In　this　paper,　a　nonisothermal　analysis　for　the　process　of　blade　coating　of　an　incompressible　couple　stress　fluid　is　presented　using　both　plane　and　exponential　coaters.　The　governing　system　is　simplified　using　lubrication　approximation　theory　(LAT).　The　interesting　quantities　from　engineering　point　of　view　like　normalized　pressure,　maximum　pressure,　pressure　gradient,　velocity,　and　effects　of　involved　parameters　on　temperature　distribution,　which　influence　the　coating　process　are　evaluated.　It　is　observed　that　pressure　is　at　maximum　near　the　edge　of　the　blade　whereas　fluid　velocity　and　temperature　are　at　maximum　near　the　substrate.　An　increasing　couple　stress　parameter　increases　the　load　and　decreases　the　coating　thickness.　It　is　worth　mentioning　that　load　and　pressure　are　the　most　significant　outcomes　of　the　present　exertion　as　these　two　physical　quantities　ensure　thickness　and　the　quality　of　coating.