NAVY MIL-A-6848-1950 ACCELEROMETER AIRCRAFT《航行加速计》.pdf
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1、M I LIA- 68 48 21 AugWt.160 Superseding AN-A-29 ACCTj AIRCRAFT This specification was approved by the Departments of the Aw, the Navy, and the Air Force for use of procurement services of the respective Departments. 1. scope 1.1 m.0 This specification comm three-pointer type visual maximum indicatin
2、g accelerometers. 2 APPLICABLE SFECIFICATIONS, OTHER PUBLICATIONS, AND *DRAWINGS 2.3 The following publications, of the issue in effect on date o invitatj.on for bids, shall form a part of this specification ta the extent specified herein: I I 2.1.1 Specifications.- (28-15i QQ-P-Ub Plathgj Cadmium (
3、Electrodeposited) Metals; Qeneral Specification For Inspection of Military MIL-D-5028 Drawings and Data LiStSj Preparation of (For Engines. Accessories and Other Auxiliam .I AN-QQ-A-696 AN-Ir-1 Luminescent Material; Fluonecent AN-N-11 Nut; Instrument Mounting AN-S-126 Screw-Threads; Strndrrd Aircraf
4、t Anodic-Films 3 Corrosion-Protective (For) Alumi- num Alloys , U* S. Anri;y 94-40645 Marking; uterior, Domestic and Export Shipment, by contractow i Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-A-68118 bb 3779706 0325757 O Bureau of supp lies
5、 and Accounts Navy Shipent Marking Handbook 2.1.3 D18Wit* Air Force-Navy Aeronautical Standard Drawings AN5727 AN5745 Accelerometer - Aircraft . AND10400 AND10404 Olase - Aircraft Instrument. Cover Numerals and Letters - Aircrait Inetniment Pointers - Standard Design of AircraPt (Copies of this spec
6、ificstion and copies of other publicaticm referenced herein or muired for Oovemnt procurement, and the Index o$ MilitaW. Aeronautioal (AN or ?EL) Standarde, my be obtained upon application to the Commanding General, Air Pateriel caamuuid, Wright-Patterson Air Force Base, Dayton, Ohio; or the Command
7、ng Officer, U. S. Naval Air Station, Johnsville, Pennsylvania. ) Dial, Standard Fo Of nstrument 3.1 Materials.- . 3.1.1 Hetals.- Metae shall be of the corrosion-resisting type, wileas suitably proteated to recomosion durin one main pDinter for indicating instantaneous acceleration, and two auxiliam
8、pointers, one for indicating maKi- mum positiva acceleration, and one for indicating maximum negative acceleration pointers shall conform to figure 1. oscillation under vibration. readily adJustable. Th They shall be light and sufficiently rigid to pmvent They shall be firmly attached to the mechani
9、sm, yet shall be 3.3.6 Ratchet Mechanism.- Each auxiliary painter shall be provided with a ratchet device so that indication of the maximum plus and minus deflections of the main pointer vsilP be maintained until the auxiliary pointers are released to obtain a new reading. 3.3.7 auxiliary Pointer Re
10、turn Mechanism.- A mechanism shall be provided-for 18- leasing the auxiliaw pointers for return into juxtaposition with the main pointer. knob located as shown on Drawing AN5745 of the size and shape specified thereon, and made of molded plastic or low-density alloy metal, shall be provided for oper
11、ating the return mechanism. indicate a lower or higher reading than that indicated by the main pointer. Stops shall be a past of the mechanism connecting the pointers and shall not directly engage them. A Stops shall be provided so that the auxiliary pointers when released shall not 3.3.7.1 pointers
12、 when the imposed acceleration is less than the acceleration indicated by the auxiliary pointers . Stops for Acceleration-Responsive Element .- Mechanical stops shall be pro- vided for arresting the motion of the acceleration-responsive element when the inst-ent is subjected to accelerations beyond
13、the limits specified. One stop shall engage the ele- ment at an acceleration of not less than -5.1 g units and not more than -5.5 g units, and the other at an acceleration of not less than +12J g units and not more than +12.5 g units; The main pointer mechanism shall not engage the mechanism of the
14、auxiliary 3.3.8 .- 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-P MIL-A-6Y 66 7977906 0125762 O to proteci the mechanism of the instrument from pos
15、sible damage during shipment. vided. this device shall be controlled by mans of a screw located in the back of th% case. If pro- 1 3.3,10 Ad u6tment.- The mechanism shall be provided with means to adjust or cor- rect the pointer -4-T ndica ions if this becomes necessary during the service of the ins
16、tru- ment. This means of adjustment shall be reasonably simple to manipulate and of such nature I the adjustment can be accomplished with tools ordinarily possessed by an instrument repairman. thon and parformance. Changea in manufacturerts part nuhers shall be governed by the I drawing number requi
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