US 4,942,653 A · Production method for a channeled wall thrust nozzle

Abstract

An improved method of manufacture is provided for producing a channeled wall thrust nozzle (10) of the type used to define a thrust chamber (12) in a jet or rocket engine. The method utilizes a precision formed mandrel (20) having an external geometry conforming generally to the converging-diverging shape of the desired thrust chamber (12), and further including longitudinally extending slots (24) for receiving channel separation ribs (26) which may be formed by die cutting from sheet stock. The channel spaces (16) between the separator ribs (26) are filled with a removable casting material (30) such as wax, and an outer housing shell (32) for the thrust nozzle is mounted about and secured to the separator ribs. The mandrel (20), which is transversely split at the throat of the thrust chamber (12), is then removed to expose the radially inboard margins of the separator ribs (26) for precision machining, followed by mounting of an inner housing shell (34) to the separator ribs. The casting material (30) is then removed from the resultant thrust nozzle (10) to leave precision process fluid channels (16) formed between the inner and outer housing shells.

Claims18

Dependent claims

A method of forming a channeled wall thrust nozzle defining a converging-diverging thrust chamber, said method comprising the steps of:

forming a mandrel having a longitudinal converging-diverging cross-section and a transverse cross-section generally conforming respectively with the geometry of the thrust chamber to be formed, the mandrel being transversely split at a narrow diameter throat of the converging-diverging cross-section, thereby defining longitudinally separable mandrel components, said mandrel forming step further including forming an array of longitudinally extending slots in an exterior surface of the mandrel;
seating a plurality of channel separator ribs individually within the mandrel slots which project outwardly therefrom, thereby defining a plurality of longitudinally extending channels between the ribs;
filling the channels with a removable casting material;
mounting an outer housing shell to outboard edge margins of the channel separator ribs, thereby enclosing outboard sides of the channels;
removing the mandrel from the channel separator ribs by longitudinally separating the mandrel components;
tailoring inboard edge margins of the channel separator ribs to a selected geometry;
mounting an inner housing shell to the inboard edge margins of the channel separator ribs, thereby enclosing inboard sides of the channels;
and
removing the casting material from the channels.

6 more elements

A method of forming a channeled wall thrust nozzle defining a converging-diverging thrust chamber, said method comprising the steps of:

providing a mandrel having a longitudinal converging-diverging cross-section conforming generally with the converging-diverging geometry of the thrust chamber to be formed, a generally circular transverse cross-section having a diametric size slightly less than the diametric size of the thrust chamber to be formed, a transverse split at a narrow diameter throat thereby defining longitudinally separable mandrel components, and an exterior array of circumferentially spaced and longitudinally extending slots each having a longitudinal profile conforming generally with the converging-diverging geometry of the thrust chamber to be formed;
seating a plurality of channel separator ribs individually into the slots which project radially outwardly from the slot, the ribs having inboard and outboard edge margins conforming generally to the converging-diverging geometry of the thrust chamber to be formed and defining therebetween a circumferentially spaced plurality of longitudinal channels;
filling the channels with a removable casting material;
mounting an outer housing shell to the outboard edge margins of the channel separator ribs;
removing the mandrel from the channel separator ribs and the casting material by longitudinally separating the mandrel components;
tailoring the inboard edge margins of the channel separator ribs to a selected geometry conforming generally with the converging-diverging geometry of the thrust chamber to be formed, said tailoring step including machining at least slightly into the casting material;
mounting an inner housing shell to the inboard edge margins of the channel separator ribs;
and
removing the casting material from the channels

6 more elements

Dependencies are inferred from the claim text.

Production method for a channeled wall thrust nozzle

Life of this patent

Production method for a channeled wall thrust nozzle

Life of this patent

Abstract

Claims18