Geared turbofan engine with targeted modular efficiency

A turbofan engine comprising;

• a fan section including a fan blade having a leading edge and hub to tip ratio of less than 0.34 and greater than 0.020 measured at the leading edge;
• a speed change mechanism with gear ratio greater than 2.6:1;
• a first compression section including a last blade trailing edge radial tip length that is greater than 67% of the radial tip length of a leading edge of a first stage of the first compression section;
• a second compression section including a last blade trailing edge radial tip length that is greater than 57% of a radial tip length of a leading edge of a first stage of the first compression section;
• and
• a turbine section including a fan drive turbine section and a second turbine section forward of the fan drive turbine section, wherein a mid-turbine frame is arranged between the fan drive turbine section and the second turbine section, the mid-turbine frame supporting a bearing system that supports rotation of at least one of the fan drive turbine and the second turbine section and includes a vane guiding core flow into the fan drive turbine section.