U.S. patent number 3,800,866 [Application Number 05/327,140] was granted by the patent office on 1974-04-02 for radiator assembly.
This patent grant is currently assigned to Stewart-Warner Corporation. Invention is credited to Robert G. Ireland, Vernon N. Tramontini.
United States Patent |
3,800,866 |
Ireland , et al. |
April 2, 1974 |
RADIATOR ASSEMBLY
Abstract
A static annular radiator having fluid passageway means and
radial air passageway means. Fluid inlet and outlet means are
provided for the fluid passageway means. Air propelling means are
located coaxially of the annular radiator for effecting air flow
radially through the air passageway means.
Inventors: |
Ireland; Robert G.
(Indianapolis, IN), Tramontini; Vernon N. (Indianapolis,
IN) |
Assignee: |
Stewart-Warner Corporation
(Chicago, IL)
|
Family
ID: |
23275317 |
Appl.
No.: |
05/327,140 |
Filed: |
January 26, 1973 |
Current U.S.
Class: |
165/122; 165/51;
165/125; 415/220; 165/DIG.304 |
Current CPC
Class: |
F28D
1/0358 (20130101); F28D 1/0471 (20130101); Y10S
165/304 (20130101) |
Current International
Class: |
F28D
1/02 (20060101); F28D 1/04 (20060101); F28D
1/03 (20060101); F28D 1/047 (20060101); F24h
003/10 () |
Field of
Search: |
;165/122-126,57 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Myhre; Charles J.
Assistant Examiner: Streule, Jr.; Theophil W.
Attorney, Agent or Firm: Douvas; Augustus G. Lesser;
Norton
Claims
The invention claimed is:
1. An annular radiator assembly for use in cooling different types
of vehicle fluids with one of said fluids being the coolant of an
engine supported on a vehicle frame and another of said fluids
being primarily an oil fluid, a pair of tanks in diametrically
opposite positions with each tank having a pair of radially spaced
axially extending walls, each tank having axially spaced radial
walls between the respective pair of said radially spaced walls to
define a plurality of sections for each tank with each section in
each tank corresponding to a respective one of said fluids, a
series of axially spaced side bars for each tank section extending
between the respective pair of radially spaced walls, a plurality
of pairs of semicircular cores connected to each tank section
between the respective side bars for communicating fluid between
the corresponding sections of said diametrically opposite tanks
with the space between said cores defining radially extending air
passageways, means for communicating said fluids to and from
selected corresponding tank sections, a fan adjacent one axial end
of said diametrically opposite tanks, a drive shaft located
coaxially of said semicircular core elements, primary support means
mounting said drive shaft on said engine for rotation by said
engine to rotate said fan, a back plate extending from said primary
support means radially of said drive shaft to a radial position
spaced adjacent the opposite axial end of said tanks from said fan,
an annular shroud adjacent said one axial end of said tanks closely
encircling said fan for cooperating with said backplate to direct
air moved by said fan in a radial direction through said air
passageways, means for supporting said tanks on said vehicle frame,
respective secondary resilient support means connected between said
shroud and the adjacent axial end of said tanks and between said
backplate and said opposite axial end of said tanks for resiliently
supporting said cores and tanks relative said shroud, backplate,
fan and engine, and a plurality of circumferentially spaced axially
extending arcuate struts fixed at opposite axial strut ends to said
shroud and backplate respectively for connecting said shroud to
said backplate and having opposite radial edges offset in a
circumferential direction for deflecting said air moved in a radial
direction.
Description
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention pertains to a radiator assembly comprising an
annular radiator for use in the cooling system of a truck, off-road
vehicle, or the like.
2. Description of the Prior Art
Conventionally, vehicle radiator assemblies comprise a vertical
flat, slab-type radiator, and a fan located immediately rearwardly
of the radiator. Air distribution over and through the radiator
core is inefficient for a number of reasons. First, because the
core is generally larger than the diameter of the fan, air is not
distributed over the entire surface of the core. Secondly, because
the fan is positioned quite close to the radiator, air flow through
the core is very uneven. Thirdly, because of the space limitations
in a vehicle and the relative motion between parts, it is
impossible to provide an effective fan shroud, and, hence, the fan
operates at a very low efficiency.
In an effort to overcome certain of the foregoing deficiencies,
rotary radiators have been proposed. However, they present at least
one additional serious problem--namely, the difficulty of providing
and maintaining satisfactory rotary seals at the connections
between stationary and rotating liquid-transfer tubing.
SUMMARY OF THE INVENTION
The radiator assembly unit of the present invention comprises a
static annular radiator and air propelling means located coaxially
thereof. With this arrangement, air is distributed about the entire
radiator, and the flow of air through the radiator is substantially
uniform. As a consequence, a vehicle engine of a given size can be
cooled with a unit which is smaller than a conventional flat
radiator; correspondingly, a unit of given size can cool a larger
engine than a conventional flat radiator of the same size.
The indicated radiator arrangement also permits a fan shroud to be
mounted close to the outer diameter of the fan of the air
propelling means. This improved shroud location contributes to
uniform air flow through the radiator, and materially increases the
efficiency of the fan. As a consequence of the latter factor, the
fan of the present unit, when compared with a fan of the same size
associated with a conventional flat radiator, provides greater air
flow at the same speed of operation and the same air flow at a
lower speed of operation. The lower speed of operation for a given
air flow demand results in lower horsepower requirements and
decreased noise generation.
In the specific embodiment of the invention disclosed herein, the
annular radiator is divided into three parts: one for the engine
coolant, one for transmission oil, and one for hydraulic fluid;
hence, three otherwise separate cooling units are integrated as a
single unit.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a front elevational view of a radiator assembly
incorporating the principles of the present invention;
FIG. 2 is a top view of the radiator assembly of FIG. 1;
FIG. 3 is a sectional view, taken substantially along the line 3--3
in FIG. 1, looking in the direction indicated by the arrows;
FIG. 4 is a partial bottom view of the radiator assembly of the
present invention, taken substantially along the line 4--4 in FIG.
3, looking in the direction indicated by the arrows;
FIG. 5 is a sectional view, taken substantially along the line 5--5
in FIG. 2, looking in the direction indicated by the arrows;
FIG. 6 is a sectional view, taken substantially along the line 6--6
in FIG. 2, looking in the direction indicated by the arrows;
and
FIG. 7 is a sectional view, taken substantially along the line 7--7
in FIG. 1, looking in the direction indicated by the arrows.
DESCRIPTION OF THE PREFERRED EMBODIMENT
Referring now to FIG. 1, there is indicated generally by the
reference numeral 10 a radiator assembly which embodies the
principles of the present invention and which is adapted to
simultaneously cool three separate fluids. The radiator assembly 10
comprises a static annular radiator 12 and air propelling means 14
located coaxially thereof.
The annular radiator 12 includes diametrically opposed first and
second tank portions 16 and 18, and a pair of substantially
semi-circular core portions 20.
The tank portions 16 and 18 (FIGS. 2-5) are each comprised of a
radially outer wall 22, a radially inner wall 24, two sets or
series of axially spaced side bars 26, and end walls 28 and 30.
Interiorly, the tank portions 16 and 18 are each divided into
first, second and third sections 32, 34 and 36 by means of
transverse partitions 38 and 40; and the second and third sections
34 and 36 of the second tank portion 18 are in turn subdivided into
two separate compartments by means of axial partitions 42 and 44.
Additionally, a first fluid inlet tube 46 is secured in the end
wall 30 of the first tank portion 16; and auxiliary fluid transfer
tube 48 is secured in the outer wall 22 of the first tank portion
16; a first fluid outlet tube 50 is secured in the end wall 30 of
the second tank portion 18; a second fluid inlet tube 52 and a
second fluid outlet tube 54 are secured in the outer wall 22 of the
second tank portion 18 on either side of the partition 42; and a
third fluid inlet tube 56 and a third fluid outlet tube 58 are
secured in the outer wall 22 of the second tank portion 18 on
either side of the partition 44.
The two core portions 20, as shown in FIGS. 2, 6 and 7, are each
comprised of a plurality of radial extending core elements 60 and
axially outer plates 62. Each core element 60 includes a pair of
semi-circular side plates 64 and two or more intermediate
semi-circular spacer rods 66. The core elements 60 are suitably
secured at their open ends between the side bars 26 of the tank
portions 16 and 18, and define a plurality of arcuate fluid
passageways 68 communicating at their ends with the tank portions
16 and 18. The arcuate fluid passageways 68 may have disposed
therein, if desired, turbulence promoting elements such as internal
fins (not shown). Also, the core elements 60 are axially spaced to
define intermediate radial air passageways 70 in which are disposed
louvered fin means 72. Additionally, one group of core elements 60
is connected to the first sections 32 of the tank portions 16 and
18, a second group of core elements 60 is connected to the second
sections 34 of the tank portions 16 and 18, and a third group of
core elements 60 is connected to the third sections 36 of the tank
portions 16 and 18. To accommodate the cooling of a greater or
lesser number of separate fluids, the number of sections of the
tank portions 16 and 18, and the corresponding number of groups of
core elements 60, may be increased or decreased as required. And,
the number of core elements 60 within each group may be varied to
provide the necessary cooling capacity for each different fluid.
The annular radiator 12 is typically mounted to a vehicle frame,
and, to accommodate such mounting, support flanges 73 are suitably
secured to the front plates 62 of the core portions 20.
The air propelling means 14, as shown in FIG. 3, includes a fan 74
which is located adjacent the front side of the annular radiator 12
and which is secured on a drive shaft 76. The shaft 76 is rotatably
mounted in primary support means comprised of a bearing assembly 78
secured to a primary support bracket 80. Also connected to the
primary support means is secondary support means comprised of a
combined secondary support bracket 82 and backplate 84 adjacent the
rear side of the annular radiator 12. Axial arcuate braces 86 are
secured between the secondary support means 82, 84 and an annular
fan shroud 88 adjacent the front side of the annular radiator 12.
The axial arcuate braces 86 serve to connect the shroud 88 to the
secondary support means 82, 84 for support thereby, and also serve
as air deflection vanes. Means, in the form of annular flexible
connectors 90, are provided intermediate the annular radiator 12
and the peripheries of the annular shroud 88 and the backplate 84
for absorbing the differential motion and for sealing the gaps
therebetween.
When the radiator assembly 10 is installed in a vehicle, the
support flanges 73 are secured to the vehicle frame (not shown);
the primary support bracket 80 is secured to the vehicle engine,
shown diagrammatically at 92 in FIG. 3; the drive shaft 76 is
driven by the engine 92 for example through a belt and pulley
arrangement (not shown); and the first fluid inlet and outlet tubes
46 and 50 are connected to the engine water jacket and water pump
(not shown) through inlet and outlet radiator hoses 94 and 96.
Additionally, the auxiliary fluid transfer tube 48 is connected to
a water reservoir tank (not shown); the second fluid inlet and
outlet tubes 52 and 54 are connected to the vehicle transmission
(not shown); and the third fluid inlet and outlet tubes 56 and 58
are connected to the vehicle hydraulic system (not shown). The
vehicle engine 92, the vehicle components referred to but not
shown, and the connections thereto, are conventional and do not
form part of the present invention.
When the engine 92 is operating, water or other coolant heated in
the engine 92 is directed therefrom through the inlet radiator hose
94 and the first fluid inlet tube 46 to the first section 32 of the
first or upper tank portion 16. The coolant received in the first
section 32 bifurcates and flows in parallel down through the first
group of core elements 60 of the core portions 20 at each side of
the radiator 12. The coolant flowing from the core elements 60 is
collected in the first tank section 32 of the second or bottom tank
portion 18 and returned through the first fluid outlet tube 50 and
the outlet radiator hose 96 to the engine 92. Required reserve
coolant is supplied through the auxiliary fluid transfer tube 48
from the reservoir tank connected thereto.
While the engine coolant is circulated as described, oil from the
vehicle transmission is directed into the second fluid inlet tube
52, circulated through the radiator 12, and returned from the
second fluid outlet tube 54 to the transmission. More specifically,
the transmission oil is circulated through one compartment of the
second section 34 of the bottom tank portion 18, the second group
of core elements 60 at one side of the radiator 12, the second
section 34 of the upper tank portion 16, the second group of core
elements 60 at the other side of the radiator 12, and the other
compartment of the second section 34 of the bottom tank portion
18.
Also concurrently, oil from the vehicle hydraulic system is
directed into the third fluid inlet tube 56, circulated through the
radiator 12, and returned from the third fluid outlet tube 58 to
the hydraulic system. In particular, the hydraulic system oil is
circulated through one compartment of the third section 36 of the
bottom tank portion 18, the third group of core elements 60 at one
side of the radiator 12, the third section 36 of the upper tank
portion 16, the third group of core elements 60 at the other side
of the radiator 12, and the other compartment of the third section
36 of the bottom tank portion 18.
To cool the liquids as they flow through the radiator 12, the fan
74 draws air axially inwardly of the radiator assembly 10 and
directs the same radially outwardly through the air passageways 70
across the air fin means 72. To be noted is that the shroud 88 is
mounted close to the outer diameter of the fan 74. By reason of the
described arrangement of the components of the radiator assembly
10, air is distributed about the entire radiator 12, the flow of
air through the radiator 12 is substantially uniform, and the
efficiency of the fan 74 is maximized. If desired, the direction of
air flow through the radiator assembly 10 could be reversed.
During operation of the engine 92 there is a certain degree of
vibration thereof. On the one hand, the fan 74 and the shroud 88,
which in effect are mounted to the engine 92 as a unit, move
conjointly with the engine 92 as the latter vibrates. On the other
hand, the radiator 12, which is mounted to the vehicle frame, is
isolated from vibrations, not only of the engine 92 but also of the
fan-shroud mounting, by means of the flexible connectors 90. The
foregoing arrangement allows the desired close fit to be maintained
between the fan 74 and the shroud 88.
While there has been shown and described a preferred embodiment of
the present invention, it will be understood by those skilled in
the art that various rearrangements and modifications may be made
therein without departing from the spirit and scope of the
invention.
* * * * *