US2004235368A1PendingUtilityA1

Jet pump having unevenly spaced blades

Priority: Apr 14, 2003Filed: Jun 17, 2004Published: Nov 25, 2004
Est. expiryApr 14, 2023(expired)· nominal 20-yr term from priority
Inventors:Gaetan Lecours
B63H 11/08B63H 2011/081B63H 21/24
36
PatentIndex Score
0
Cited by
0
References
0
Claims

Abstract

The invention is directed to a thick stator vane that effects continuous acceleration of the water stream within the jet pump, a non-uniform spacing of stator vanes or impeller blades to reduce noise output of the jet pump during operation, and a coupling structure positioned between the impeller and engine that prevents transfer of axial thrust to the engine caused by jet pump failure.

Claims

exact text as granted — not AI-modified
What is claimed is:  
     
         1 . A stator for use in a jet pump having an impeller rotatably coupled with respect to the stator, comprising: 
 a central hub portion; and    a plurality of stator vanes extending outward from the central hub portion arranged with irregular spacing between adjacent vanes, such that at least one stator vane is spaced from an adjacent stator vane a different distance than that stator vane is spaced from its other adjacent stator vane.    
     
     
         2 . A watercraft comprising: 
 a) a hull;    b) an engine supported by the hull; and    c) a jet pump supported by the hull, the jet pump including an impeller, and the stator of  claim 1 .    
     
     
         3 . An impeller for use in a jet pump having a stator fixed with respect to the impeller, comprising: 
 a) a central hub portion operatively connectable to an engine to rotate the central hub portion; and    b) a plurality of impeller blades extending outward from the central hub portion arranged with irregular spacing between adjacent blades, such that at least one impeller blade is spaced from an adjacent impeller blade a different distance than that impeller blade is spaced its other adjacent impeller blade.    
     
     
         4 . A watercraft comprising: 
 a) a hull;    b) an engine supported by the hull; and    c) a jet pump supported by the hull, the jet pump including a stator, and the impeller of  claim 3 , wherein the central hub portion is operatively connected to the engine.    
     
     
         5 . A jet pump comprising: 
 a) an impeller having: 
 a central hub;  
 a plurality of impeller blades extending outward from the central hub portion arranged with irregular spacing between adjacent blades, such that at least one impeller blade is spaced from an adjacent impeller blade a different distance than that impeller blade is spaced its other adjacent impeller blade;  
   b) a stator, fixed with respect to the impeller, having: 
 a central hub portion; and  
 a plurality of impeller blades extending outward from the central hub portion arranged with irregular spacing between adjacent blades, such that at least one impeller blade is spaced from an adjacent impeller blade a different distance than that impeller blade is spaced its other adjacent impeller blade.  
   
     
     
         6 . A watercraft comprising: 
 a) a hull;    b) an engine supported by the hull;    c) the jet pump of  claim 5 , wherein the central hub portion of the impeller is operatively connected to the engine.

Join the waitlist — get patent alerts

Track US2004235368A1 — get alerts on status changes and closely related new filings.

We store only your email — no account needed. See our privacy policy.