IP Library Granted Patent US 7,165,515
Granted Patent B2
US 7,165,515 · App. 10/929,996 · Granted Jan 23, 2007

Engine cooling fan shroud

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Quick Facts
Patent No.
US 7,165,515
App. No.
10/929,996
Granted
Jan 23, 2007
Kind
B2
Abstract

A fan ( 16 ) draws air through a core ( 14 ) of a radiator ( 10 ) to which coolant from coolant passages in an engine ( 12 ) rejects heat. A shroud ( 28 ) having first and second parts ( 30, 32 ) in axial succession channels air that has been drawn through the core toward the fan. The first part ( 30 ) is a non-elastomeric ring, and the second part ( 32 ) has an elastomeric ring ( 34 ) having opposite axial ends, one of which telescopically fits to the non-elastomeric ring of the first part ( 30 ) and the other of which joins with a second non-elastomeric ring ( 36 ).

Claims (8)

1. An engine comprising:

engine structure that defines combustion chambers in which fuel is combusted to run the engine and coolant passages through which coolant is circulated to absorb some of the heat of combustion;

a fan that draws air through a core of a radiator to which coolant from the coolant passages in the engine structure rejects heat; and

a shroud for channeling air that has been drawn through the core toward the fan and that comprises a part comprising a non-elastomeric ring and an elastomeric ring joined to each other through a bond of elastomeric material of the elastomeric ring with non-elastomeric material of the non-elastomeric ring.

2. An engine as set forth in claim 1 wherein the non-elastomeric ring comprises a synthetic material having first and second zones, the first zone defining the open area through the part and the second axial zone comprising a radial flange that provides for attachment of the part to a further part that is itself attached to the engine structure, and the axial thickness of the radial flange sets the axial distance of the first zone from the further part.

3. An engine as set forth in claim 2 wherein the fan comprises blades having tips, and the axial thickness of the radial flange sets the axial distance of the first zone from the further part to place the first zone in axial registration with the fan blade tips.

4. An engine as set forth in claim 3 wherein the shroud further comprises a further part comprising a non-elastomeric ring that is attached to the radiator and with which the elastomeric ring has a sealed telescopic fit.

5. An engine as set forth in claim 1 wherein the shroud comprises a further part that is attached to the radiator and that comprises a non-elastomeric ring, and the elastomeric ring telescopes over the non-elastomeric ring of the further part.

Assignments (3)
RELEASE OF SECURITY INTEREST Recorded Nov 10, 2017
From: JPMORGAN CHASE BANK, N.A., AS COLLATERAL AGENT
To: INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC; INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC; NAVISTAR, INC.; NAVISTAR INTERNATIONAL CORPORATION
Reel/Frame 044416/0867 →
SECURITY AGREEMENT Recorded Sep 12, 2012
From: INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC; INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC; NAVISTAR INTERNATIONAL CORPORATION; NAVISTAR, INC.
To: JPMORGAN CHASE BANK, N.A., AS COLLATERAL AGENT
Reel/Frame 028944/0730 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 5, 2004
From: JACQUAY, BRIAN J.
To: INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC
Reel/Frame 015346/0750 →