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US4559628A Expired / Lapsed US ⏱️ 0.0 years remaining

Shear layer control in a free-vortex aerodynamic window

Assignee: RTX Corp
•
Filing: 1983-04-26
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Granted: 1985-12-17
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Expires: 2003-04-26
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Abstract

Abstract A boundary-controlled aerodynamic window positioned adjacent the exit aperture of a gas laser is transparent to the laser beam emitted from the cavity of the laser. The boundary-controlled aerodynamic window is formed by a high velocity gas flow directed by a duct across the exit aperture for the laser beam isolating the low pressure region of the cavity from the high pressure of the atmosphere. The exit aperture is enlarged and an auxiliary gas flow injected along the sidewall of the duct adjacent the exit aperture to expand the thickness of the boundary layer. In a second embodiment, particulate matter is fixedly attached to the sidewall of the duct to increase the roughness of the wall surface. A third embodiment uses a plurality of nozzles, each injecting gas with a predetermined velocity.

Inventors

  • 👤 Bruce V. Johnson
  • 👤 Roy N. Guile

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 11:06
CPC Classifications
H; H01; H01S; H01S3/00; H01S3/02; H01S3/03; H01S3/034; H01S3/0343

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 84 words
An aerodynamic window for use with a gas laser, comprising: housing means in which said gas laser is positioned, including an exit aperture from which said laser beam passes; means including a duct for directing a high velocity gas flow across said exit aperture providing a barrier to isolate the cavity of said gas laser from the atmosphere; and means along said duct for increasing the thickness of the shear boundary layer so that eddies and density variations in the transparent window are minimized.
Claim 2
Dependent Claim 84 words
An aerodynamic window for use with a gas laser, comprising: housing means in which said gas laser is positioned, including an exit aperture from which said laser beam passes; means including a duct for directing a high velocity gas flow across said exit aperture providing a barrier to isolate the cavity of said gas laser from the atmosphere; and means along said duct for increasing the thickness of the shear boundary layer so that eddies and density variations in the transparent window are minimized.
Claim 3
Dependent Claim 42 words
An aerodynamic window according to claim 1, wherein said means along said duct for increasing the thickness of said shear layer thickness is a porous wall through which an auxiliary gas flow is directed to increase the thickness of the shear layer.
Claim 4
Dependent Claim 32 words
An aerodynamic window according to claim 1, wherein said means for increasing the thickness of said shear layer is a plurality of particulate matter fixedly attached to said sidewall of said duct.
Claim 5
Dependent Claim 44 words
An aerodynamic window according to claim 1, wherein said means along said duct for increasing the thickness of said shear layer is one or more jets positioned along the sidewall of said duct for directing an auxiliary gas flow into said main flow stream.

References Cited (Backward Citations)

US3617928A Cited
US3654569A Cited
US3873939A Cited
US3973218A Cited
US4152672A Cited
US4207542A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1988-12-16 1989-06-17 1989-12-17 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1992-12-16 1993-06-17 1993-12-17 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1996-12-16 1997-06-17 1997-12-17 $7700.00 Window Closed / Lapsed

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