Information
-
Patent Grant
-
6676040
-
Patent Number
6,676,040
-
Date Filed
Wednesday, November 21, 200123 years ago
-
Date Issued
Tuesday, January 13, 200420 years ago
-
Inventors
-
Original Assignees
-
Examiners
- Mar; Michael
- Gorman; Darren
Agents
- Birch, Stewart, Kolasch & Birch, LLP
-
CPC
-
US Classifications
Field of Search
US
- 239 463
- 239 53312
- 239 484
- 239 483
- 239 473
- 239 475
- 239 490
- 239 5332
- 239 5333
- 239 5855
- 239 390
- 239 391
- 239 394
- 239 89
- 239 91
- 251 12915
- 251 12921
- 251 127
-
International Classifications
-
Abstract
The present invention provides a GDI injector of a vehicle engine that can change the level of swirl motion and make it possible to increase engine output and fuel mileage, comprising a nozzle body having an opening along its longitudinal axis, a fuel inlet member, a cylindrically-shaped needle valve being centrally located within the opening of the nozzle body, and a swirl generator, the swirl generator comprising: an inner case having a cylindrically-shaped body and a plurality of equally and angularly spaced lobes, the inner case being coupled to the needle; an outer case having a cylindrically-shaped body and a plurality of equally and angularly spaced grooves, the outer case being fixedly attached to the nozzle body; and an inner case rotator.
Description
CROSS-REFERENCE TO RELATED APPLICATION
This application claims priority of Korea patent Application No. 10-2000-0086902, filed on Dec. 30, 2000.
BACKGROUND OF THE INVENTION
(a) Field of the Invention
The present invention relates to a fuel injector of a vehicle engine, and more particularly, to a high-pressure, direct-injection fuel injector having a swirl generator for imparting a desired level of swirling motion to the fuel as it exits the injector.
(b) Description of the Related Art
Generally, because a fuel injector of a GDI (Gasoline Direct Injection) engine injects fuel into a combustion chamber directly, it operates under high pressure. Also, the fuel injector of the GDI engine (hereinafter called a GDI injector) is required to inject a specific amount of fuel for a specific period. Moreover, in the process of injecting fuel there are many parameters to be considered, such as injection range, injection angle, size of fuel droplets, evaporation level and the like, and because the fuel injector is installed in the combustion chamber it has restrictions of space and temperature. Recently, several types of GDI injectors have been proposed, and among them a swirl type injector, which has a swirl generator, is widely adopted. The swirl generator imparts a swirling motion to the fuel as it exits the injector. Therefore, fuel dispersibility increases and fuel is prevented from being directly sprayed against a piston or a cylinder liner, and the fuel is well mixed with air.
But in the GDI engine it becomes necessary to change a level of a swirl flow component according to driving conditions. That is, when stratification combustion in the latter part of compression is performed at a low load range, a high level of swirl motion is required because the injection range should be relatively small, and fuel should be mixed with air quickly to get a suitable air-fuel mixture around a spark plug in a small combustion volume. On the other hand, when in a high load range, fuel is injected at an intake stroke or an early state of compression, and a low level of swirl motion is required because there is a large volume for burning and relatively sufficient time for mixing.
A conventional GDI injector is provided with a swirl generator around a needle being located in a nozzle tip. If the needle is operated such that a fuel passageway is formed, fuel passing through an inclined passageway of the swirl generator has a constant level of swirl motion.
Because the conventional GDI injector has a constant level of swirl motion under constant injection pressure, the conventional GDI injector has the same injection range and air-fuel mixing level in both uniform combustion and stratification combustion, and therefore optimal driving control is almost impossible.
SUMMARY OF THE INVENTION
The present invention has been made in an effort to solve the above problems. It is an object of the present invention to provide a GDI fuel injector having a swirl generator around the needle of the nozzle tip, which can change a level of a swirl motion component of injected fuel.
To achieve the above object, a GDI fuel injector has a nozzle body, a needle member centrally located within a nozzle body such that a fuel passageway is formed between the needle and the nozzle body, and a swirl generator, the swirl generator comprising:
an inner case having a cylindrically-shaped body having an opening from the upper end to the bottom end along its longitudinal axis, and several equally and angularly spaced lobes;
an outer case having a cylindrically-shaped body having an opening from the upper end to the bottom end along its longitudinal axis, and several equally and angularly spaced grooves
36
inside the body
34
, of such size and shape so as to receive the lobes of the inner case; and
an inner case rotator, one end of which is fixedly connected to the inner case such that the inner case can be axially rotated by axially rotating the inner case rotator, the other end being provided with a grip.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1
is a cross-sectional view of an injector provided with a swirl generator according to the present invention.
FIG. 2
is a perspective view of an inner case of the swirl generator according to the present invention.
FIG. 3
is a perspective view of an outer case of the swirl generator according to the present invention.
FIG. 4
is a sectional view of outside parts of region “A” of FIG.
1
.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
Hereinafter, a preferred embodiment of the present invention will be described in detail with reference to the accompanying drawings.
FIG. 1
is a cross-sectional view of an injector provided with a swirl generator according to the present invention,
FIG. 2
is a perspective view of an inner case of the swirl generator according to the present invention,
FIG. 3
is a perspective view of an outer case of the swirl generator according to the present invention, and
FIG. 4
is a sectional view of outside parts of region “A” of FIG.
1
.
As shown in
FIG. 1
, the injector has a fuel inlet member
22
, a nozzle body
12
having an opening along a longitudinal axis, and a cylindrically-shaped needle valve
14
that is centrally located within the opening of the nozzle body
12
and reciprocally moves between a closed position and one of a plurality of open positions, and a swirl generator
24
. There is a space between the circumference of the needle valve
14
and the nozzle body
12
, the space acting as a fuel passageway
16
, and the swirl generator
24
is disposed in a lower part of the fuel passageway.
The swirl generator
24
comprises a moveable inner case
26
secured to the needle valve
14
, a fixed outer case
32
fabricated to receive the inner case
26
, and an inner case rotator
18
. It is through the cooperation of these two cases
26
and
32
that the fuel passing through the injector is imparted with a tangential swirl force resulting in a swirl pattern.
The inner case
26
, as shown in
FIG. 2
, has a cylindrically-shaped body
28
having an opening from the upper end to the bottom end along its longitudinal axis, and several equally and angularly spaced lobes
30
. The width of the lobes gradually increases at an increasing rate in a downward direction, and therefore the shape of the lobes becomes generally a right triangle with a concave hypotenuse.
The needle valve
14
, as shown in
FIG. 1
, is inserted into the opening of the inner case
26
. The inner case
26
is secured to the needle valve
14
and therefore reciprocates and rotates with the needle. In order to prevent the inner case from rotating on the needle, the inner case is fabricated such that the radius of the opening of the inner case is identical to the outer radius of the needle, and furthermore, when the needle valve is inserted into the opening of the inner case in the process of manufacture, an adhesive material is applied between the needle valve and the inner case.
The outer case
32
, as shown in
FIG. 3
, has a cylindrically-shaped body
34
having an opening from the upper end to the bottom end along its longitudinal axis, and it has several equally and angularly spaced grooves
36
inside the body
34
, of such size and shape so as to receive the lobes of the inner case
26
, the number of which is equal to that of the lobes of the inner case.
The width of the grooves gradually increases in a downward direction, and therefore the shape of the grooves becomes generally trapezoidal. The area of the grooves
36
is greater than that of the lobes
30
, but the shape of the grooves
36
generally matches that of the lobes
30
.
The outer case
32
is disposed outside of the inner case
26
such that the lobes of the inner case are located in the grooves of the outer case, and therefore inclined passageways are formed between inclined edges of the lobes of the inner case and inclined edges of the grooves of the outer case.
The outer diameter of the outer case
32
is identical to the inner diameter of the nozzle body, and the outer case is forced into the nozzle body
12
. The outer case
32
, as shown in
FIG. 3
, can be manufactured in two parts such that the outer case can be easily inserted into the nozzle body.
The inner case rotator
18
is located inside the nozzle body, one end of which is fixedly connected to the inner case
26
, the other end being provided with a grip
20
. By rotating the grip
20
, the inner case
26
can be rotated in a clockwise or a counterclockwise direction such that the inclined fuel passageways can be changed, hence the level of swirl motion can be changed.
As shown in
FIG. 1
, the needle valve
14
is coaxially disposed within the inner case rotator
18
, and the grip
20
protrudes from an upper end of the nozzle body, and the fuel inlet member
22
is connected to the upper end of the nozzle body at an angle such that the grip is accessible.
Consequently, when fuel passes the fuel inlet member
22
of the injector
10
and the nozzle body and is injected into a combustion chamber, fuel passes through the inclined passageways formed between the outer case
32
and the inner case
26
of the swirl generator
24
that is installed in the lower part of the fuel passageway
16
. Above the swirl generator
24
fuel flows in a straight line, but as it passes through the swirl generator
24
it acquires a high level of swirl motion because it passes through the inclined passageways.
After fuel passes through the swirl generator, it is injected into the combustion chamber with a high level of swirl motion.
If the inner case
26
is rotated by rotating the grip
20
, the shape of the passageways formed between the lobes
30
of the inner case
26
and the grooves
36
of the outer case
32
is changed. Therefore, if the inner case
26
is rotated, the level of swirl motion of injected fuel is changed.
If the inner case
26
is rotated clockwise (being seen from the top) such that the vertical surfaces of the lobes
30
and the grooves
36
contact each other, inclined passageways are formed, and thus injected fuel has a high level of swirl motion.
On the other hand, if the inner case
26
is rotated counterclockwise such that the inclined surfaces of the lobes
30
and the grooves
36
contact each other when the needle valve is open, straight passageways are formed, and thus injected fuel doesn't swirl.
Furthermore, by regulating an angle of the inclined surfaces of the lobes
30
and the grooves
36
, a level of the swirl motion can be changed, and by changing direction of the inclination, swirl direction can be changed.
The conventional GDI injector has a constant level of swirl motion under constant injection pressure, and the same injection range and air-fuel mixing level in both uniform combustion and stratification combustion, and therefore optimal driving control is almost impossible. The swirl generator according to the present invention, by rotating the inner case, can change the level of the swirl motion and therefore fuel can be optimally injected in a GDI engine such that engine output and fuel mileage can be increased.
While the present invention has been described in detail with reference to the preferred embodiment, those skilled in the art will appreciate that various modifications and substitutions can be made thereto without departing from the spirit and scope of the present invention as set forth in the appended claims.
Claims
- 1. A GDI injector of a vehicle engine including a nozzle body having an opening along its longitudinal axis, a cylindrically-shaped needle valve being centrally located within the opening of the nozzle body, a fuel inlet member, and a swirl generator, wherein the swirl generator comprises:an inner case having a cylindrically-shaped body and a plurality of equally and angularly spaced lobes, the inner case being coupled to the needle valve such that the inner case does not rotate on the needle valve; an outer case having a cylindrically-shaped body and a plurality of equally and angularly spaced grooves that are fabricated to define a fuel passageway in cooperation with the lobes of the inner case, the outer case being fixedly attached to the nozzle body; and an inner case rotator for adjusting the level of swirl motion of the injected fuel by axially rotating the inner case relative to the outer case.
- 2. The GDI injector of claim 1 wherein a width of the lobes gradually increases at an increasing rate in a downward direction such that the shape of the lobes becomes generally a right triangle with a concave hypotenuse, and the width of the grooves gradually increases in a downward direction such that the shape of the grooves becomes generally trapezoidal.
- 3. The GDI injector of claim 1 wherein the outer case is divided into two parts along a centerline.
- 4. The GDI injector of claim 1 wherein the needle valve is coaxially disposed within the inner case rotator, and one end of the inner case rotator is fixedly connected to the inner case, the other end being provided with a grip.
Priority Claims (1)
Number |
Date |
Country |
Kind |
2000-86902 |
Dec 2000 |
KR |
|
US Referenced Citations (2)
Number |
Name |
Date |
Kind |
5207384 |
Horsting |
May 1993 |
A |
6206304 |
Koseki et al. |
Mar 2001 |
B1 |