CA1136250A - Compact flowing gas system for lasers - Google Patents

Compact flowing gas system for lasers

Info

Publication number
CA1136250A
CA1136250A CA000344171A CA344171A CA1136250A CA 1136250 A CA1136250 A CA 1136250A CA 000344171 A CA000344171 A CA 000344171A CA 344171 A CA344171 A CA 344171A CA 1136250 A CA1136250 A CA 1136250A
Authority
CA
Canada
Prior art keywords
laser
gas
cavity
housing
high pressure
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.)
Expired
Application number
CA000344171A
Other languages
French (fr)
Inventor
Henry L. Pratt
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
US Department of Army
Original Assignee
US Department of Army
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by US Department of Army filed Critical US Department of Army
Application granted granted Critical
Publication of CA1136250A publication Critical patent/CA1136250A/en
Expired legal-status Critical Current

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Abstract

Abstract of the Disclosure A miniature air actuated vacuum transducer is connected on the down-stream side of a laser and is disposed for creating a vacuum suction for exhausting gas from a flowing gas laser system. Specifically, a compact flow-ing laser is disclosed in combination with a specific pulp or vacuum trans-ducer. A small high pressure gas cylinder is provided such that applicant's laser can operate in a miniaturized environment.

Description

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Miniature gas lasers ~uch as waveguide C02 systems utilize internal gas mixtures at partial atmospheric pressures~ Longitudinally excited lasers typically are operated at low pressures on the order of 35 to 200 Torr. The transversely excited (TE) waveguide lasers are operated at some-what higher pressures (50 to 300 Torr typically), and although pressures as high as 4 atmospheres have been reported, numerou6 limitations still exist in the development of positive pressure tranversely excited (TEA) lasers in waveguide configurations.
Successful operation of low power, longitudinally excited C02 wave-guide lasers has been obtained with sealed off gas reservoirs, and commercial versions of CW waveguide lasers are now available from at least two sources.
However~for higher power, pulsed, and TE configurations, flowing gas systems at partial atmospheric pressures are generally employed with some sort of vacuum pumping. The trip]e requirements of relatively low absolute pressure (lOO Torr), capable of starting at atmospheric pressure, and capable of exhaus-ting into atmospheric pressure cannot be met by most of the lighter and smaller classes of vacuum pumps.
; To overcome many of these limitations and to provide a more compact, -~
portable gas handling system, the present invention utilizes a miniature air -operated vacuum pump which works on the principle of the venturi tube in which a high pressure source of air or other gas is rapidly expanded in an enlarged chamber downstream of a small orifice. This creates a very low pressure area within the venturi chamber J which provides a vacuum suction at a side port located backstream of the rapidly expanding gas. The downstream side of the laser resonator is connected to thi~ port.
A flowing gas laser systen) utilizing internal gas mixture~ at partial atmospheric pressure. A regulated active medium supply directs the gas (C02~ ~le, N2) into the laser cavity. A vacuum transducer i~ connected on the downstream side of the laser cavity to exhaust the gas from the laser cavity. A high pressure source of air is directed through a small orifice and is rapidly expanded in an enlarged chamber do~mstream of the small orifice and is rapidly expanded in an enlarged chamber downstream of the small orifice creating a -., .,- : , ., ",,,~ , :

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low pressure area within the venturi charnber to provide a vacuum suction at a side port which is connected to the laser cavity.
Figure 1 i8 a diagra~natic vlew of the ilowing gas la~er system oi the present invention.
~igure 2 is a pictorial view of a miniature vacuum pump used in the laser system.
Figure 3 is a graph illustratLng the absolute pressure and the air supply pressure in a particuLar application of the device.
As shown in Figure 1, a waveguide laser 10 includes a body 12 having a pair of mirrors 13 and 15 forming a resonant optical cavity 17. Mirror 15 is partially transmissive to form an energy abstracting means. A pair of electrodes l9 and 21 are connected to a high voltage power source 23 and mounted ~-in body 12. A pair of inlets 14 and 16 connect into an axial cavity 18. A
regulated gas supply 20 (C02, He, N2) is connected through a valve 22 to inlets i 14 and 16. An outlet port 24 i8 in communication with cavity 18.
A vacuum transducer 26 is provided with a port 28 which i9 connected to outlet port 24 of the laser. Pressure is monitored via a vacuum gage, 29.
.
." ~, The housing of transducer 26 includes an inlet port 39 and an exhaust port 32.
The transducer includes a body 34 having a small orifice 36 therein disposed in communication with an enlarged chamber or exhaust port 32. A gas supply 38 ~ -(N2~or air) is connected through a valve 40 to inlet port 30 of the transducer.
In operation, gas from supply 38 is directed into the transducer through inlet 30, and through orifice 36 and is rapidly expanded in chamber 32. -A low pressure area is created in Port 26 to provide a vacuum suction through port 24 to draw the ilowing laser gas tberethrough where it is drawn into the transducer to be directed to the atmosphere.
In one example an ALr-Vac Modcl AVR-046 vacuum transducer (dimensions on the order of 6 cm x 2.5 cm x 1.5 cm and a mas~ about 0.06 kg) was utiliæed with a pulsed wavegulde T~ la~er whic~l had been previously optimlzed Eor a cavity pressure of about 250 Torr, and a relatively high ga~ flow rate of 1300 cm3/minO Figure 2 indicates thatatmaxlmum supply pressure this flow ' ,
- 2 -3F~ ~ 5 O7 rate can be maintained even with the cavity pressures as low as 200 Torr~ so the transducer has some margin above that needed for this particular applica-tion. The air supply pressure ~7as then reduced to 4~2 kgm/cm2~ and performanceof the laser was found to meet the noted requirements.

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Claims (3)

THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A compact flowing gas laser having pumping-means associated there-with, said laser comprising:
(a) a body having a transverse optical resonant cavity therein and a pair of inlet passages and an outlet passage connected to said cavity in said body;
(b) an active laser medium connected to said inlet passages for flow into said cavity through said inlet passages;
(c) regulating means for regulating the flow of said active medium into said cavity; and, (d) vacuum transducer means for directing said active medium to the atmosphere, said vacuum transducer means including a housing enclosing a body having an orifice therein, an air inlet connected with said body through a first side of said housing, a high pressure source of gas connected to said inlet for flow through said orifice, an enlarged exhaust port opening through a second side of said housing for directing said gas from said orifice to the atmosphere and a port in said housing connected to said outlet passage in said body of said laser, whereby a low pressure area is created in said port as a result of said high pressure gas being expanded in said orifice and said active medium is drawn into said housing and directed to the atmosphere through said exhaust port.
2. Apparatus as in claim 1, wherein said high pressure gas is air.
3. Apparatus as in claim 1, wherein said high pressure gas is N2.
CA000344171A 1979-04-23 1980-01-22 Compact flowing gas system for lasers Expired CA1136250A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US3242179A 1979-04-23 1979-04-23
US32,421 1979-04-23

Publications (1)

Publication Number Publication Date
CA1136250A true CA1136250A (en) 1982-11-23

Family

ID=21864876

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000344171A Expired CA1136250A (en) 1979-04-23 1980-01-22 Compact flowing gas system for lasers

Country Status (1)

Country Link
CA (1) CA1136250A (en)

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