Freezing Point (Aviation Fuels)

ASTM D2386 IP 16 ISO 3013 DIN 51421 (obs) FREEZING POINT OF AVIATION FUELS
This test method covers the determination of the temperature below which solid hydrocarbon crystals may form in aviation turbine fuels and aviation gasoline.

MANUAL FREEZING POINT
Consisting of: tripod stand with clamp the jacketed sample tube into the Dewar flask at the level required from method; Dewar flask Ø75×280 mm. int. for cooling medium, with stainless steel support; jacketed sample tube Dewar Ø20×234 mm. int.; silicone stopper with hole for thermometer and supporting the brass moisture-proof collar (with silica gel and glass wool) through which the manual brass stirrer passes.

Semi-automatic Freezing Point
SEMI -AUTOMATIC FREEZING POINT
Base painted with anti-acid epoxidic products supporting Dewar flask Ø75×280 mm. int. for cooling medium, with stainless steel support; jacketed sample tube Dewar Ø20×234 mm. int.; cork stopper with two holes one for thermometer and one for supporting the brass moisture-proof collar (with silica gel and glass wool) through which the manual brass stirrer passes joined to a geared motor for automatic stirrer at 70 rpm. The base accommodate the stirrer switch.

Technical specifications:
– Power supply: 220V 50 Hz
– Dimensions: 26x35x115 cm
– Weight: 11 kg

SEMI -AUTOMATIC FREEZING POINT (2 POSITIONS)
2 places stand-alone with base painted with anti-acid epoxidic products supporting two Dewar flask Ø75×280 mm. int. for cooling medium, with stainless steel support, each with; jacketed sample tube Dewar Ø20×234 mm. int.; cork stopper with two holes one for thermometer and one for supporting the brass moisture-proof collar (with silica gel and glass wool) through which the manual brass stirrer passes joined to a geared motor for automatic stirrer at 70 rpm. The base accommodate two stirrer switch.

Technical specifications:
– Power supply: 220V 50 Hz
– Dimensions: 60x40x115 cm
– Weight: 38 kg

Semi-automatic Freezing Point (2 positions)