PatentVote.com: Vote on your favourite invention!

Next ten patents ordered by date:
Translate:
En
De
Es
Fr
It
Pt
Ja
Ko
Zh 

 

Title: Subsonic flow aerodynamic window for high energy laser



Do you think this is a good invention? Vote now:

 Votes so far: For:(0) Against:(0)
Claims: What is claimed is:

1. A subsonic flow aerodynamic window in a high energy gas laser, which seals off the laser optical cavity from the ambient gas while minimizing the degradation of the laser output beam, comprising:

a gas laser for providing a laser beam including a laser cavity and an outlet chamber for said beam to traverse;

an entrance in said chamber for receiving said laser beam from said laser cavity;

means connected to a flow system for providing a gas for producing a subsonic gas jet flowing transversely to said laser output beam for sealing off said chamber from the ambient gas with reduced degradation of said output laser beam;

an exhaust duct transverse to said chamber for exhausting said gas jet;

convergent nozzle for acceleration of the gas to provide said subsonic flow; and

a plurality of plates and screens positioned in said cavity between said means and said convergent nozzle for reducing the turbulence of the gas jet.

2. A subsonic flow aerodynamic window in a high energy gas laser, which seals off the laser optical cavity from the ambient gas comprising:

means for providing a laser beam;

a gas laser power amplifier;

said amplifier including a laser cavity for amplifying said laser beam;

an inlet chamber for said beam to enter said cavity;

an outlet chamber for said beam to exist said cavity;

a duct in said chamber for receiving said beam;

means connected to a flow system for providing a gas for producing a subsonic gas jet flowing transversely to said laser beam for sealing off said cavity from the ambient gas with reduced degradation of said laser beam;

an exhaust duct transverse to said cavity for exhausting said gas jet;

a convergent nozzle for acceleration of the gas to provide said subsonic flow; and

a plurality of plates and screens positioned in said cavity between said means and said convergent nozzle for reducing the turbulance of the gas jet.

Other info:


Inventors: Kallis, James M. (Los Angeles, CA, US)

Application Number: 455437
Filing Date: 1974-03-27
Publication_date: 1976-02-03
Assignee: Hughes Aircraft Company (Culver City, CA)
Primary Class(es): 372/104 359/894
Other Classes:
US Patent Ref:
3617928Nov, 1971Hausmann331/94.
3654569Apr, 1972Hausmann331/94.
3768035Oct, 1973Zar331/94.

Other Refs:
Primary Examiner: Sikes, William L.
Assistant Examiner:
Attorney: MacAllister, Jr.; W. H., Kozem; F. I.