|
殼牌潤滑油系列 > 殼牌航空潤滑油 > AEROSHELL FLUID 3 |
AEROSHELL FLUID 3 詳細(xì)說明 (瀏覽1276次) |
AEROSHELL FLUID 3 AeroShell Fluid 3 is a general purpose mineral lubricating oil recommended for general lubrication of aircraft parts that require a light oil with good low temperature characteristics and a low freezing point. It is inhibited against oxidation and corrosion. AeroShell Fluid 3 is a relatively low viscosity product with good resistance to evaporation. APPLICATIONS AeroShell Fluid 3 is recommended for general lubrication of aircraft parts that require a light oil, e.g. hinges, pivot joints, shaft joints, linkage pins and bearings, pulleys, cables, camera mechanisms, radio and radar gear and instruments. AeroShell Fluid 3 is normally applied by means of an oil can or brush. For this reason it is also described as ‘a(chǎn)n oilcan lubricant’. Operating temperature range of AeroShell Fluid 3 is -54°C to +121°C. For high temperature applications where no provision is made for frequent re-lubrication the synthetic oil, AeroShell Fluid 12, should be used in place of the mineral oil, AeroShell Fluid 3; however in this case care should be taken to ensure that there is no incompatibility between AeroShell Fluid 12 and seals, paints etc. SPECIFICATIONS U.S. Approved MIL-PRF-7870C British Approved DEF STAN 91-47 French – Russian – NATO Code O-142 Joint Service Designation OM-12 www.shell.com/aviation 230 Other Fluids PROPERTIES MIL-PRF-7870C TYPICAL Oil type – Mineral Kinematic viscosity mm 2 /s @ 38°C 10 min 10.0 @ ?40°C 4000 max Less than 4000 Flashpoint Cleveland Open Cup °C 130 min 155 Pourpoint °C ?57 max Below ?57 Evaporation @ 99°C, 22hrs %m 25 max 13 Total acid number mgKOH/g – 0.3 Relative Density @ 15.6/15.6°C – 0.89 Low temperature stability 72 hrs @ ?54°C Must pass Passes Oxidation & corrosion stability 168 hrs @ 121°C – metal weight change Must pass Passes – viscosity change % ?5 to +20 10 – acid number change mgKOH/g 0.2 max 0.02 Corrosivity Must pass Passes ASTM colour – < 0.5 A viscosity/temperature curve is shown at the end of this section. |
|
|