specification is approved for use by all Departments and Agencies of the Department of Defense. 1 . SCOPE 1.1

    2、 Scope. This specification covers the general requirements for weapon systems hydraulic jacks as used with all types of military aircraft. - t I r ! L E f i. 1.2 Classification. All aircraft jacks shall be classified as to their design or use. These classifications shall be.in accordance with Table

    3、I. TABLE 1. Classification of Aircraft Jacks. CLASSIFICATION CHARACTERISTIC OF REFERENCE OF JACKS JACK DESIGN LANDING GEAR HAND CARRI ED- MS26566 (AXLE) DOLLY MOUNTED CANTILEVER AIRFRAME FIXED HEIGHT MS33589 (UNIPOD quantity; warning symbol; signal word designating degree of hazard; affirmative stat

    4、ement of hazards; precautionary measures covering actions to be followed or avoided; instructions in case of contact or exposure; antidotes and notes to physic.ians; instructions in case of fire, spill, or leak; instructions for handling and storage; and disposal instructions. Characteristics and op

    5、erating-hazards which require labeling include: toxic, high toxic, irritant, corrosive, strong sensitizer, combustible liquid, flammable, extremely flammable liquid, dangerously reactive, pressure- generation, explosive, magnetic, ionizing radiation, non-ionizing radiation; high voltage, implosion,-

    6、 noise, and etiologic agent. Marking of hazardous materials shall be in conformance .with establ i shed and approved procedures. 3.5.1.3 Recycled, virgin and reclaimed materials. When the intended use of the aircraft jack(s) will be jeopardized by the use of reclaimed or recycled materials these mat

    7、erials shall not be used. However, the following shal-1 apply: 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-J-261 49E MIL-J-26L49E L7 9 7779706 OL938B7 B 9 a. There is no exclusion to the use of recovered materials. b. There is no requiremen

    8、t that an i tem be manufactured from virgin materi al s. c. Within 1 year from the date of issue by the environmental protection agency of guidelines designating items which are or can be produced with recovered materials, specifications for such products require the use of recovered materials to th

    9、e maximum extent possible. 3.5.2 Metals. Metals shall be corrosion resistant or treated to resist corrosion due to fuels, salt fog, or atmospheric conditions likely to be encountered in.strage or normal service. Stock used in the fabrication of jacks shall have a properly refined structure with unif

    10、orm elemental distribution, sound and free from nonmetallic inclusions, injurious porosity, excess segregation, and soft or hard spots. Castings shall be of uniform quality, free from blowholes, excess porosity, and soft or hard spots. All castings shall be subjected to a seasoning or aging process,

    11、 either natural or artificial, to insure maximum stabi 1 i ty. 3.5.2.1 Dissimilar metals. Unless specifically protected against electrolytic corrosion, dissimilar metals shall not be used in intimate contact with each other. Dissimilar metals are defined in and s.hall be used in accordance wi th MIL

    12、-STD-889. 3.5.2.2 Standard steel. Suitable steel complying with ASTM or AIS1 standards shall be uti 1 ized in the manufacture of the jack 3.5.2.3 Welding material. All welding of the jack shall be in accordance with the structural welding code for steel, Dl.1-86, as issued by the American Welding So

    13、ciety (AWS) and welding aluminum shall be in accordance with 01.2-83. 3.5.2.4 Brazing. All brazing shall be accomplished in accordance with the Brazing Manual 1976 issued by the American Welding Society. 3.6 Design and construction. The jack shall be axle, cantilever, unipod or tripod, designed for

    14、the load capacity required. The aircraft configuration which will effect the jack installation and operation shall be considered in the design of all jacks. The jack shall be designed and constructed so that all parts are made for assembly without interference and no parts will work loose in service

    15、. The jack shall be designed and constructed to withstand the strains, jars, vibration, and other.conditions incident to shipping, storage, installation and service. MS26566 or MS33589 *shall be used as design guides. 3.6.1 Component arrangement. Al 1 components shall be arranged for maximum ease of

    16、 operation and maintenance consistent with the utility and efficiency required to conform to the requirements specified herein. 7 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-J-26347E L7 m 777770b 0373888 T m MIL-J-26149E 3.6.1.1 Component sel

    17、ection. All components shal proper clearances and adjustments. They shall so work will supply the rated capacity. 1 be new and shall have together that the jack 3,6.1.2 Component maintenance. All components shall be selected on the basis of maximum life cycle with a minimum of maintenance. Selection

    18、 shall be made primarily from approved standard parts using the best engineering practices. Whenever possible extended life parts shall be utilized. As required by the contract the parts control program shall be in accordance with MIL-STD-965. 3.6.2 Reliability. (MTBF) of not less than for a 1-cycle

    19、 mission at The jack shall have a-mean-time-between-failures 0.9 confidence (see 6.7.4). 108 cycles with a reliability of not less than 0.9908 3.6.3 Maintainability. The jack shall be designed and constructed as specified herein and to provide the following: a. Minimum number of parts consistent wit

    20、h reliability and performance specified herein. b. Minimum amount of training and time necessary for assembly, disassembly, location of trouble sources, and maintenance including servicing. Where practical, parts and components shall be located or positioned for rapid and simple inspection and recog

    21、nition of excessivewear or potential failure. c. Permit adjustments, servicing, replacement of parts and components, and other maintenance with minimum disturbance to other equipment parts or components. Parts and components shall be located for ample and rapid access unless performance .or re1 iabi

    22、lity will be appreciably degraded by the accessible -location. In performing maintenance, if engineering reasoning or data determines that physical or visual interference between items cannot be avoided, the i tem predicted to require the most maintenance shall be located for best accessi bi 1 i ty

    23、and ease of maintenance. d. Permit maintenance with general purpose tools and equipment normally available commercially. Use of special purpose tools and equipment shall be subject to .approval by the procuring activity. e. Minimum number of tools required for maintenance by design practices such as

    24、 reducing the variety of bolt head sizes- to the practicable -minimum; 8 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-J-26247E 27 W 7777706 0273887 L W MIL-J-26149E f. Foolproofness - Where improper installation of an item could cause malfunct

    25、ion of the item or the equipment in which it is installed, an unsymmetrical mounting means shall be provided where practical. That mounting shall allow the item to be installed only in its proper operating position. If an unsymmetrical mounting means is not practical, the item shall be so mounted th

    26、at its proper operating position can be readily and visibly determined by service maintenance personnel. g. Repair kits and soft kits shall be desig-ned and developed to extend the life of the jack assembly by repairing or replacing those piece parts that are subject to wear during normal use. 3.6.4

    27、 Capacity and type. The rated capacity shall be specified in U.S. tons ( kg.). The type of jack shall be specified as axle, .cantilever, unipod or tripod (see 1.2 and 6.2). 3.6.5 Floor loading. The jack base or foot pads shall be of such proportions, relative to floor contact area, as to prevent flo

    28、or loading in excess of 400 psi (2758 kPa) when supporting a rated capacity load. However, in those circumstances where tight clearances or special aecomodations are necessary, the floor loading may not exceed 600 psi- (4137 kPa). Floor loadings *in excess of 400 PS1 (2758KPA) will require approval

    29、of the responsible procuring activity. 3.6.6 Mobility. Jacks having a gross weight in excess of 120 pounds (54.4 kg.) shall be provided with type I, class lb mobility in accordance with MIL-STD-1784 except that the slope requirement shall be a maximum of 15“. 3.6.6.1 Casters or wheels. Unless otherw

    30、ise specified by the procuring activity, al 1 casters shall be furni shed in accordance with requirements of MS24380. Casters on tripod or axle jacks may be spring loaded for ease of placement. 3.6.6.2 Towbar. A towbar meeting the requirements for type I, class 2 of MIL-STD-1784 shall be provided. W

    31、hen specified, provisionsshall be made to secure the towbar to the jack structure when not in use. 3.6.6.3 Carrying handles. All hand carried jacks shall have carrying handle(s. The design of the carrying handles shall favor the user. Handles shall be ruggedized and located in relationship to the ce

    32、nter of gravity (cg) such that the jack is easily controlled while it is being moved about. Also, if possible, the carry,ing handles may be used to protect the controls while the jack is in operation. A jack having a gross weight not to exceed 60 lbs. (27.2 Kg) shall require only one handle. For a j

    33、ack weighing between 61 lbs. (27.7 Kg) to 120 lbs. (54.4 Kg), two handles shall be required. Any jack exceeding 120 lbs. shall meet the mobility requirements stated herein. 3.6.7 Heat treatment. Heat treatment of steel materials shall be- in accordance with MIL-H-6875. 9 Provided by IHSNot for Resal

    34、eNo reproduction or networking permitted without license from IHS-,-,-MIL-J-261 49E 3.6.8 Structural design. The jack ram and cylinder shall be designed to include a factor of safety of 1.75 based on the rated capacity of the jack. The remainder of the jack supporting structure .shall be designed fo

    35、r a factor of safety of 2.0 based on the rated capacity of the jack (see 6.7.8). 3.7 Performance. The jack shall operate under the following conditions: . An internal pressure equal to 1-112 times the pressure at rated capacity without leakage. b. Maximum settling of 0.020 inch (0.51 mm) per ram per

    36、 hour under rated capacity load. c, . Rai sing verti cal ly 150 percent of the rated capacity load. d. Withstanding a horizontal load equa1,to 15 percent of rated capacity while supporting a rated capacity loadwi th the ram fully extended and the screw extension retracted. e. Operating at all temper

    37、atures ranging from -65F to t130“F (-53.9“C to 54.4“C). f. Two hundred cycles of raising a rated capacity load and sixty cycles of rai sing a rated capacity load- while being fubjected to a horizontal load of 15 percent of rated capacity. g. Dust particles as encountered in desert areas. h. Exposure

    38、 to salt fog or salt laden atmosphere. j. Operating in rain, snow, or bright sunlight. l. Interface properly and securely with the aircraft jack points. m. The hydraulic fluid system shall have overload protection capabi 1 i ti es. 3.8 Hydraulic system. The hydraulic system (figure 1) shall be desig

    39、ned for operation with hydraulic fluid conforming to MIL-H-5606, MIL-H-83282, or MIL-H-81019 and shall consist of a jack ram and cylinder, pump, necessary bypass and check valves, reservoir, tubing, hose and fittings. The hydraulic system sha-11 be provided with a device designed and located to blee

    40、d all entrapped air from the system. The jack shall be equipped with a self- contained, hand operated, hydraulic pumping system and shall also have provisions for connection to an external hydraulic pumping source when specified. Hydraulic hose shall conform to MS28759 and the hose shall have a fema

    41、le connector 43A13905 which will mate with the connector on the jack. The external leakage of the system shall not exceed 0.05 cc per hour at any pressure. For design purposes the optimum hydraulic pressure shall be 3000 psi *(20,684 kPa) at the rated capacity. 10 Provided by IHSNot for ResaleNo rep

    42、roduction or networking permitted without license from IHS-,-,-i MIL-J-26149E ; PUMP. ASSEMBLY .SPRING LOADED CHECK VALVE PUMP (ONE OR MORE) SAFETY BY-PASS PUMP ASSEMBLY CHECK VALV RE LEAS E VALVE SUCTION I 1 HYDRAULIC FLU ID RESERVO1 R i 1: I , long and shall be provided with a suitable grasp (knur

    43、led) surface. For jacks of less than 10 tons (9070KG) capacity a shorter handle may be provided ie 18“ (0.456M) or 20“ (0.51M). Provisions *shall be made to stow the pump handle on-the jack. The pump inlet shall be provided with a screen-of approximately 50-mesh, 0.007-inch (0.18 mm) diameter brass

    44、wire. The internal leakage of the pump shall not exceed 5.0 cc per hour. * 3.8.2 Safety Bypa?s valve. The jack shall .be equipped with a bypass valve adjusted and set to 105 to 110 percent of the rated capacity of the jack. This valve shall be-located between the pump check valve and the jack ram to

    45、 prevent overload and shall vent into the reservoir. 3.8.3 Safety device. The tripod jack ram(s shall be provided with a hydraulic pressure removed. The safety device shall prevent dropping the load during and after the jacking operation in the event,the hydraulic system fai 1s. The safety devi ce s

    46、hall be in operation at al 1 times when the jack ram is raised and supporting the load. . mechanical safety device capable of supporting the rated load with the 3.8.4 Reservoir. The hydraulic fluid reservoir shall have a capacity sufficient to fully extend the jack ram plus a 10-percent minimum rese

    47、rve. air relief valve and filler plug in accordance- with Drawing 1128AS121 shal provided on top of the reservoir (not shown in Figure 1). _. An 1 be * 3.8.4.1 Reservoir Dumping or safety valve. The dumping or safety valve (not shown in Figure No. 1) shall be located on or near the top of the reserv

    48、oir. This valve shall automatically vent excess air from the reservoir when this air is being replaced by hydraulic fluid. This valve shall be sized to accomodate the maximum flow of hydraulic fluid that may pass through the release valve. Also when relatively small-sized jacks are tipped or overtur

    49、ned this valve may not leak hydraulic fluid. * 3.8.4,2 Reservoir overflow vent valve. Those hydraulic jack systems that include a connection for an external pumping source connector shall also include an overflow vent valve located at the top of the reservoir (not shown in Figur.e No. 11 This vent shall relieve excess fluid that may be inadvertently transferred from the external pumping source. The vent valve shall open at about 100 psig pressure to prevent any damage to the


    注意事项

    本文(DLA MIL-J-26149 E-1988 JACK HYDRAULIC AIRCRAFT MAINTENANCE GENERAL SPECIFICATION FOR《飞行器维护液压支撑物的常规》.pdf)为本站会员(sofeeling205)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