Sentence examples for cooling method used from inspiring English sources

The cooling method used for the toroidal-type SMES is the conduction cooling type.

In order to improve the cooling and lubrication, through in-depth research of self-inhaling internal cooling method and intermittent grinding mechanism, a new spray cooling method used in high speed grinding is proposed.

These adverse events of surface cooling were not observed in the modern surface cooling method using hydrogel pads.

An extracorporeal cooling method using KTEK-3 (Kawasumi, Tokyo, Japan) has been used in post-cardiac arrest patients in Japan [ 49].

Kory et al. [ 25] published a fast cooling method, using a combination of core and surface cooling modalities without the use of a commercial device, which resulted in a cooling rate of 2.6°C/h.

Although overcooling, rebound hyperthermia, rewarming-related hypoglycemia and rewarming-related hypotension were significantly increased in the surface cooling group compared with the endovascular cooling group, these complications were not associated with the surface cooling method using hydrogel pads.

Since most of the cooling methods used involve forced circulation of the coolant, modification of properties of fluids which can result in an increased pumping power requirement could be critical.

Moreover, there are a number of physical cooling methods used to reduce body temperature, including undressing, sponging or toweling with tepid or cold water or alcohol, and these are involved in convection and evaporation but do not treat the underlying causes of the fever and the physical methods can cause discomfort [ 43, 44], such as shivering, hypoglycemia, coma and even death [ 4].

With the once-through-cooling method used at the AES plant, Poseidon will intake 100 million gallons of water per day, 365 days a year and return 50 million gallons per day of twice-salty effluent to the ocean off our coast.

The selected cooling methods use water to cool the module front side.

Traditional cooling methods using honeycomb-type radiators were known to cause high drag in flight; consequently it was decided to use the surface skins of the S.6 wings and floats as heat exchangers, employing a double-skinned structure through which the coolant could circulate.