Aerodynamic window method and apparatus

Claim 3

A method of producing an aerodynamic window according to claim 1 wherein the multiple component aerodynamic window gas stream is produced with an intermediate shear zone between said two separate gas stream components and with said two separate gas components having approximately the same velocity adjacent said intermediate shear zone to reduce the thickness thereof.

Claim 4

A method of producing an aerodynamic window according to claim 1 wherein the two different gas regions have substantially different molecular weights and wherein each of the two separate gas stream components has approximately the same molecular weight as the respective adjacent gas region.

Claim 5

A method of producing an aerodynamic window according to claim 1 wherein the two separate gas stream components have approximately the same composition and have substantially different stagnation temperatures to produce said different stagnation indices of refraction.

Claim 6

In an aerodynamic window system for producing an aerodynamic window between the first and second separate gas regions with substantially different static pressures and indices of refraction and comprising first conduit means for connecting the separate gas regions and providing an unobstructed optical beam transmission passageway therebetween, and aerodynamic window producing means having second conduit means intersecting the first conduit means and operable for discharging a high velocity gas medium across the optical beam transmission passageway to produce an aerodynamic window for preventing substantial gas flow through the passageway between said gas regions, the improvement wherein the second conduit means provides first and second separate passageways upstream of the aerodynamic window for discharging first and second different aerodynamic window gas medium components respectively at high velocity across the optical beam transmission passageway and at opposite sides of the aerodynamic window adjacent to said first and second gas regions respectively, and wherein the aerodynamic window producing means provides for discharging through the first and second separate passageway sections, said first and second gas medium components respectively having substantially different stagnation indices of refraction which are generally the same as the different indices of refraction of said first and second gas regions respectively, and so as to produce a said aerodynamic window with turbulent shear zones on opposite sides thereof having substantially uniform stagnation indices of refraction respectively.

Claim 7

In an aerodynamic window system for producing an aerodynamic window between the first and second separate gas regions with substantially different static pressures and indices of refraction and comprising first conduit means for connecting the separate gas regions and providing an unobstructed optical beam transmission passageway therebetween, and aerodynamic window producing means having second conduit means intersecting the first conduit means and operable for discharging a high velocity gas medium across the optical beam transmission passageway to produce an aerodynamic window for preventing substantial gas flow through the passageway between said gas regions, the improvement wherein the second conduit means provides first and second separate passageways upstream of the aerodynamic window for discharging first and second different aerodynamic window gas medium components respectively at high velocity across the optical beam transmission passageway and at opposite sides of the aerodynamic window adjacent to said first and second gas regions respectively, and wherein the aerodynamic window producing means provides for discharging through the first and second separate passageway sections, said first and second gas medium components respectively having substantially different stagnation indices of refraction which are generally the same as the different indices of refraction of said first and second gas regions respectively, and so as to produce a said aerodynamic window with turbulent shear zones on opposite sides thereof having substantially uniform stagnation indices of refraction respectively.

Claim 8

In a laser generator having an unobstructed laser transmission passageway connecting two separate gas regions with substantially different static pressures and indices of refraction, and aerodynamic window producing means for producing an aerodynamic window across the laser transmission passageway between said two separate gas regions for preventing substantial gas flow therebetween through the laser transmission passageway, the improvement wherein the aerodynamic window gas stream producing means produces a said aerodynamic window with at least two different high velocity gas stream components across the laser transmission passageway on opposite sides of the aerodynamic window adjacent to and forming turbulent shear zones with the two gas regions respectively and having substantially different stagnation indices of refraction generally the same as the different indices of refraction of the corresponding gas regions respectively and so as to form turbulent shear zones therewith respectively, each having a generally uniform stagnation index of refraction.

Claim 9

In a laser generator having an unobstructed laser transmission passageway connecting two separate gas regions with substantially different static pressures and indices of refraction, and aerodynamic window producing means for producing an aerodynamic window across the laser transmission passageway between said two separate gas regions for preventing substantial gas flow therebetween through the laser transmission passageway, the improvement wherein the aerodynamic window gas stream producing means produces a said aerodynamic window with at least two different high velocity gas stream components across the laser transmission passageway on opposite sides of the aerodynamic window adjacent to and forming turbulent shear zones with the two gas regions respectively and having substantially different stagnation indices of refraction generally the same as the different indices of refraction of the corresponding gas regions respectively and so as to form turbulent shear zones therewith respectively, each having a generally uniform stagnation index of refraction.