Force dissipation seat pedestal

摘要: The present invention generally relates to a force dissipation seat pedestal that is particularly useful in aircraft design. includes two rear supports having multi-strip legs, front unibody and gussets located proximal the legs. One end of each leg pivotally secured pedestal. An other floor via hinged mount assembly. are designed maintain their shape during normal operation aircraft, but deform an emergency landing reduce forces transmitted occupant seat.