Method of forming a reinforcing layer on the inner wall of the combustion and/or thrust nozzles for a liquid rocket engine

Claim 1

A method of forming the combustion chamber and/or thrust nozzle of a liquid rocket engine having an inner wall and an outer wall with laterally spaced cooling ducts located between the inner wall and outer wall and formed by shaping the inner wall with laterally spaced inwardly extending projections forming troughs closed by the outer wall and the inwardly facing surface of the inner wall having a corrugated-like shape, comprising the steps of electroplating a layer on a core having the negative form of the inner wall with the troughs formed therein for forming the inner wall with the cooling ducts, and removing the core, wherein the improvement comprises, after the removal of the core, electroplating a reinforcing layer at least on the radially inwardly projecting portions of the inner surface of the inner wall the radially outer surfaces of which projecting portions in combination with the radially inwardly facing surfaces of said outer wall define the cooling ducts, and effecting the electroplating by positioning the inner wall within an electrolytic bath and locating a material-depositing electrode within the bath equidistantly spaced radially inwardly of the inner wall.

Claim 2

A method of forming the combustion chamber and/or thrust nozzle of a liquid rocket engine having an inner wall and an outer wall with laterally spaced cooling ducts located between the inner wall and outer wall and formed by shaping the inner wall with laterally spaced inwardly extending projections forming troughs closed by the outer wall and the inwardly facing surface of the inner wall having a corrugated-like shape, comprising the steps of electroplating a layer on a core having the negative form of the inner wall with the troughs formed therein for forming the inner wall with the cooling ducts, and removing the core, wherein the improvement comprises, after the removal of the core, electroplating a reinforcing layer at least on the radially inwardly projecting portions of the inner surface of the inner wall the radially outer surfaces of which projecting portions in combination with the radially inwardly facing surfaces of said outer wall define the cooling ducts, and effecting the electroplating by positioning the inner wall within an electrolytic bath and locating a material-depositing electrode within the bath equidistantly spaced radially inwardly of the inner wall.

Claim 7

A method for the production of the combustion chamber and/or thrust nozzle of a liquid rocket engine having an inner wall and an outer wall with laterally spaced cooling ducts located between the inner wall and outer wall and formed by shaping the inner wall with laterally spaced inwardly extending projections forming troughs closed by the outer wall with the inwardly directed surface of the projections having a corrugated-like shape, comprising the steps of electroplating a layer on a core having the negative form of the inner wall with the troughs for forming the inner wall with the cooling ducts, filling the troughs with electrically conductive material, electroplating the outer wall on the inner wall so that the outer wall spans the troughs forming the cooling ducts, removing the electrically conductive material from within the cooling ducts, removing the core from the inner walls, wherein the improvement comprises, after the removal of the core, electroplating a reinforcing layer at least on the radially inwardly projecting portions of the inner surface of the inner wall which projections define the cooling ducts and effecting the electroplating by positioning the inner wall with its central axis extending vertically and supporting the inner wall for rotation about its central axis, locating the material-depositing electrode along the central axis of the inner wall with the electrode extending upwardly from the lower end of the inner wall for only a portion of the axial length of the inner wall, submerging the inner wall into the electrolytic bath to a selected level intermediate its ends, commencing the electroplating operation and during the electroplating operation continuously moving the inner wall axially for a selected distance to provide an axially extending tapering reinforcing layer to the inwardly facing surface of the inner wall.

Claim 8

A method for the production of the combustion chamber and/or thrust nozzle of a liquid rocket engine having an inner wall and an outer wall with laterally spaced cooling ducts located between the inner wall and outer wall and formed by shaping the inner wall with laterally spaced inwardly extending projections forming troughs closed by the outer wall with the inwardly directed surface of the projections having a corrugated-like shape, comprising the steps of electroplating a layer on a core having the negative form of the inner wall with the troughs for forming the inner wall with the cooling ducts, filling the troughs with electrically conductive material, electroplating the outer wall on the inner wall so that the outer wall spans the troughs forming the cooling ducts, removing the electrically conductive material from within the cooling ducts, removing the core from the inner walls, wherein the improvement comprises, after the removal of the core, electroplating a reinforcing layer at least on the radially inwardly projecting portions of the inner surface of the inner wall which projections define the cooling ducts and effecting the electroplating by positioning the inner wall with its central axis extending vertically and supporting the inner wall for rotation about its central axis, locating the material-depositing electrode along the central axis of the inner wall with the electrode extending upwardly from the lower end of the inner wall for only a portion of the axial length of the inner wall, submerging the inner wall into the electrolytic bath to a selected level intermediate its ends, commencing the electroplating operation and during the electroplating operation continuously moving the inner wall axially for a selected distance to provide an axially extending tapering reinforcing layer to the inwardly facing surface of the inner wall.