rambharath94 said:
We first came up with a Floater design that would keep the recorders above the water surface ( I assume the crash happens above the oceans...most of the times they are ) but then that became absurd as that would carry it away from the crash site !
And then we came up with this..The blackbox be provided with a GPS ( in the existing design ).
We also thought about an idea of black box fitted with impact sensors ! which will send all the data which it has recorded to the ground station immaediately after impact ! But that would make it complicated !and Its not our field , so we were afraid to pursue/reject that idea !
regarding #2 ... Its an idea of reducing the accidents that occur due to the small length of the runways ! ( Many small airports suffer from these )
#5... Its is an idea of effectively using the KERS to recover energy from aircraft and to use it during taxiing
Thanks
In order for the black boxes to float, they would need to separate from the aircraft - even after the aircraft has been severely crumpled. Also, the float mechanism would need to inflate even after being subjected to very high G forces and high temperatures. And there should be essentially no chance of the black box separating from the aircraft or the floatation mechanism inflating except during a crash.
I think you'll find that airports with very short runways, like Washington Reagan, have pretty good safety records. This is because pilots recognize the runway as a problem and make their approach and departure plans accordingly. Factors include:
* Aircraft type, gross weight
* Atmospheric conditions - temp, pressure, humidity, wind speed and direction
* Runway conditions - direction, take off location, obstacles, type of surface, inclination
* Aircraft configuration - flaps, etc.
There are apps to assist pilots with these calculations - for both takeoff and landings.
KERS: Of course, you will be absorbing energy from the braking system and restoring it to the propeller or jet engines - and doing it without adding a lot of weight to the aircraft.