Nozzle particularly for lasers
AssigneeRockwell International Corporation
InventorDonald H. Morris
Life of this patent
Estimating the term…
Abstract
A plurality of arcuate, secondary (fuel) nozzle members are juxtaposed, so that respective two of them define between them a curved, primary slit nozzle, producing a primary (oxidizer) expansion flow while the two flows mix downstream, predominantly transversely to the expansion. The nozzle members are mounted in the aperture of a plate; large-scale assemblies are described.
Claims24
A nozzle structure for combining two gas components in a cavity comprising a plurality of first nozzle means for providing a diverging expansion flow of a first gas component into the cavity, the expansion occurring predominantly in a first direction, being angular to an average flow direction from each of the first nozzle means;
- and
- a plurality of second nozzle means respectively interposed between the nozzle means of the first plurality to provide a flow of the second component along the flow of the first component, so that mixing between the flows occurs predominantly in a second direction, being angular to said first direction and to said average flow direction.
In a chemical laser, a nozzle construction, comprising:
- a primary nozzle, having (i) an arcuate slit-like throat, (ii) two mutually inclined end walls respectively at two opposite ends of the slit-like throat, and (iii) side walls terminating radially outwardly from the slit-like throat in an arcuate exit plane being concentric to the slit-like throat, in order to obtain a supersonic, expanding primary flow in the nozzle and flow expansion downstream from the exit plane, the flow expanding predominantly in a plane traversing and being normal to the slit and to the curved exit plane;
- and
- secondary nozzle means in said exit plane and disposed alongside the primary nozzle means and directing secondary jet flow in different radially outward directions corresponding to the curvature of the arcuate exit plane, the primary and secondary jet flows mixing in directions transversely to said plane traversing the throat and the exit plane.
In a chemical laser, a nozzle structure for mixing oxidizer and fuel, comprising:
- primary nozzle means for providing an expansion flow of oxidizer in different directions;
- and
- secondary arcuate nozzle means, providing a flow of fuel also in the different directions and being positioned so that fuel and oxidizer mix in an expansion flow field of the oxidizer flow and predominantly in directions angular to said different directions, said primary and secondary nozzle means having a common, curved, cylindrically shaped exit plane.
In a chemical laser, a separting construction between a first oxidizer preparation chamber and a second, optical laser cavity, comprising:
- frame means defining at least one rectangular aperture;
- a plurality of arcuate members inserted in the aperture in parallel, side-by side relationship, leaving nozzle slits in between, facing said first chamber, and establishing primary nozzles for directing supersonic oxidizer flow into the second chamber;
- aperture means in the arcuate members defining fuel nozzles oriented in different directions on account of the arcuate configuration of the members, the arcuate members further including duct means for feeding the aperture means;
- and
- manifold means in the frame means for feeding the fuel to the duct means of the members.
In a chemical laser, a nozzle construction for feeding oxidizer and fuel into an optical laser cavity, the combination comprising:
- at least two arcuate members disposed for curving in two parallel planes and defining an expansion nozzle for the oxidizer, the expansion occurring predominantly in said planes;
- and
- aperture means in each one of the said members for the discharge of the fuel gas component also in and parallel to said planes, so that the fuel and oxidizer mix in directions normal to said planes.
In a chemical laser, a nozzle structure for combining oxidizer and fuel gases in an optical cavity in which the gases undergo a chemical reaction, comprising:
- a plurality of first nozzle means for providing a diverging expansion flow of an oxidizer into the cavity, the expansion occurring predominantly in a first direction, being angular to an average flow direction from each of the first nozzle means;
- and
- a plurality of second nozzle means respectively interposed between the nozzle means of the first plurality in order to provide the flow of a fuel gas along the flow of the ozidizer, so that mixing between the flows occurs predominantly in a second direction, being angular to said first direction and to said average flow direction.
A nozzle structure for mixing two gases, comprising:
- primary nozzle means for providing an expansion flow of a first one of the gases, the expansion occurring in different directions;
- and
- secondary arcuate nozzle means, providing a flow of a second one of the gases also in different directions and being positioned, so that the two gases mix in an expansion flow field of the flow of the first gas and predominantly in directions angular to said different directions, said primary and secondary nozzle means having a common, curved, cylindrically shaped exit plane.
Dependencies are inferred from the claim text.