Information
-
Patent Grant
-
6328222
-
Patent Number
6,328,222
-
Date Filed
Tuesday, April 25, 200024 years ago
-
Date Issued
Tuesday, December 11, 200122 years ago
-
Inventors
-
Original Assignees
-
Examiners
- Morris; Lesley D.
- Nguyen; Dinh Q.
-
CPC
-
US Classifications
Field of Search
US
- 239 5
- 239 5331
- 239 53312
- 239 5851
- 239 5855
- 239 406
- 239 417
- 137 898
- 137 628
- 137 870
- 251 12921
- 123 585
- 123 531
-
International Classifications
-
Abstract
A fuel injector for use in a internal combustion engine is disclosed. The fuel injector includes a body having a discharge end and a longitudinal axis extending therethrough, and an electromagnetic coil located within the body. The fuel injector further includes a fuel metering valve operable between an open position and a closed position and an air metering valve operable between an open position and a closed position. The fuel injector also includes a valve seat located within the body proximate to the discharge end and includes an orifice extending therethrough along the longitudinal axis. A needle is reciprocally mounted along the longitudinal axis between an open position and a closed position. The needle has an upstream end, a downstream end, and a needle channel extending therethrough along the longitudinal axis. The needle engages the valve seat in the closed position. A guide is disposed along the longitudinal axis such that the upstream end of the needle is reciprocable within the guide. A seal having a seal opening therethrough is located within the guide. A bellows fluidly connects the seal opening and the needle channel. The bellows and the guide form a generally annular chamber therebetween. The bellows is movable between a compressed and an extended position. The annular chamber is adapted to receive fuel. The seal prevents the fuel in the annular chamber from entering the needle channel. A method of operating the fuel injector is also disclosed.
Description
FIELD OF THE INVENTION
This invention relates to fuel injectors, and more particularly, to fuel injectors having a pulsed air assist air valve module.
BACKGROUND OF THE INVENTION
Fuel injectors are commonly employed in internal combustion engines to provide precise metering of fuel for injection into each combustion chamber. An electro-magnetic fuel injector typically utilizes an electromagnetic solenoid assembly to supply an actuating force to a fuel metering valve. Typically, the fuel metering valve is a plunger style needle valve which reciprocates between a closed position, where the needle is seated in a valve seat to prevent fuel from escaping through a metering orifice into the combustion chamber, and an open position, where the needle is lifted from the valve seat, allowing fuel to discharge through the metering orifice for injection into the combustion chamber.
The fuel injector atomizes the fuel during injection into the combustion chamber, breaking the fuel into a large number of very small particles, increasing the surface area of the fuel being injected, and allowing the oxidizer, typically ambient air, to more thoroughly mix with the fuel prior to combustion. The precise metering and atomization of the fuel reduces combustion emissions and increases the fuel efficiency of the engine.
Additionally, pressurized assist air can be injected into the fuel to assist in the atomization of the fuel into small particles. To optimize the fuel break-up, it would be beneficial to provide the pressurized air generally along the same direction as the fuel flow in order to reduce fuel pressure loss due to the air impacting the fuel. To do this, the air can be provided through a hollow needle. However, due to clearances between parts, fuel can leak into the needle, impeding the air flow.
It would be beneficial to provide a fuel injector in which both fuel and assist air is provided simultaneously by the operation of the fuel injector, and in which fuel cannot leak into the supply of assist air.
SUMMARY OF THE INVENTION
Briefly, the present invention provides a fuel injector for an internal combustion engine The fuel injector comprises a body and a fuel metering valve reciprocally located within the body. The fuel metering valve is operable between an open position and a closed position. The fuel injector also includes an air metering valve reciprocally located within the body, the air metering valve being operable between an open position and a closed position and an electromagnetic coil operatively connected to each of the fuel metering valve and the air metering valve to reciprocate the fuel metering valve and the air metering valve between the open position and closed positions.
The present invention also provides a fuel injector for an internal combustion engine. The fuel injector comprises a body having a discharge end and a longitudinal axis extending therethrough and a valve seat located within the body proximate to the discharge end. The valve seat includes an orifice extending therethrough along the longitudinal axis. The fuel injector also includes a needle reciprocally mounted along the longitudinal axis between an open position and a closed position. The needle having an upstream end, a downstream end, and a needle channel extending therethrough along the longitudinal axis. The needle engages the valve seat in the closed position. The fuel injector further includes a guide disposed along the longitudinal axis upstream of the needle and a seal located within the guide. The seal has a seal opening therethrough. The fuel injector also includes a bellows communicating the seal opening and the needle channel.
The present invention also provides a method of providing an atomizing air stream to fuel within a fuel injector. The method comprises providing a fuel injector having a body and a fuel metering valve reciprocally located within the body. The fuel metering valve is operable between an open position and a closed position. The fuel injector also includes an air metering valve reciprocally located within the body, the air metering valve being operable between an open position and a closed position and an electromagnetic coil operatively connected to each of the fuel metering valve and the air metering valve to reciprocate the fuel metering valve and the air metering valve between the open position and closed positions. The method further comprises providing fuel through the fuel metering valve and providing air through the air metering valve so that the air mixes with the fuel and assists in atomizing the fuel.
The present invention also provides a fuel valve for an air assisted fuel injector. The fuel valve comprises a needle having a longitudinal axis, an upstream end, a downstream end and a needle channel extending therethrough along the longitudinal axis. The fuel valve also includes a generally annular guide disposed along the longitudinal axis upstream of the needle and a seal located within the guide. The seal has a seal opening therethrough. The fuel valve also includes a bellows communicating the seal opening and the needle channel.
Additionally, the present invention provides a bellows for a fuel injector. The bellows comprises a first portion having a first portion interior and a first portion exterior and a second portion having a second portion interior and a second portion exterior. The second portion is biased away from the first portion. The bellows further includes a middle portion connecting the first portion and the second portion. The middle portion has a middle portion interior and a middle portion exterior. The middle portion has a plurality of first sections aligned in a first oblique direction to the longitudinal axis and a plurality of second sections aligned in a second oblique direction to the longitudinal axis. The first and second sections are alternately spaced.
BRIEF DESCRIPTION OF THE DRAWINGS
The accompanying drawings, which are incorporated herein and constitute part of this specification, illustrate the presently preferred embodiments of the invention, and, together with the general description given above and the detailed description given below, serve to explain features of the invention. In the drawings:
FIG. 1
is a side view, partially in section, of a fuel injector according to the present invention;
FIG. 2
is an enlarged side view, in section, of a downstream end of a fuel injector according to the present invention with a fuel metering needle in a closed position;
FIG. 3
is a side view, in section, of the downstream end of the fuel injector according to the present invention with the fuel metering needle in an open position;
FIG. 4
is a side view, in section, of an upstream end of a fuel injector according to the present invention with an assist air metering needle in a closed position; and
FIG. 5
is a side view, in section, of the upstream end of the fuel injector according to the present invention with the assist air metering needle in an open position.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
In the drawings, like numerals are used to indicate like elements throughout. A preferred embodiment of the present invention, shown in
FIGS. 1-5
, is a fuel injector
10
for use in a fuel injection system of an internal combustion engine. Referring to
FIG. 1
, the injector
10
includes a body
20
, a valve seat
30
, a fuel valve assembly
400
comprised of a needle
40
, a generally planar fuel metering orifice
50
, a mixing chamber or sac
60
, and an air inlet system
70
comprised of an air metering needle
720
. Details of the operation of the fuel injector
10
in relation to the operation of the internal combustion engine (not shown) are well known and will not be described in detail herein, except as the operation relates to the present invention. Although the present invention is generally directed to injector valves for internal combustion engines, those skilled in the art will recognize from present disclosure that the present invention can be adapted for other applications in which precise metering of fluids is desired or required.
Still referring to
FIG. 1
, the body
20
has an upstream or inlet end
210
and a downstream or outlet end
220
. As used herein, the term “upstream” generally refers to a portion of the injector
10
or a fluid flow proximate to the top of the injector
10
, and “downstream” generally refers to a portion of the injector
10
or a fluid flow proximate to the bottom of the injector
10
. The body
20
includes an armature
240
enclosed therein. An electromagnetic coil
242
located within the body
20
is selectively energized and deenergized to reciprocate the armature
240
and the needle
40
within the body
20
. The body
20
further includes a valve body shell
250
which is constructed from ferromagnetic material and which forms part of a magnetic circuit which operates the electromagnetic coil
242
. The valve body shell
250
partially surrounds a valve body
260
which includes a chamber
262
. The chamber
262
extends through a central longitudinal portion of the body
20
along a longitudinal axis
270
extending therethrough and is formed by an interior wall
264
. A needle guide
280
having a central needle guide opening
282
and a plurality of radially spaced fuel flow openings
284
(shown in
FIGS. 2 and 3
) is located within the chamber
262
proximate to the downstream end
220
of the body
20
. The needle guide
280
assists in maintaining reciprocation of the needle
40
along the longitudinal axis
270
. Referring back to
FIG. 1
, an overmold
285
constructed of a dielectric material, preferably a plastic or other suitable material, encompasses the valve body shell
250
. An o-ring
12
is located around the outer circumference of the valve body
260
to seat the injector
10
in an internal combustion engine (not shown).
Referring now to
FIGS. 2 and 3
, the fuel valve assembly further includes a guide or inlet tube
290
, which extends along the longitudinal axis
270
. The inlet tube
290
includes an upstream end
292
and a downstream end
294
and helps to guide the armature
240
during operation. The location of the inlet tube
290
in the body
20
determines the maximum height that the needle
40
lifts during operation. The inlet tube
290
communicates with a source of pressurized air (not shown) at the upstream end
292
of the inlet tube
290
such that air is able to pass between the source of pressurized air and the inlet tube
290
. A seal
296
is located within the inlet tube
290
, between the upstream end
292
and the downstream end
294
. The seal
296
includes a seal opening
298
extending therethrough, preferably along the longitudinal axis
270
.
The valve seat
30
is located within the chamber
262
proximate to the outlet end
220
between the needle guide
280
and the discharge end
220
. The valve seat
30
includes a passage or orifice
320
which extends generally along the longitudinal axis
270
of the body
20
and is formed by a generally cylindrical wall
322
. The valve seat
30
also includes a beveled sealing surface
330
which surrounds the orifice
320
and which tapers radially downstream and inward toward the orifice
320
such that the sealing surface
330
is oblique to the longitudinal axis
270
.
The needle
40
is reciprocally located within the chamber
262
generally along the longitudinal axis
270
of the body
20
. The needle
40
includes a longitudinal axis
402
which is co-linear with the longitudinal axis
270
of the body
20
. The needle
40
is reciprocable between a first, or open, position wherein the needle
40
is displaced from the valve seat
30
(as shown in FIG.
3
), allowing pressurized fuel to flow downstream past the needle
40
, and a second, or closed, position wherein the needle
40
is biased against the valve seat
30
(as shown in
FIG. 2
) by a biasing element, preferably a bellows
450
, precluding fuel flow past the needle
40
. The bellows
450
is preferably constructed from a spring-type metal for reasons that will be explained later herein.
Referring now to
FIGS. 2 and 3
, the needle
40
is located downstream of the inlet tube
290
. The needle
40
includes an upstream end
410
and a downstream end
420
. The upstream end
410
is fixedly connected to the armature
240
. The downstream end
420
includes a generally rounded valve contact face
422
which sealingly engages the beveled valve sealing surface
330
when the needle
40
is in the closed position. However, those skilled in the art will recognize that the downstream end
420
can be other shapes, including but not limited to, conical or frusto-conical, as well. Additionally, the downstream end
420
can include an extension (not shown) which extends into the sac
60
, reducing the area of the sac
60
. When the needle
40
is in the open position (shown in FIG.
3
), a generally annular channel
430
is formed between the valve contact face
422
and the valve sealing surface
330
, allowing fuel flow to the orifice
320
for discharge from the injector
10
.
The needle
40
is hollow and includes a needle channel
440
, which extends along the longitudinal axis
402
of the needle
40
between the upstream end
410
and the downstream end
420
. The bellows
450
, located within the inlet tube
290
, is fixedly connected to the inlet tube
290
through the seal
296
at a first portion or upstream end
452
. A second portion or downstream end
454
of the bellows
450
is fixedly connected to the upstream end of the needle
40
. A middle portion
458
connects the upstream end
452
and the downstream end
454
. The middle portion
458
has a plurality of first sections
458
a
aligned in a first oblique direction to the longitudinal axis
270
and a plurality of second sections
458
b
aligned in a second oblique direction to the longitudinal axis
270
. The first and second sections
458
a,
458
b
are alternately spaced to allow compression and extension of the bellows
450
as will be described in more detail herein. Each of the upstream end
452
, the downstream end
454
, and the middle portion
458
includes and interior and an exterior. A longitudinal channel
456
of the bellows
450
, comprised of the interiors of each of the upstream end
452
, the downstream end
454
, and the middle portion
458
, communicates the seal opening
298
with the needle channel
440
such that fluid can pass between the seal opening
298
and the needle channel
440
. The bellows
450
is movable between a compressed position when the needle
40
is in the open position and an extended position when the needle
40
is in the closed position. Preferably, the bellows
450
is biased to the extended position to seat the needle contact face
422
against the sealing surface
330
of the valve seat
30
and to bias the needle
40
away from the inlet tube
290
. Those skilled in the art will recognize that the bellows
450
can be constructed from other than a spring material, and a separate biasing spring (not shown) can be used to bias the needle
40
to the closed position.
A generally annular channel
460
is formed between the exterior of the bellows
450
and the inlet tube
290
. An upstream end of the channel
460
is sealed by the seal
296
, and a downstream end of the channel
460
is in fluid communication with an opening formed between the interface of the armature
240
and the inlet tube
290
, such that any fuel that leaks past the interface of the armature
240
and the inlet tube
290
is trapped within the annular channel
460
, and cannot flow into the upstream end
292
of the inlet tube
290
. In other words, the bellows
450
hermetically separates the annular channel
460
and the needle channel
440
.
Referring now to
FIGS. 4 and 5
, the air inlet system
70
includes a seat
710
, the air metering needle
720
, an armature
730
, and an air chamber
740
, located downstream of the seat
710
. The seat
710
includes a beveled contact surface
712
, which extends downstream and away from the longitudinal axis
270
. The contact surface
712
includes a sealing area
714
, which engages the air needle
720
when the air needle
720
is in the closed position. The seat
710
further includes a seat orifice
716
, which extends through the seat
710
along the longitudinal axis
270
.
The air needle
720
is reciprocably located within the body
20
along the longitudinal axis
270
. The needle
720
includes a longitudinal axis
722
, which is co-linear with the longitudinal axis
270
of the body
20
. The electromagnetic coil
242
is operatively connected to the needle
720
so that the needle
720
is reciprocable between a first, or open, position wherein the needle
720
is displaced from the seat
710
(as shown in FIG.
5
), allowing pressurized air from an assist air source (not shown) to flow downstream through the seat orifice
716
and past the needle
720
, and a second, or closed, position wherein the needle
720
is biased against the seat
710
(as shown in
FIG. 4
) by a biasing element, preferably a spring
244
, precluding air flow through the seat orifice
716
and past the needle
720
.
Referring still to
FIGS. 4 and 5
, the needle
720
also includes an upstream end
724
and a downstream end
726
. The upstream end
724
includes a generally rounded valve contact face
728
which sealingly engages the sealing area
714
when the needle
720
is in the closed position. However, those skilled in the art will recognize that the upstream end
724
can be other shapes, including but not limited to, conical or frusto-conical, as well. The downstream end
726
of the needle
720
is fixedly connected to the armature
730
. The armature
730
includes a plurality of air openings
732
which allow air to communicate between the air chamber
740
and the upstream end
292
of the inlet tube
290
.
The operation of the injector
10
is as follows. Preferably, the injector
10
is a bottom fuel feed injector. Pressurized fuel flow into the injector
10
is provided by a fuel pump (not shown). The pressurized fuel enters the injector
10
and passes through a fuel filter (not shown) and into the chamber
262
. The fuel flows through the valve body
260
, the fuel flow openings
284
in the guide
280
to the interface between the valve contact face
422
and the valve sealing surface
330
. In the closed position (shown in FIG.
2
), the needle
40
is biased against the valve seat
30
so that the valve contact face
422
sealingly engages the valve sealing surface
330
, preventing flow of fuel through the metering orifice
50
. The air needle
720
is biased to a closed position against the seat
710
, precluding assist air flow through the seat orifice
716
.
In the open position (shown in FIG.
3
), the electromagnetic coil
242
or other actuating device overcomes the biasing force of the bellows
450
, compressing the bellows
450
at the middle portion
458
, and reciprocates the needle
40
to an open position, removing the valve contact face
422
of the needle
40
from the sealing surface
330
of the valve seat
30
and forming the generally annular channel
430
. The pressurized fuel within the chamber
262
flows through the annular channel
430
, through the valve seat orifice
320
and into the sac
60
, as shown by the arrows F
1
in
FIG. 3
, where the fuel impacts on the metering orifice
50
. Some of the fuel flows through a space between the armature
240
and the inlet tube
290
, and into the annular channel
430
. The bellows
450
and the seal
296
prevent the fuel from entering the needle channel
440
.
Preferably, the spring
244
has a lower spring coefficient than the bellows
450
, so that the electromagnetic coil
242
activates the air supply armature
730
prior to the armature
240
, overcoming the biasing force of the spring
244
, and pulling the air needle
720
away from the seat
710
before the needle
40
is pulled away from the valve seat
30
. Pressurized air enters the air chamber
740
through the seat orifice
716
, as shown by the arrows F
2
in FIG.
5
and flows through the openings
732
in the armature
730
to the upstream end of the inlet tube
290
. The air flows through the inlet tube
290
toward the downstream end
294
, through the seal opening
298
, through the longitudinal channel
456
of the bellows
450
, and through the needle channel
440
. The air is discharged from the downstream end
420
of the needle
40
and into the sac
60
(shown in FIG.
3
), where the air mixes with the fuel, generating turbulence in the fuel and assisting in atomizing the fuel. The fuel/air mixture then flows through the metering orifice
50
and into the combustion chamber (not shown) for combustion.
When a pre-determined amount of fuel has been injected into the combustion chamber, the electromagnetic coil
242
or other actuating device deactivates, allowing the bellows
450
to extend and bias the needle
40
to the closed position, seating the valve contact face
422
of the needle
40
onto the sealing surface
330
of the valve seat
30
and closing the generally annular channel
430
. Since the spring
244
preferably has a lower spring coefficient than the bellows
450
, the air needle
720
closes after the needle
40
. When the air needle
720
closes, the air needle
720
shuts off the flow of pressurized air to the injector
10
. Those skilled in the art will recognize that the bellows
450
and the spring
244
can have different spring coefficients so that the needle
40
moves to the open position before the air needle
720
and to the closed position after the air needle
720
, or the bellows
450
and the spring
244
can have similar spring coefficients, so that the needles
40
,
720
move to the open and closed positions at the same time.
By adding assist air through the needle
40
into the sac
60
to mix with fuel in the sac
60
, turbulence is generated which improves atomization of the fuel in the sac
60
prior to metering through the metering orifice
50
. The improved spray atomization of the fuel through the metering orifice
50
into the fuel chamber decreases unwanted hydrocarbon emissions and increases the fuel efficiency of the internal combustion engine.
Preferably, in each of the embodiments described above, the valve seat
30
, the needle
40
, the metering orifice
50
, and the air inlet system
70
are each constructed from stainless steel. However, those skilled in the art will recognize that the valve seat
30
, the needle
40
, the metering orifice
50
, and the air inlet system
70
can be constructed of other, suitable materials.
It will be appreciated by those skilled in the art that changes could be made to the embodiments described above without departing from the broad inventive concept thereof. It is understood, therefore, that this invention is not limited to the particular embodiments disclosed, but it is intended to cover modifications within the spirit and scope of the present invention as defined in the appended claims.
Claims
- 1. A fuel injector for an internal combustion engine comprising:a body having a longitudinal axis; a fuel metering valve reciprocally located within the body, the fuel metering valve being operable between an open position and a closed position; an air metering valve reciprocally located within the body, the air metering valve being operable between an open position and a closed position; and an electromagnetic coil positioned between each of the fuel metering valve and the air metering valve along the longitudinal axis, the electromagnetic coil operative to reciprocate the fuel metering valve and the air metering valve in opposite directions along the longitudinal axis to place the respective air metering and fuel metering valves in their respective open position.
- 2. The fuel injector according to claim 1 wherein, when the fuel metering valve and the air metering valve are in the open position, fuel from the fuel metering valve and air from the air metering valve mix together, the air assisting in atomizing the fuel.
- 3. The fuel injector according to claim 2, wherein the fuel metering valve includes a needle having a channel extending therethrough, the channel adapted to allow a fluid to flow therethrough.
- 4. The fuel injector according to claim 1, wherein the fuel metering valve is biased toward the closed position by a first biasing element and the air metering valve is biased toward the closed position by a second biasing element.
- 5. The fuel injector according to claim 4, wherein the first biasing element has a first biasing coefficient and the second biasing element has a second biasing coefficient.
- 6. A fuel injector for an internal combustion engine comprising:a body having a discharge end and a longitudinal axis extending therethrough; a valve seat located within the body proximate to the discharge end, the valve seat including an orifice extending therethrough along the longitudinal axis; a needle reciprocally mounted along the longitudinal axis between an open position and a closed position, the needle having an upstream end, a downstream end, and a needle channel extending therethrough along the longitudinal axis, the needle engaging the valve seat in the closed position; a guide disposed along the longitudinal axis upstream of the needle; a seal located within the guide, the seal having a seal opening therethrough; and a bellows communicating the seal opening and the needle channel.
- 7. The fuel injector according to claim 6, wherein the bellows and the guide form a generally annular chamber therebetween.
- 8. The fuel injector according to claim 7, wherein the bellows hermetically separates the annular chamber and the needle channel.
- 9. The fuel injector according to claim 6, wherein the bellows is biased to an extended position.
- 10. The fuel injector according to claim 6, wherein air is forced into the seal opening, through the bellows and through the needle channel for discharge from the downstream end of the needle, the air mixing with the fuel.
- 11. The fuel injector according to claim 6, further comprising a fuel pathway within the body, the fuel pathway being in fluid communication with the annular chamber.
- 12. The fuel injector according to claim 6, wherein the guide comprises an inlet tube.
- 13. The fuel injector according to claim 6, wherein the bellows comprises a spring material.
- 14. The fuel injector according to claim 6, wherein the fuel injector further comprises an electromagnet located within the body.
- 15. The fuel injector according to claim 6, wherein the bellows further comprising:a first portion having a first portion interior and a first portion exterior; a second portion having a second portion interior and a second portion exterior, the second portion being biased away from the first portion; and a middle portion connecting the first portion and the second portion, the middle portion having a middle portion interior and a middle portion exterior, the middle portion having a plurality of first sections aligned in a first oblique direction to the longitudinal axis and a plurality of second sections aligned in a second oblique direction to the longitudinal axis, the first and second sections being alternately spaced.
- 16. The bellows according to claim 15, wherein the first portion interior, the middle portion interior, and the second portion interior comprise a fluid channel.
- 17. A method of providing an atomizing air stream to fuel within a fuel injector, the method comprising:providing a fuel injector having: a body disposed along a longitudinal axis; a fuel metering valve located within the body; and an air metering valve located within the body; moving the fuel metering valve in a first direction along the longitudinal axis, such that fuel flows through the body; and moving the air metering valve in a second direction opposite to the first direction along the longitudinal axis, such that air flows through the body.
- 18. The method according to claim 17, further comprising reciprocally operating the fuel metering valve between an open position and a closed position.
- 19. The method according to claim 18, further comprising reciprocally operating the air metering valve between an open position and a closed position.
- 20. The method according to claim 19, the body further including an electromagnetic coil operatively connected to each of the fuel metering valve and the air metering valve to reciprocate the fuel metering valve and the air metering valve between the open position and the closed position.
- 21. A fuel valve for an air assisted fuel injector comprising:a needle having a longitudinal axis, an upstream end, a downstream end and a needle channel extending therethrough along the longitudinal axis; a generally annular guide disposed along the longitudinal axis upstream of the needle; a seal located within the guide, the seal having a seal opening therethrough; and a bellows communicating the seal opening and the needle channel.
- 22. The fuel valve according to claim 21, wherein the bellows and the guide form a generally annular chamber therebetween.
- 23. The fuel valve according to claim 22, wherein the bellows hermetically separates the annular chamber and the needle channel.
- 24. The fuel valve according to claim 21, wherein the bellows is biased to an extended position.
- 25. The fuel injector according to claim 21, wherein the bellows further comprising:a first portion having a first portion interior and a first portion exterior; a second portion having a second portion interior and a second portion exterior, the second portion being biased away from the first portion; and a middle portion connecting the first portion and the second portion, the middle portion having a middle portion interior and a middle portion exterior, the middle portion having a plurality of first sections aligned in a first oblique direction to the longitudinal axis and a plurality of second sections aligned in a second oblique direction to the longitudinal axis, the first and second sections being alternately spaced.
- 26. The bellows according to claim 25, wherein the first portion interior, the middle portion interior, and the second portion interior comprise a fluid channel.
- 27. A fuel injector for an internal combustion engine, the fuel injector comprising:a body having an upstream end and a downstream end, the first and second ends disposed along a longitudinal axis; a fuel metering valve disposed at one of the upstream and downstream ends, the fuel metering valve reciprocable along the longitudinal axis from a closed position to an open position in a first direction and from an open position to a closed position in a second direction, the second direction being opposite to the first direction; and an air metering valve disposed at the other of the upstream and downstream ends, the air metering valve reciprocable along the longitudinal axis from a closed position to an open position in the second direction and from an open position to a closed position in the first direction.
US Referenced Citations (12)
Foreign Referenced Citations (2)
Number |
Date |
Country |
0 360 040 |
Mar 1990 |
EP |
0 683 315 A1 |
Nov 1995 |
EP |