Air oil cooler airflow augmentation system

A gas turbine engine comprising:

• a fan, a compressor section, including a low pressure compressor section and a high pressure compressor section;
• a combustor;
• a turbine section including both a low pressure turbine and a high pressure turbine section, and said low pressure turbine section driving said low pressure compressor section;
• and
• a fan drive gear system provided such that said low pressure turbine further driving said fan, with said fan and said low pressure compressor being driven at different speeds;
• a lubricant system including a lubricant pump delivering lubricant to an outlet line that splits into at least a hot line and a cool line, said hot line being directed primarily to locations associated with the gas turbine engine that are not intended to receive cooler lubricant, and said cool line being directed to at least one component with an operating temperature lower than the locations associated with the gas turbine engine that are not intended to receive cooler lubricant;
• and
• an air/oil cooler wherein air is pulled across said air/oil cooler to cool lubricant in said cool line, wherein at least a portion of the lubricant in said cool line bypasses the air/oil cooler and is passed through a first fuel/oil cooler configured to cool the at least a portion of the lubricant using fuel leading to a combustion section of the associated gas turbine engine;
• an oil/oil cooler configured to cool lubricant from a generator with lubricant from the air/oil cooler;
• and
• a second fuel/oil cooler configured to cool another lubricant exhausted from the oil/oil cooler with the fuel leading to the combustion section.