U.S. patent number 3,776,209 [Application Number 05/348,360] was granted by the patent office on 1973-12-04 for fuel injector manifold and mounting arrangement.
This patent grant is currently assigned to The Bendix Corporation. Invention is credited to William A. Peterson, Jr., Harry P. Wertheimer.
United States Patent |
3,776,209 |
Wertheimer , et al. |
December 4, 1973 |
FUEL INJECTOR MANIFOLD AND MOUNTING ARRANGEMENT
Abstract
A liquid injector manifold and mounting arrangement wherein the
fuel injector is supported in the engine at one end in a
cylindrical bore with the aid of a circular seal. The injector
extends from the engine and is supported at its other end by an
extending fitting which tees off from a tubular common rail liquid
fuel manifold. The tubular liquid fuel manifold is supported by
brackets at a raised elevation. The connection between manifold
fitting and fuel injector also employs a cylindrical surface and
circular seal connection.
Inventors: |
Wertheimer; Harry P.
(Horseheads, NY), Peterson, Jr.; William A. (Corning,
NY) |
Assignee: |
The Bendix Corporation
(Southfield, MI)
|
Family
ID: |
23367677 |
Appl.
No.: |
05/348,360 |
Filed: |
April 5, 1973 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
|
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181680 |
Sep 20, 1971 |
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Current U.S.
Class: |
123/470; 123/469;
239/550 |
Current CPC
Class: |
F02M
51/005 (20130101); F02M 55/00 (20130101); F02M
69/465 (20130101); F02M 61/145 (20130101) |
Current International
Class: |
F02M
51/00 (20060101); F02M 61/14 (20060101); F02M
69/46 (20060101); F02M 55/00 (20060101); F02M
61/00 (20060101); F02m 055/00 () |
Field of
Search: |
;123/32AE,32EA,148A,32V,139AW,32E,119R,32SU,32F,32G,32H,32R,52M
;285/345 ;239/550,551 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Burns; Wendell E.
Parent Case Text
This is a continuation, division, of application Ser. No. 181,680,
filed Sept. 20, 1971 now abandoned.
Claims
I claim:
1. A fuel injector mounting arrangement for an engine
comprising:
a tubular common fuel rail for maintaining an available standby
source of fuel;
a rigid bracket member connected to said fuel rail and adapted to
be fixedly attached to an engine to provide support at a location
along the fuel rail;
at least one fitting connected to said fuel rail a spaced distance
from the location of support provided by said bracket member;
and
an injector valve assembly having connections at each end with said
fitting and the engine to provide two-point support at spaced
distances along the length of the injector valve, each said end
connections having its respective interfitting cylindrical surfaces
aligned along the longitudinal axis of the injector valve assembly
and each end connection arranged to confine movement of the
injector valve assembly in one direction while permitting slidable
movement in the opposite direction along said axis.
Description
BACKGROUND OF THE INVENTION
Liquid fuel injection systems are receiving increasing acceptance
because of the need for more accurate fuel handling systems to
combat excessive exhaust emissions. Unfortunately, fuel injection
systems are complex and expensive, particularly multiple point
injection systems where injection occurs adjacent each engine
cylinder or subgrouping of cylinders. Another problem has been to
dissipate heat in and around the injectors to reduce consequent
fuel vaporization which leads to loss of metering accuracy.
DESCRIPTION OF THE PRIOR ART
Perhaps the most common prior art approach to injector mounting is
to simply form a boss on the engine block or air intake manifold
for each injector location, drill and thread the boss, and form
complementary threads on the injector housing. Thus, the injector
is securely mounted and entirely supported at one end, as
illustrated in prior U. S. Pat. No. 2,980,090. The injector may be
partly recessed and arranged to receive fuel from passages partly
formed in the block as illustrated in U. S. Pat. No. 3,247,833. In
prior practice, the liquid fuel manifold does not substantially
assist in supporting the injectors.
SUMMARY OF THE INVENTION
In the present invention the liquid fuel manifold is utilized as a
support member at one end of the injector valve, giving the
required structural support without the necessity of expensive
pockets or passages or thread-forming operations. Moreover, by the
use of circular seals on cylindrical surfaces at the connection
points at either end of the injector, mating tolerances along the
injector valve axis are considerably relaxed.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a top view of a common fuel rail injector valve
installation as it might appear for one bank of a V-8 engine;
FIG. 2 is a side view of the installation of FIG. 1;
FIG. 3 is an end view of the installation of FIG. 1 showing
particularly in detail the support bracket for common injector fuel
rail; and
FIGS. 4 and 5 illustrate two configurations of injector mounting
detail.
DETAILED DESCRIPTION OF THE DRAWINGS
The drawings illustrate a common rail liquid fuel distribution
injection system which is particularly arranged to provide good
support for the injectors by means of a mounting technique which
can be easily manufactured in mass production with very low
tolerance requirements.
The common fuel rail or manifold consists of interconnected
passages 10, 12, and 14 which receive fuel through tee connection
11 from a fuel inlet 9. A fuel return passage 18 is normally
provided, leading back to the fuel tank (not shown) from fuel
pressure control valve 16.
A portion of the engine in the embodiment of FIGS. 1-3 is
designated by numeral 20 which is representative of that portion of
the engine where it is desired to mount the injectors. This may be
either the engine block per se, cylinder head(s), or a portion of
the air intake manifold, depending on engine and manifold design
and desired point of injection. A pair of wing-shaped brackets 22
and 24, best shown in FIG. 3, are affixed by studs 26 to the top of
engine portion 20 to provide rigid fixed support members for the
fuel rail. Horseshoe straps 28 secure fuel rail passage 12 to the
ends of the support brackets at a point of raised elevation above
the engine. A plurality of fittings 30a, 30b, 30c, and 30d are
secured to fuel rail passage 12 at spaced locations and each
receives the top end of a respective injector 32a, 32b, 32c, and
32d. The injectors may be of several well-known types of
electromechanical injector valves, two configurations of which are
illustrated in the referred to prior patents. The lower ends of the
injector valves are received in the raised bosses 34a, 34b, 34c and
34d formed in the engine block or manifold 20. Each injector also
has an electrical connector 36a, 36b, 36c and 36d respectively to
supply the energizing electrical energy to selectively open the
injectors at desired intervals.
Referring to FIGS. 4 and 5, two configurations illustrating the
injector support connections are shown. In the FIG. 4 arrangement,
the injector 32a is received in cylindrical bore 40 formed in the
engine portion 20 which bore contains a seal groove 42 which
receives elastic or deformable circular seal 44. On its inner
diameter seal 44 cooperates with a large diameter cylindrical
surface 46 formed on the injector housing which permits the
injector to project well through the engine wall. The elastic seal
on cylindrical surface permits tolerances to be relaxed in both the
radial and axial directions. The seal will, of course, deform to
compensate for radial deviations in dimensions or concentricity and
is capable of sealing along a considerable length of cylindrical
surface 46 of the injector to accept wide deviations in an axial
sense.
FIG. 5 shows most clearly the connection between the other end of
the injector and fitting 30b. Fitting 30b is secured to fuel rail
12 by brazing or the like. A hole 48 is drilled through the side
wall of tube 12 to permit fuel to flow into the cylindrical bore 50
formed in the fitting. A seal groove 52 receives an elastic and
deformable circular seal 54. Seal 54 cooperates with the
cylindrical surface 56 formed on the injector end to accept both
radial and axial tolerance variations in the manner previously
described and perform a liquid-to-air sealing function.
Referring to FIGS. 1 and 2, it will be noted that each fitting 30
is a spaced distance away from the points of connection of the fuel
rail to rigid supports 22 and 24. The fuel rail may be of simple
metal tubular construction or equivalent materials and
configuration to permit some deflection or bending transversely to
the axis of the fuel rail. Thus, the fitting may be utilized to
provide an axial seating load to the injector housing and may be
displaced by bending the fuel rail to accept further tolerance
variations and facilitate injector assembly and/or replacement.
While an axial seating load has some locating advantages, it is not
essential to the practice of the invention since sealing at both
ends is accomplished by radial compression of the deformable seals
54 and 42.
The described mounting arrangement is well suited to mass
production manufacture at low cost since simple, easy to machine,
cylindrical surfaces are utilized at the attachment points and
elastic seals, which permits manufacturing tolerances to be
considerably relaxed. The use of the fuel rail as an injector
support device utilizes existing structure to perform an additional
function with virtually no increase in cost, but merely by means of
judicious arrangement. The injectors are mounted to project well
out of the engine block and need not be recessed therein to provide
good ventilation while still having durable two-point support.
* * * * *