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US4178078A Expired / Lapsed US ⏱️ 0.0 years remaining

Aerodynamic window

Assignee: RTX Corp
•
Filing: 1978-09-19
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Granted: 1979-12-11
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Expires: 1998-09-19
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Abstract

Abstract An apparatus adapted for providing an aerodynamic window having a cylindrical configuration with an annular cross section capable of enveloping annularly a cavity therein is disclosed. The apparatus includes an annular injector adapted for providing a flow of first gas therefrom through a gas path having an annular cross section, an annular collector disposed in a spaced apart relation with the annular injector and adapted for collecting gas flowing through the gas path wherein the annular collector, the annular injector and the gas path cooperate to enclose a cavity therebetween and a gas insertion means for providing a flow of second gas within the cavity. In one embodiment electrodes disposed within the cavity are adapted for enhancing the energy level of the recipient elements of the second gas, as for example by ionization, to produce a high intensity light source. First gas passing through the flow path produces an aerodynamic window having an annular cross section capable of maintaining second gas within the cavity at a desired pressure level.

Inventors

  • 👤 George F. Hausmann

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-31 09:41
CPC Classifications
G; G02; G02B; G02B5/00; H; H01; H01J; H01J61/00; H01J61/02; H01J61/52; H01J61/70; H01J61/80

Claims Analysis

Total Claims: 20
Claim 1
Independent Claim 169 words
An apparatus adapted for providing an aerodynamic window capable of enveloping annularly a cavity therein to maintain a gas within the cavity at a desired pressure comprising: a truncated injector, having an annular configuration symmetrically disposed about a center line axis, adapted for expanding a first gas to supersonic velocity to provide a flow of first gas through a flow path having a cylindrical configuration with an annular cross section; an annular collector, disposed symmetrically about the center line axis in a spaced apart relationship with the truncated injector, having an annular collection duct in flow alignment with the truncated injector and the flow path wherein the annular collector cooperates with the annular injector and the flow path to define a cavity therebetween; and means for providing a flow of second gas into the cavity, said means adapted for maintaining the second gas within the cavity at a desired pressure level while said first gas flows through the flow path to form an aerodynamic window annularly enveloping the cavity.
Claim 2
Independent Claim 169 words
An apparatus adapted for providing an aerodynamic window capable of enveloping annularly a cavity therein to maintain a gas within the cavity at a desired pressure comprising: a truncated injector, having an annular configuration symmetrically disposed about a center line axis, adapted for expanding a first gas to supersonic velocity to provide a flow of first gas through a flow path having a cylindrical configuration with an annular cross section; an annular collector, disposed symmetrically about the center line axis in a spaced apart relationship with the truncated injector, having an annular collection duct in flow alignment with the truncated injector and the flow path wherein the annular collector cooperates with the annular injector and the flow path to define a cavity therebetween; and means for providing a flow of second gas into the cavity, said means adapted for maintaining the second gas within the cavity at a desired pressure level while said first gas flows through the flow path to form an aerodynamic window annularly enveloping the cavity.
Claim 3
Dependent Claim 147 words
The invention in accordance with claim 1 wherein the truncated injector comprises: an annular plenum chamber having an inlet port adapted for connection to a source of first gas and an annular exit adapted for passing first gas annularly therefrom; a truncated flow duct having a curvilinear configuration with an annular cross section including a first end attachment to and enclosing the annular exit of the plenum chamber and a second end having an annular exit adapted for providing an upstream end of the flow path enveloping the cavity wherein the flow duct has a curvature adapted for providing a flow of first gas through the flow path to the annular collector to form an aerodynamic window defined by the flow path and; a core region, annularly enveloped by the truncated low duct, adapted for accommodating gas handling means for passing a second gas through the cavity.
Claim 4
Dependent Claim 72 words
The invention in accordance with claim 2 wherein the truncated flow duct includes an entrance chamber at the first end having an annular cross section adapted for attachment to the plenum chamber, a supersonic nozzle annularly attached to a downstream end of the entrance chamber and an injection duct attached at one end to the downstream end of the supersonic nozzle and terminating at the second end of the truncated flow duct.
Claim 5
Dependent Claim 19 words
The invention in accordance with claim 2 wherein the truncated flow duct has the configuration of an annular funnel.
Claim 6
Dependent Claim 22 words
The invention in accordance with claim 2 wherein the first end has a diameter larger than the diameter of the second end.
Claim 7
Dependent Claim 79 words
The invention in accordance with claim 2 wherein the truncated flow duct has a curvilinear configuration adapted for providing a flow of first gas through the flow path to form an aerodynamic window capable of supporting a large pressure differential between the pressure of an atmosphere external to the cavity and the pressure of second gas maintained within the cavity wherein the cavity is maintained at a pressure greater than the pressure of the atmosphere external to the cavity.
Claim 8
Dependent Claim 78 words
The invention in accordance with claim 2 wherein the truncated flow duct has a curvilinear configuration adapted for providing a flow of first gas through the flow path to form an aerodynamic window capable of supporting a large pressure differential between the pressure of an atmosphere external to the cavity and the pressure of second gas within the cavity wherein the cavity is maintained at a pressure less than the pressure of the atmosphere external to the cavity.
Claim 9
Dependent Claim 81 words
The invention in accordance with claim 2 wherein the gas handling means is a gas handling assembly extending through the core region into the cavity through an aperture in an end cap enclosing the core region and defining an upstream end of the cavity wherein the gas handling assembly includes a gas inlet passage adapted for passing a second gas through the core region into the cavity and a gas exit passage adapted for passing second gas out of the cavity.
Claim 10
Dependent Claim 27 words
The invention in accordance with claim 8 wherein the gas inlet passage is adapted for passing second gas into the cavity tangentially to the center line axis.
Claim 11
Dependent Claim 27 words
The invention in accordance with claim 1 further including means for enhancing the population of ionized and excited energy states of recipient elements of the second gas.
Claim 12
Dependent Claim 60 words
The invention in accordance with claim 10 wherein the means for enhancing the population of ionized and excited energy states includes a first electrode positioned within the cavity at an upstream end thereof and a second electrode positioned within the cavity at a downstream end thereof wherein the first and second electrodes are adapted for maintaining an electric field therebetween.
Claim 13
Dependent Claim 60 words
The invention in accordance with claim 10 wherein the means for enhancing the population of ionized and excited energy states includes an induction coil symmetrically disposed about the center line axis external to the cavity wherein the induction coil is adapted for providing an electromagnetic field within the cavity capable of enhancing the population of ionized and excited energy states.
Claim 14
Dependent Claim 61 words
The invention in accordance with claim 1 further including: a source of radiation located external to the cavity capable of producing radiation having high intensity; focusing means for focusing the radiation into the cavity to enhance the population of ionized and excited energy states of recipient elements of the second gas to provide a high intensity light source within the cavity.
Claim 15
Dependent Claim 15 words
The invention in accordance with claim 13 wherein the source of radiation is a laser.
Claim 16
Dependent Claim 30 words
The invention in accordance with claim 13 wherein the focusing means is a lens having a cylindrical configuration adapted for focusing the radiation to a focal line within the cavity.
Claim 17
Dependent Claim 30 words
The invention in accordance with claim 13 wherein the focusing means is a lens having a spherical configuration adapted for focusing the radiation to a focal volume within the cavity.
Claim 18
Independent Claim 131 words
The method for forming an annular aerodynamic window comprising: pressurizing a plenum chamber with a first gas; passing the first gas through a truncated annular flow duct having a configuration adapted for providing a flow of first gas through a cylindrical gas path having an annular cross section to form an aerodynamic window capable of maintaining a pressure differential between the pressure of an atmosphere exterior to the cylindrical flow path and the pressure of a second gas interior to the cylindrical flow path; collecting the first gas passing through the annular flow path with an annular collector maintained in flow alignment and in a spaced apart relationship with the annular flow duct wherein the annular collector cooperates with the annular injector at the flow path to enclose a cavity therebetween.
Claim 19
Independent Claim 131 words
The method for forming an annular aerodynamic window comprising: pressurizing a plenum chamber with a first gas; passing the first gas through a truncated annular flow duct having a configuration adapted for providing a flow of first gas through a cylindrical gas path having an annular cross section to form an aerodynamic window capable of maintaining a pressure differential between the pressure of an atmosphere exterior to the cylindrical flow path and the pressure of a second gas interior to the cylindrical flow path; collecting the first gas passing through the annular flow path with an annular collector maintained in flow alignment and in a spaced apart relationship with the annular flow duct wherein the annular collector cooperates with the annular injector at the flow path to enclose a cavity therebetween.
Claim 20
Dependent Claim 49 words
The invention in accordance with claim 17 further including: maintaining a second gas within the cavity; and enhancing the population of ionized and excited energy levels of recipient elements of the second gas to form a light source within the cavity capable of providing radiation having a high intensity.

References Cited (Backward Citations)

US3292028A Cited
US3321265A Cited
US3604789A Cited
US3617928A Cited
US3873939A Cited
US3907409A Cited
US3918800A Cited
US3973218A Cited
US3973217A Cited
US4112388A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1982-12-10 1983-06-11 1983-12-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1986-12-10 1987-06-11 1987-12-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1990-12-10 1991-06-11 1991-12-11 $7700.00 Window Closed / Lapsed

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