US4048586A
Expired / Lapsed
US
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Chemical laser with mixing enhancement device for power improvement
Assignee: Northrop Grumman Space and Mission Systems Corp
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Filing: 1976-01-12
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Granted: 1977-09-13
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Expires: 1996-01-12
Abstract
Abstract An inert diluent such as N 2 , He, Ar, etc., is injected into the reactant streams emerging from the cavity nozzle of a CW, supersonic, laser to increase the cavity power and lower the cavity temperature by enhancing mixing of the reactant stream while maintaining high pressure recovery.
Inventors
- 👤 Arvel B. Witte
- 👤 James E. Broadwell
- 👤 Dale L. Hook
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 02:41
CPC Classifications
H; H01; H01S; H01S3/00; H01S3/09; H01S3/095; H01S3/0951; H01S3/0953
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
196 words
A cavity nozzle for a supersonic CW chemical laser fueled by the reactants (a) atomic fluorine and (b) H 2 D 2 and having a lasing cavity in which said reactants (a) and (b) react, comprising: a nozzle body having parallel linear nozzle passages with each pair of adjacent passages separated by a wall tapering to a narrow trailing edge at the exit ends of said passages for injecting parallel contiguous streams of said reactants (a) and (b) from said passages, respectively, into said cavity along parallel linear paths at supersonic velocity in a manner such that each pair of contiquous streams of said reactants (a) and (b) have an intervening common mixing region; and trip means comprising a plurality of trip fluid injection orifices spaced along each trailing wall immediately adjacent the edge between reactant nozzles with certain of the orifices opening toward one adjacent reactant stream path and the remaining orifices opening toward the other adjacent reactant stream path for injecting inert diluent fluid streams laterally into the respective reactant streams as the latter issue from their nozzle passages to induce turbulent-like fast mixing of the contiguous reactant streams within their respective boundary region.
Claim 2
Dependent Claim
196 words
A cavity nozzle for a supersonic CW chemical laser fueled by the reactants (a) atomic fluorine and (b) H 2 D 2 and having a lasing cavity in which said reactants (a) and (b) react, comprising: a nozzle body having parallel linear nozzle passages with each pair of adjacent passages separated by a wall tapering to a narrow trailing edge at the exit ends of said passages for injecting parallel contiguous streams of said reactants (a) and (b) from said passages, respectively, into said cavity along parallel linear paths at supersonic velocity in a manner such that each pair of contiquous streams of said reactants (a) and (b) have an intervening common mixing region; and trip means comprising a plurality of trip fluid injection orifices spaced along each trailing wall immediately adjacent the edge between reactant nozzles with certain of the orifices opening toward one adjacent reactant stream path and the remaining orifices opening toward the other adjacent reactant stream path for injecting inert diluent fluid streams laterally into the respective reactant streams as the latter issue from their nozzle passages to induce turbulent-like fast mixing of the contiguous reactant streams within their respective boundary region.
Claim 3
Dependent Claim
32 words
A supersonic chemical laser cavity nozzle according to claim 1 wherein said trip fluid injection orifices along each wall trailing edge open toward the respective adjacent reactant stream paths in alternate sequence.
Claim 4
Dependent Claim
35 words
A supersonic chemical laser cavity nozzle according to claim 1 wherein said trip means comprises a trip tube extending along and secured to each trailing wall edge and containing the respective trip fluid injection orifices.
Claim 5
Dependent Claim
32 words
A supersonic chemical laser cavity nozzle according to claim 3 wherein said trip fluid injection orifices along each wall trailing edge open toward the respective adjacent reactant stream paths in alternate sequence.
Claim 6
Dependent Claim
66 words
A supersonic chemical laser cavity nozzle according to claim 1 wherein each nozzle all has convergent sides bounding the adjacent nozzle passages, respectively; and said trip means comprises a trip fluid passage extending through each wall between its sides and lengthwise of its trailing edge, and communicating with the respective trip fluid injection orifices, and said trip orifices in each wall open through said wall sides.
Claim 7
Dependent Claim
32 words
A supersonic chemical laser cavity nozzle according to claim 5 wherein said trip fluid injection orifices along each wall trailing edge open toward the respective adjacent reactant stream paths in alternate sequence.
Claim 8
Independent Claim
168 words
The method of mixing the reactants (a) atomic fluorine and (b) H 2 or D 2 in a supersonic CW chemical laser having a lasing cavity in which said reactants (a) and (b) react comprising the steps of injecting contiguous parallel streams of said reactants (a) and (b) into said lasing cavity at supersonic velocity through parallel linear nozzle passages of a nozzle having a wall separating each pair of adjacent passages and tapering to a narrow trailing edge at the exit ends of said passages in a manner such that each pair of contiguous streams of said reactants (a) and (b) have an intervening common mixing region; and injecting trip fluid streams of an inert diluent fluid through trip fluid injection orifices spaced along each trailing wall immediately adjacent the edge of said nozzle laterally into the adjacent contiguous reactant streams as the latter issue from their nozzle passages to induce turbulent-like fast mixing of the continguous streams within the mixing region of the respective contiguous streams.
Claim 9
Independent Claim
168 words
The method of mixing the reactants (a) atomic fluorine and (b) H 2 or D 2 in a supersonic CW chemical laser having a lasing cavity in which said reactants (a) and (b) react comprising the steps of injecting contiguous parallel streams of said reactants (a) and (b) into said lasing cavity at supersonic velocity through parallel linear nozzle passages of a nozzle having a wall separating each pair of adjacent passages and tapering to a narrow trailing edge at the exit ends of said passages in a manner such that each pair of contiguous streams of said reactants (a) and (b) have an intervening common mixing region; and injecting trip fluid streams of an inert diluent fluid through trip fluid injection orifices spaced along each trailing wall immediately adjacent the edge of said nozzle laterally into the adjacent contiguous reactant streams as the latter issue from their nozzle passages to induce turbulent-like fast mixing of the continguous streams within the mixing region of the respective contiguous streams.
Claim 10
Dependent Claim
28 words
The mixing method of claim 7 wherein said trip fluid injection orifices along each nozzle wall trailing edge open toward the adjacent contiguous reactant streams in alternate sequence.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1980-09-12 | 1981-03-14 | 1981-09-13 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1984-09-12 | 1985-03-14 | 1985-09-13 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1988-09-12 | 1989-03-14 | 1989-09-13 | $7700.00 | Window Closed / Lapsed |