GB2161319A - Gas discharge lasers - Google Patents
Gas discharge lasers Download PDFInfo
- Publication number
- GB2161319A GB2161319A GB08516113A GB8516113A GB2161319A GB 2161319 A GB2161319 A GB 2161319A GB 08516113 A GB08516113 A GB 08516113A GB 8516113 A GB8516113 A GB 8516113A GB 2161319 A GB2161319 A GB 2161319A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas laser
- laser tube
- tube according
- discs
- tube
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
- H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
- H01S3/02—Constructional details
- H01S3/03—Constructional details of gas laser discharge tubes
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
- H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
- H01S3/02—Constructional details
- H01S3/03—Constructional details of gas laser discharge tubes
- H01S3/032—Constructional details of gas laser discharge tubes for confinement of the discharge, e.g. by special features of the discharge constricting tube
- H01S3/0323—Constructional details of gas laser discharge tubes for confinement of the discharge, e.g. by special features of the discharge constricting tube by special features of the discharge constricting tube, e.g. capillary
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
- H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
- H01S3/02—Constructional details
- H01S3/04—Arrangements for thermal management
- H01S3/041—Arrangements for thermal management for gas lasers
Landscapes
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Engineering & Computer Science (AREA)
- Plasma & Fusion (AREA)
- Optics & Photonics (AREA)
- Lasers (AREA)
Abstract
A gas laser tube has a beryllium inner tube (10) with a precision ground bore aligned on the axies between the anode (20) and the cathode (18) by supporting said inner tube within an alumina outer tube (12) by means of axially spaced, perforated, copper support discs (14). A preferred arrangement has a stainless steel outer jacket forming part of a closed, de-ionised water cooling system. <IMAGE>
Description
SPECIFICATION
Gas laser tube apparatus
Field of the Invention
This invention relates to gas laser tube apparatus, and more especially to an improvement in the construction of the laser tube in particular to enable simplified manufacture and easier alignment.
Prior Art
In the accompanying drawings, Figures 1 to 3 diagrammatically illustrate three known designs of ion laser tube.
In the design shown in Figure 1, a continuous bore 10 is formed in a Beryllia rod 12.
In the design shown in Figure 2, a non-continuous bore 14 extends through thick disc segments 16 of graphite located in a quartz outer tube 18.
In the design shown in Figure 3, a bore is defined by aligned apertures 20 in tungsten discs 22 axially spaced along an alumina outer tube 24.
In each of Figures 1 to 3, the metal anode and metal cathode are identified by reference numerals 26, 28. In each case, the laser tube is terminated beyond the cathode and/or anode by a window assembly, such as a Brewster stub, and provision is made for cooling by means of a water jacket at least partly surrounding the tube over the major part of its length.
The known arrangements have various disadvantages, such as risk of cracking at the cathode due to thermal stress, electrolysis at the anode, and risk of the window becoming coated due to sputtering, especially in the case of the design shown in Figure 3,
Furthermore, the arrangement of Figure 3 presents a particular problem during manufacture, namely that of ensuring correct alignment on the anode/cathode axis of the centrally apertured tungsten discs. On the other hand, whilst this problem is minimised with the construction of Figure 1, this arrangement, like that of Figure 2, presents problems during manufacture due to the difficulty and number of steps required to achieve satisfactory jointing between the glass window assemblies, the metal anode and cathode and the ceramic material around the bore.
This problem is present to a much lesser extent with the construction of Figure 3, but only at the expense of increased alignment problems.
Object of the Invention
It is a primary object of this invention to provide a gas laser tube arrangement which avoids or minimises the manufacturing disadvantages of the known laser tube designs above described.
The Invention
Gas laser tube apparatus according to the invention comprises, between the anode and the cathode, a continuous bore formed by inner tubular means centered within an outer tube on the anode/ cathode axis by axially spaced discs each fixed in position to at Feast one of the tubes.
The inner tubular means may be a single tube or two or more tubular parts abutting end to end.
A preferred construction employs an alumina outer tube, an inner tube of beryllia (BeO) and copper support discs. These discs are each preferably connected to the outer tube, and most preferably to the inner tube as well.
The internal bore of the beryllia tube is preferably made by precision grinding.
The support discs are preferably perforated to enable free gas flow between the inner and outer tubes, thus permitting return gas flow, in a manner in itself known from the construction of Figure 3.
Further-more, the discs are preferably convoluted or otherwise shaped to facilitate expansion due to thermal stresses and the like.
A preferred window assembly at each end of the tube arrangement is a Brewster stub.
Cooling may be effected by means of a water jacket, and according to a further feature of the invention a closed cycle de-ionised water system may be employed. The water jacket surrounding the alumina outer tube is preferably made of stainless steel. However, air cooling will often be satisfactory in view of the relatively large surface area of the outer tube.
In practice, the bore in the inner tube may have a diameter of the order of 0.5 to 2.5 mm, typically 1.6 to 2.0 mm, and the outer tube can have a diameter of the order of 25 to 40 mm. It is envisaged that the discharge length may be of the order of 26 cms, but for differing purposes and applications the length of the inner tube may be any value in the range 3 to 45 cm.
In one practical watercooled design, an operating voltage of about 180 V is convenient, delivering about 21 Amps, thereby giving a power input into the tube of about 3780 watts. This operating voltage is readily obtainable from a 240 V single-phase source. However, tubes of different lengths and bores will have different operating voltages and currents.
The practical construction referred to is for an
Argon ion laser, but the invention is also applicable to other gas ion lasers such as a Krypton laser.
Description of the drawings
In the accompanying drawings:
Figures 1 to 3 illustrate known laser tube designs as hereinbefore described; and
Figure 4 illustrates a gas laser tube arrangement in accordance with the present invention; and
Figure 5 shows to an enlarged scale the convoluted support discs used in the invention; and
Figure 6 shows part of a closed loop cooling system.
Figure 7 shows a modified arrangement in somewhat diagrammatic manner; and
Figures 8 and 9 shows possible modifications.
Description of the embodiment
Referring to Figures 4 to 6, the Argon or Krypton filled laser tube has a bore formed by a beryllia tube 10 having a nominal external diameter of the order of 12 mm and a precision ground axial bore of 1.8 mm diameter. This is surrounded by an outer alumina tube 12, say of about 32 mm diameter, which is used to support the bore tube 10 by means of axially spaced copper fins or discs 14.
These discs 14 are brazed in position to both the tubes 10 and 12, and contain perforations 16 for return gas flow. In addition, the discs 14 have a convoluted shape (as best shown in Figure 5) to enable thermal expansion.
The anode 18 and the cathode/heater 20 are brazed in position via suitable supports to the alumina outer tube 12, and the tube arrangement is completed at each end by a Brewster window stub 19 or 20, fixed in position to the cathode and anode supports.
Thus the invention avoids awkward ceramic to glass joints, and alignment problems are minimised as compared with aligning a plurality of annular inserts since the beryllia tube only has to be aligned with the anode/cathode axis.
All brazing may be effected in one continuous step, thus simplifying manufacture.
A stainless steel water jacket 22 surrounds the alumina outer tube 12. This forms part of a closed cycle system (see Figure 6) using de-ionised water which passes through a radiator 30 air cooled by a motor driven fan 32. A pump 34 is employed to ensure good flow.
In addition to the manufacturing and alignment
advantages, the laser tube arrangement in accordance with the invention is also found to reduce other disadvantages of the known constructions of
laser tube, such as thermal stress at the cathode
and electrolysis at the anode.
Figure 7 shows a modified arrangement employ
ing air cooling, which is practicable due to the relatively large surface area of the outer Alumina tube
12. In this modified arrangement, the anode 18 is
not centred by spacers within the outer tube 12; in fact the anode assembly 40 and cathode assembly
42 adjoin the ends of the outer tube in this modifi
cation.
Figures 8 and 9 show possible modifications
wherein the inner Beryllia tube 10 is formed in two
abutting parts (although three or more such parts
are equally possible provided a continuous bore is
defined).
In Figure 8, two beryllia tube parts are formed
with selflocating end portions 44 at their abutting
ends.
In Figure 9, a copper jointing sleeve 46 is em
ployed, which may be brazed in place and centred,
although this is not shown, by a disc 14.
An advantage of the modifications exemplified
by Figures 8 and 9 is that longer continuous preci
sion bores can be formed, notwithstanding limita
tions on the length of an integral Beryllia tube,
which can be satisfactorily bored with high preci
sion.
Various other modifications of the described em
bodiments are possible within the scope of the in
vention hereinbefore described.
Claims (21)
1. Gas laser tube apparatus having a continuous bore aligned on the anode/cathode axis, wherein inner tubular means defining the said continuous bore is centred on said anode/cathode axis within an outer tube by means of axially spaced discs each fixed in position to at least one of the tubes.
2. A gas laser tube according to claim 1, wherein the inner tubular means is a beryllia tube.
3. A gas laser tube according to claim 1 or claim 2, wherein the outer tube is an alumina tube.
4. A gas laser tube according to claim 1, 2 or 3 wherein the discs are copper discs.
5. A gas laser tube according to any of claims 1 to 4, wherein the inner tubular means has a precision ground bore.
6. A gas laser tube according to any of claims 1 to 5, wherein the discs are perforated to enable gas flow between the inner and outer tubes.
7. A gas laser tube according to any of claims 1 to 6, wherein the discs are convoluted to accommodate thermal expansion.
8. A gas laser tube according to any of claims 1 to 7, having a window assembly in the form of a
Brewster stub at each end.
9. A gas laser tube according to any of claims 1 to 8, wherein the discs are connected to both the inner and outer tubes.
10. A gas laser tube according to any of claims 1 to 9, wherein the anode and/or cathode are fixed to the outer tube.
11. A gas laser tube according to claim 10, wherein the anode and/or cathode are aligned within the outer tube by supporting annular spacers.
12. A gas laser tube according to any of claims 1 to 11, wherein the outer tube is surrounded by a cooling jacket.
13. A gas laser tube according to claim 12, wherein the cooling jacket forms part of a closed cycle de- ionised water cooling system.
14. A gas laser tube according to claim 11 or 12, wherein the cooling jacket is made of stainless steel.
15. A gas laser tube according to any of claims 1 to 11, wherein the outer tube is air cooled.
16. A gas laser tube according to any of claims 11 to 15, wherein the inner tubular means is formed of two or more tubular parts abutting end to end.
17. A gas laser tube according to any of claims 1 to 16, wherein the inner tube has a diameter in the range 0.5 to 2.5 mm and the outer tube has a diameter in the range 25 to 40 mm.
18. A gas laser tube according to claim 17, having in operation a discharge length of the order of 3 to 45 cm.
19. A gas laser tube according to any preceding claim, in combination with power supply means for producing an operating voltage selected for given tube dimensions.
20. A gas laser tube according to any of claims 1 to 17, being an Argon or Krypton laser tube.
21. A gas laser tube substantially as hereinbefore described with reference to Figures 4 to 6 or
Figure 7 or Figure 8 or Figure 9 of the accompany ing drawings.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB08516113A GB2161319B (en) | 1984-07-03 | 1985-06-26 | Gas discharge lasers |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB848416916A GB8416916D0 (en) | 1984-07-03 | 1984-07-03 | Gas laser tube apparatus |
GB08516113A GB2161319B (en) | 1984-07-03 | 1985-06-26 | Gas discharge lasers |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8516113D0 GB8516113D0 (en) | 1985-07-31 |
GB2161319A true GB2161319A (en) | 1986-01-08 |
GB2161319B GB2161319B (en) | 1988-02-24 |
Family
ID=26287946
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08516113A Expired GB2161319B (en) | 1984-07-03 | 1985-06-26 | Gas discharge lasers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2161319B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4774713A (en) * | 1986-12-16 | 1988-09-27 | American Laser Corporation | Segmented laser tube structure |
US4779284A (en) * | 1987-03-26 | 1988-10-18 | Spectra-Physics, Inc. | Gas laser with coaxial gas resevoir |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1271425A (en) * | 1968-06-21 | 1972-04-19 | Hitachi Ltd | Electrical discharge tube |
GB1302847A (en) * | 1969-11-27 | 1973-01-10 | ||
GB1336667A (en) * | 1970-05-08 | 1973-11-07 | Rca Corp | Gas laser discharge tube |
GB1385608A (en) * | 1972-06-12 | 1975-02-26 | Rca Corp | Means for ensuring starting of a gas laser |
GB1422602A (en) * | 1972-05-24 | 1976-01-28 | Thomson Csf | Cold cathode gas lasers |
GB1452899A (en) * | 1972-11-06 | 1976-10-20 | Rca Corp | Metal vapour laser discharge device |
GB1496446A (en) * | 1974-04-19 | 1977-12-30 | Rca Corp | Gas laser tube |
-
1985
- 1985-06-26 GB GB08516113A patent/GB2161319B/en not_active Expired
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1271425A (en) * | 1968-06-21 | 1972-04-19 | Hitachi Ltd | Electrical discharge tube |
GB1302847A (en) * | 1969-11-27 | 1973-01-10 | ||
GB1336667A (en) * | 1970-05-08 | 1973-11-07 | Rca Corp | Gas laser discharge tube |
GB1422602A (en) * | 1972-05-24 | 1976-01-28 | Thomson Csf | Cold cathode gas lasers |
GB1385608A (en) * | 1972-06-12 | 1975-02-26 | Rca Corp | Means for ensuring starting of a gas laser |
GB1452899A (en) * | 1972-11-06 | 1976-10-20 | Rca Corp | Metal vapour laser discharge device |
GB1496446A (en) * | 1974-04-19 | 1977-12-30 | Rca Corp | Gas laser tube |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4774713A (en) * | 1986-12-16 | 1988-09-27 | American Laser Corporation | Segmented laser tube structure |
US4779284A (en) * | 1987-03-26 | 1988-10-18 | Spectra-Physics, Inc. | Gas laser with coaxial gas resevoir |
Also Published As
Publication number | Publication date |
---|---|
GB8516113D0 (en) | 1985-07-31 |
GB2161319B (en) | 1988-02-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |