US2004202539A1PendingUtilityA1
Rotor disk
Priority: May 9, 2001Filed: May 4, 2002Published: Oct 14, 2004
Est. expiryMay 9, 2021(expired)· nominal 20-yr term from priority
F04D 29/666F04D 29/662F04D 29/281F04D 25/02F04D 29/284
34
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Claims
Abstract
An impeller ( 1 ), in particular a radial-flow fan or compressor impeller is proposed for an internal combustion engine. This impeller has an unequal number of full blades and split blades ( 4, 5 ) arranged at a different angular distance and in a different order. This further reduces the noise produced.
Claims
exact text as granted — not AI-modified1 . Impeller for a radial-flow fan or compressor impeller, comprising full blades and split blades different in number from the full blade, wherein the full blades and the split blades are arranged at a different angular distance and in a different order.
2 . Impeller as claimed in claim 1 , further comprising a coupling and a bearing integrated on a rear side of the impeller.
3 . Impeller as claimed in claim 2 , wherein the impeller is made of a material selected to minimize mass moment of inertia.
4 . Impeller as claimed in claim 3 , wherein balancing holes are arranged on the impeller to compensate for an imbalance in the fan wheel.
5 . Impeller as claimed in claim 4 , wherein the balancing holes are arranged on at least one of a cover plate and a base plate.
6 . Impeller as claimed in claim 1 , wherein the impeller is made of a material selected to minimize mass moment of inertia.
7 . Impeller as claimed in claim 1 , wherein balancing holes are arranged on the impeller to compensate for an imbalance in the fan wheel.
8 . Impeller as claimed in claim 7 , wherein the balancing holes are arranged on at least one of a cover plate and a base plate.Join the waitlist — get patent alerts
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