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

Claim 18:
19. The aircraft of claim 16, further comprising a first seal (372), located at the first end (304, 704) of the sleeve (302), the first seal (372) configured to receive the third end (350, 748) of the spool (348, 702), wherein:
the first seal (372) comprises a first orifice (374) that receives the third end (350, 748) of the spool (348, 702);
the first orifice (374) has a first radius (376) that is equal to a third outer diameter (354) of the third end (350, 748); and
the first radius (376) of the first orifice (374) is smaller than the first outer diameter (360, 1200) of the first ridge (358, 752).