Laser oscillating apparatus

Coherent light generators – Particular active media – Gas

Reexamination Certificate

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Details

C372S061000, C372S090000

Reexamination Certificate

active

06580742

ABSTRACT:

FIELD OF THE INVENTION
The present invention relates to an axial flow type gas laser oscillating apparatus for passing laser gas in a discharge tube.
BACKGROUND OF THE INVENTION
FIG. 37
shows an example of a schematic structure of a gas laser oscillating apparatus known as axial flow type. Referring to
FIG. 37
, the axial flow type gas laser oscillating apparatus (hereinafter referred to simply as “AFGLO”) is explained below. As shown in
FIG. 37
, the AFGLO is mainly composed of a laser resonator, a power supply unit, and a laser gas circulation part.
The laser resonator further comprises a discharge tube
1
having a discharge area
5
, a rear mirror (hereinafter referred to simply as “RM”)
6
, and an output mirror (hereinafter referred to simply as “OPM”)
7
. The discharge tube (hereinafter referred to simply as “DT”)
1
is composed of glass or other dielectric material, and electrodes
2
,
3
are provided near both ends of the DT
1
. In the space of the DT
1
enclosed by the electrodes
2
,
3
, the discharge area (hereinafter referred to simply as “DA”)
5
is formed. Plural DAs
5
are disposed between the RM
6
and OPM
7
. The RM
6
is a reflector having a reflectivity of about 100%. The OPM
7
is a partial reflector, and a laser beam
8
is emitted from the OPM
7
.
The power supply unit
4
is connected to the electrodes
2
,
3
in order to discharge in the DA
5
.
The laser gas circulating part (hereinafter referred to simply as “LGCP”) comprises a blower
13
, heat exchangers
11
,
12
, a laser gas passage
10
, DT
1
, and a laser gas lead-in part
14
. The laser gas lead-in part
14
is a part for leading the laser gas into the DT
1
from the laser gas passage
10
. The laser gas circulates the LGCP for composing the AFGLO in the direction of arrow
9
. The blower
13
is for circulating the laser gas. By this blower
13
, the flow velocity of laser gas is set around 100 m/sec in the DA
5
of the DT
1
. The pressure of the LGCP is about 100 to 200 Torr. When a specific voltage is applied from the power supply unit
4
, the DA
5
discharges. By this discharge and operation of the blower, the temperature of the laser gas climbs up. The heat exchangers
11
and
12
are for cooling the heated laser gas.
This is a structure of the conventional AFGLO, and its operation is explained.
The laser gas sent out from the blower
13
passes through the laser gas passage
10
, and is led into the DT
1
through the lead-in part
14
. In this state, when a specific voltage is applied to the electrodes
2
,
3
from the power supply unit
4
, the DA
5
discharges. The laser gas in the DA
5
obtains this discharge energy and is excited. The excited laser gas is resonated by the laser resonator composed of the RM
6
and OPM
7
. As a result, a laser beam
8
is emitted from the OPM
7
. This emitted laser beam
8
is utilized in laser processing and other applications.
Such conventional AFGLO had the following problems.
In the gas laser apparatus, the flow of laser gas in the DT
1
is preferred to be uniform from introduction of gas into the discharge tube until discharge, as far as possible, in the gas flow direction. If the gas flow is uniform, a stable discharge is obtained in the DA
5
. When the discharge is stable, the laser output from an electric input injected for discharge becomes higher. That is, the efficiency of laser output is high in terms of the injected electric input. To make the laser gas uniform in the DT
1
, the laser gas lead-in part may be formed coaxially with the DT
1
. However, due to structural characteristics of the AFGLO, it is difficult to install the laser gas lead-in part coaxially with the DT
1
. Accordingly, as shown in partial sectional views of the lead-in part
14
and DT
1
in FIG.
38
and
FIG. 39
(
FIG. 39
being a sectional view along line
39

39
in FIG.
38
), the laser gas lead-in part
14
is composed of a lead-in pipe
142
disposed nearly at right angle to the DT
1
, and a chamber
144
communicating with the laser gas passage
10
at the upstream side of the lead-in pipe
142
. The laser gas flows from the chamber
144
into the DT
1
through the lead-in pipe
142
. In this structure, the laser output characteristic (L
102
) is shown in FIG.
40
.
FIG. 40
shows the laser output with respect to the electric input to the discharge tube. In
FIG. 40
, the axis of abscissas denotes the discharge electric input, and the axis of ordinates represents the laser output. As shown in
FIG. 40
, as the discharge electric input into the DT
1
increases, the laser output saturates. In this structure, the discharge tended to be deviated in the outer circumference of the discharge tube. This deviation of discharge is visually recognized. Considering from this deviation of discharge, it is estimated that the gas flow is not uniform in the discharge tube. For example, the flow of laser gas from the lead-in pipe
14
into the DT
1
is estimated as shown in
FIG. 41
, that is, a gas flow disturbance (vortex)
18
is formed in the DT
1
, especially near the gas lead-in pipe
142
.
Further, as shown in partial sectional views of the lead-in part
14
and DT
1
in FIG.
42
and
FIG. 43
(
FIG. 43
being a sectional view along line
43

43
in FIG.
42
), an orifice
15
is disposed between the DT
1
and the lead-in pipe
14
. The orifice
15
is composed of a portion for impeding the flow of laser gas, and one hole
16
for passing laser gas. The hole
16
of the orifice
15
is deviated from the center. In this case, the laser output characteristic (L
104
) is as shown in FIG.
44
. As clear from
FIG. 44
, as the discharge electric input into the DT
1
increases, the laser output saturates, but as compared with the structure shown in
FIG. 38
, the laser output is slightly improved. However, in this structure, too, same as in the structure in
FIG. 38
, the discharge tended to be deviated into the outer circumference of the discharge tube. Considering from this result, for example, the flow of laser gas from the lead-in pipe
142
into the DT
1
is estimated as shown in
FIG. 45
, that is, a gas flow disturbance (vortex)
18
is formed in the DT
1
, especially near the gas lead-in pipe
142
.
Further, for example, Japanese Laid-open Patent No. 7-142787 discloses a structure in which a chamber for temporarily storing gas is provided, and it is connected to the laser gas lead-in part. This structure is intended to eliminate deviation of gas flow in the discharge tube by canceling directivity of laser gas flowing into the laser gas lead-in part. Also by disposing the laser gas lead-in part in a ring form around the discharge tube, it is attempted to dispose the laser gas lead-in part coaxially with the discharge tube. As investigated by the present inventors, in a same structure as in Japanese Laid-open Patent No. 7-142787, it is found that the laser gas flow in the discharge tube tends to deviate the discharge either into the central part or into the outer circumference of the discharge tube. This deviation of discharge can be visually recognized. Considering from this deviation of discharge, it is estimated that the gas flow is not uniform in the discharge tube. Besides, the structure is complicated.
SUMMARY OF THE INVENTION
To solve the above problems, the invention comprises a discharge tube for passing laser gas inside and exciting laser gas, a laser gas lead-in pipe connected to the discharge tube for leading the laser gas into the discharge tube, and a laser gas relay pipe for supplying laser gas into the laser gas lead-in pipe, and having a portion for allowing the laser gas to flow parallel to the flowing direction of the laser gas in the discharge tube. The flowing direction of laser gas in the laser gas relay pipe is parallel to and in the same direction as the flowing direction of the laser gas in the discharge tube.
The invention further comprises a discharge tube for passing laser gas inside and exciting laser gas, a laser gas lead-in pipe connected to the discharge tube for leading the laser gas int

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