Patent ID: 11927271
Assignee: THE BOEING COMPANY
Field: Transport (Mechanical engineering)
Classification: CPC B  F | IPC B  F

Claim 7:
8. The spool-sleeve assembly (300) of claim 7, further comprising a second seal (384, 1828), located at the second end (306, 706) of the sleeve (302) and configured to receive the fourth end (352, 750) of the spool (348, 702),
wherein:
the second seal (384, 1828) comprises a second orifice (386) that receives the fourth end (352, 750) of the spool (348, 702),
the second orifice (386) has a second radius (388), which is equal to a fourth outer diameter (356, 1210) of the fourth end (352, 750),
the second radius (388) of the second orifice (386) is also smaller than the third inner radius (342) of the second ridge (364, 754),
the second seal (384, 1828) further comprises a second retainer (390, 618), located opposite the second orifice (386) and sized and dimensioned to retain the fourth end (352, 750) of the spool (348, 702), and
the second seal (384, 1828) further comprises a second interior seal (392), having a second interior seal radius (394), which is equal to the fourth outer diameter (356, 1210) of the fourth end (352, 750) of the spool (348, 702).