US2024068704A1PendingUtilityA1

Airfoil blade and method of assembly

75
Assignee: MESTEK INCPriority: Jan 23, 2015Filed: Nov 9, 2023Published: Feb 29, 2024
Est. expiryJan 23, 2035(~8.5 yrs left)· nominal 20-yr term from priority
F24F 13/15F24F 13/14F24F 13/1406F24F 13/1426
75
PatentIndex Score
0
Cited by
0
References
0
Claims

Abstract

An airfoil blade assembly includes an upper airfoil shell, and a lower airfoil shell and a pair of upper legs protruding from the upper airfoil shell and extending towards the lower airfoil shell. A pair of lower legs protrudes from the lower airfoil shell and extending towards the upper airfoil shell and are formed by bending material of the lower airfoil shell back upon itself. An upper strengthening rib formed is in the upper airfoil shell, and a lower strengthening rib is formed in the lower airfoil shell. The pair of upper legs and the pair of lower legs are abutting when the upper airfoil shell and the lower airfoil shell are selectively fixed to one another.

Claims

exact text as granted — not AI-modified
What is claimed is: 
     
         1 . An airfoil blade assembly, comprising:
 an upper airfoil shell;   a lower airfoil shell, one of said upper airfoil shell and said lower airfoil shell defining a lateral seam;   an elastic bead positioned within said lateral seam; and   wherein said elastic bead extends beyond a periphery of said lateral seam when said upper airfoil shell is fixed to said lower airfoil shell.

Cited by (0)

No later patents cite this yet.

References (0)

No backward citations on record.