US4200819A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Unitary supersonic electrical discharge laser nozzle-channel
Assignee: Boeing Co
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Filing: 1977-09-21
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Granted: 1980-04-29
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Expires: 1997-09-21
Abstract
Abstract The nozzle and laser channel walls for a supersonic electrical discharge gas laser are formed from fully contoured single pieces of dielectric material. The axially symmetric, two-dimensional wall contours of the combined nozzle and laser channel describe a continuous extension of the subsonic flow plenum, into which the gas is initially introduced, and which is located upstream of the combined nozzle-laser channel. A high precision portion of the contour of the combined nozzle-laser channel extends from a beginning point in the nozzle inlet region near the throat to a termination point which is beyond the nozzle exit plane a distance equal to approximately one-half of the nozzle exit height. The high precision portion is a region of continuous curvature supersonic expansion. Beyond the termination point of the continuous curvature region the walls of the combined nozzle-laser channel are flat and diverge at a constant angle, relative to the flow axis of the laser, to the end of the combined nozzle-laser channel. Flat, flush mounted electrodes are positioned in the flat walled section of the laser channel, forming a discharge region with maximum flow density uniformity and minimum boundary layer thickness. In one embodiment, one electrode is a grid, with bars normal to the direction of flow, and is mounted in a laser channel wall section which is capable of rotation.
Inventors
- 👤 Ralph L. Haslund
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-23 14:03
CPC Classifications
H; H01; H01S; H01S3/00; H01S3/09; H01S3/097; H01S3/0979
Claims Analysis
Total Claims: 14
Claim 1
Independent Claim
138 words
A combined nozzle and laser channel apparatus for use in a supersonic electrical discharge laser, comprising: a nozzle portion having an entry plane and an exit plane, and a channel portion contiguous to the nozzle portion, wherein the laser gas mixture enters the nozzle/laser channel at the entry plane of said nozzle portion and flows through the nozzle portion and the laser channel portion, exiting at the downstream edge of said laser channel portion, said exit plane defined as being located at the point along the combined nozzle and laser channel apparatus where the velocity of the flowing gas becomes constant, wherein the contour of said nozzle portion is curved and extends downstream of the exit plane into said laser channel portion a distance equal to one-half of the height of said nozzle portion at the exit plane.
Claim 2
Dependent Claim
138 words
A combined nozzle and laser channel apparatus for use in a supersonic electrical discharge laser, comprising: a nozzle portion having an entry plane and an exit plane, and a channel portion contiguous to the nozzle portion, wherein the laser gas mixture enters the nozzle/laser channel at the entry plane of said nozzle portion and flows through the nozzle portion and the laser channel portion, exiting at the downstream edge of said laser channel portion, said exit plane defined as being located at the point along the combined nozzle and laser channel apparatus where the velocity of the flowing gas becomes constant, wherein the contour of said nozzle portion is curved and extends downstream of the exit plane into said laser channel portion a distance equal to one-half of the height of said nozzle portion at the exit plane.
Claim 3
Dependent Claim
25 words
An apparatus of claim 1, wherein said nozzle portion and said laser channel portion comprise continuous portions of electrically insulating material having no transverse joints.
Claim 4
Dependent Claim
15 words
An apparatus of claim 2, wherein said insulating material is a nonporous, dimensionally stable material.
Claim 5
Dependent Claim
15 words
An apparatus of claim 3, wherein said electrically insulating material is a machinable glass ceramic.
Claim 6
Dependent Claim
91 words
An apparatus of claim 2, wherein said nozzle/laser channel comprises four continuous walls of said electrically insulating material, including top and bottom walls and two side walls connecting said top and bottom walls, wherein the interior surfaces of the top and bottom walls are curved throughout said nozzle portion and into said laser channel portion a distance equal to one-half the height of said nozzle portion at the exit plane thereof, and then diverge at a predetermined angle thereafter, and wherein the interior surfaces of said side walls are substantially flat.
Claim 7
Dependent Claim
14 words
An apparatus of claim 5, wherein said nozzle portion is a continuous curvature nozzle.
Claim 8
Dependent Claim
41 words
An apparatus of claim 6, wherein the angle of divergence of the interior surfaces of said top and bottom walls in said laser channel portion is sufficient to compensate for the viscous flow of the laser gas in said laser channel.
Claim 9
Dependent Claim
33 words
An apparatus of claim 5, including discharge electrodes located in the top and bottom walls of the apparatus, approximately at the point where the curved contour of said top and bottom walls terminates.
Claim 10
Dependent Claim
43 words
An apparatus of claim 8, including means for rotating a portion of one of said top and bottom walls containing one discharge electrode about a line transverse of said laser channel portion and coincident with the upstream edge of said one discharge electrode.
Claim 11
Dependent Claim
24 words
An apparatus of claim 9, wherein said rotating means includes means for controlling the rotation of said portion in increments substantially less than 1°.
Claim 12
Dependent Claim
22 words
An apparatus of claim 10, including means for locking said portion in position when the desired amount of rotation has been achieved.
Claim 13
Dependent Claim
56 words
An apparatus of claim 11, wherein said nozzle portion further includes a throat region, and wherein said top and bottom walls of the nozzle portion have a continuous contour from the entry plane to the throat, and are sufficiently long that the gas flow changes from a laminar to a turbulent flow upstream of said throat.
Claim 14
Dependent Claim
101 words
An apparatus of claim 12, wherein the portion of the nozzle between the entry plane and the throat region is defined as the inlet region, and wherein the contour of said top and bottom walls is characterized by an increasing radius of curvature from the point in the inlet region where the flowing gas has a mach number of 0.75 to the throat of the nozzle, where the gas has a mach number of 1, wherein the increasing radius of curvature is so arranged as to result in the gas having a straight sonic line at the throat of the nozzle.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1983-04-29 | 1983-10-29 | 1984-04-29 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-04-29 | 1987-10-29 | 1988-04-29 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-04-29 | 1991-10-29 | 1992-04-29 | $7700.00 | Window Closed / Lapsed |