摘要 |
Described are seat support assemblies comprising at least one of a pitch reducer assembly, a fitting assembly, an energy absorption assembly, and an integrated leg assembly. The pitch reducer assembly may include a pitch reducer housing, at least one pitch riser, and at least one pitch stop. The integrated leg assembly may include a forward leg and an aft leg, where the forward leg is coupled to the pitch reducer assembly. The fitting assembly may include a pair of forward housing mating components and a pair of aft housing mating components, where the pairs of mating components are coupled to the forward and aft legs, respectively. The energy absorption assembly may include a tubular member, a die slidingly coupled to the tubular member, and a die holder coupled to the die, wherein the die holder has a hemispherical outer surface that is configured to pivotally mate with a passenger seat housing and rotate about an arc of rotation relative to the tubular member. |
申请人 |
WEBER AIRCRAFT LLC;TRIMBLE, ROBERT, W.;ISLAM, RAKIBUL |
发明人 |
TRIMBLE, ROBERT, W.;ISLAM, RAKIBUL |