@ reinforcing the gear
Sorry, but wont work.
The whole way an aircraft functions is by a combination of forces on the aircraft, these are thrust, lift, drag and weight. In cruise they balance out nicely so your aircraft stays in the air and maintains a nice and comfortable speed. On the ground, the thrust from the engines still produces lift on the wings and this lifts the aircraft slightly off the undercarriage thereby reducing the weight felt by the undercarriage.
Hence, by dragging the aircraft around the whole time without the engines running, you add a significant amount of weight that the undercarriage has to carry and which it hasn't been designed to carry whilst in movement. This leads to an increase in fatigue, and fatigue is what limits the life of aircraft.
At present, fatigue limits for your undercarriage are known based on huge amounts of simulations, calculations, stress data and fatigue testing of the aircraft/undercarriage systems (completed over years and years of testing), but the moment you start dragging them around this changes and where before you might have thought you only needed to check for cracks every 500 landings* you now have a crack forming and reaching critical length in under 500 landings, this means your undercarriage will fail, the aircraft will crash and people will be hurt/killed. This is generally considered a bad thing.
*figure pulled out of my ass for lack of desire to go searching for the exact figure
So whilst it may be an idea for future aircraft to be designed with undercarriage that are rated for this sort of activity it is impractical for in service aircraft.
Oh and before some one suggestions recalculating the fatigue limits - this is not an easy task, it takes years to do. The C130J Hercules fatigue test aircraft is STILL undergoing fatigue testing as we speak (24hr a day cycling for years on end) and how long has it been in service?