Two-piece aft closure for a rocket motor case
AssigneeAerojet-General Corporation
InventorsWilliam M. Wallace, Michael T. Gagne, Chester A. Copperthite
Life of this patent
Estimating the term…
Abstract
An aft closure assembly manufactured from two separate and distinct pieces made from different materials is provided for a rocket motor case. The aft closure assembly includes at least a retaining ring piece made from a first material similar to or having a coefficient of thermal expansion similar to that of the motor case. The aft closure assembly includes a blast tube and closure piece that can be manufactured from a second material that does not need to be similar to nor have a coefficient of thermal expansion similar to the motor case and retaining ring piece. This is possible because the blast tube and closure piece includes a face seal that seals against a face of the retaining ring.
Claims28
A system for sealing a rocket motor case to an aft closure assembly, wherein the aft closure assembly comprises a retaining ring piece and a closure piece, comprising:
- (a) a retaining ring made from a material having a coefficient of expansion similar to the rocket motor case material, the retaining ring piece having a first seal to seal between an outer surface of the retaining ring and the inner surface of the rocket motor case;
- and
- (b) a closure made from a material having a coefficient of expansion different to the coefficient of expansion of the retaining ring, the closure stationarily connected to a fixed location on the retaining ring, the closure having a second seal to seal between the closure and a face of the retaining ring;
- (c) wherein the face of the retaining ring that is sealed by the second seal is orthogonal to the outer surface of the retaining ring.
A system for sealing a rocket motor case, comprising a retaining ring inside the rocket motor case, the retaining ring having a proximal end and a distal end, a radial seal to seal between an inside surface of the rocket motor case and the retaining ring, and a closure having a face seal to seal between a distal facing surface of the closure and a proximal facing surface at the proximal end of the retaining ring, the closure connected to a fixed location on the retaining ring, wherein the face seal is maintained as the closure moves relative to the retaining ring.
An aft closure assembly for a rocket motor case, comprising:
- (a) a retaining ring piece inside the rocket motor case and having a first seal around the outer circumference that seals against an inner circumference of the rocket motor case, the retaining ring piece stationarily attached to the motor case;
- and
- (b) an aft closure piece comprising a blast tube, the closure piece stationarily attached to the retaining ring piece and having a second seal on a face of the retaining ring piece to seal between the retaining ring piece and the closure piece, wherein the rocket motor case is open to the exterior via the blast tube.
A system for sealing a rocket motor case having an opening, comprising:
- (a) a retaining ring on the inside of the rocket motor case to seal between the rocket motor case and the retaining ring;
- and
- (b) a closure connected to the retaining ring, the closure having a surface orthogonal to the outside circumference of the retaining ring to seal between an end face of the retaining ring and the orthogonal surface, wherein the orthogonal surface contacts the end face and is configured to move radially relative to the end face of the retaining ring, and wherein the closure includes an aperture that provides an opening from the interior of the rocket motor case to the exterior.
An aft closure assembly for a rocket motor case, comprising:
- (a) a retaining ring piece inside the rocket motor case having a first seal to seal between an outer surface of the retaining ring piece and an interior surface of a rocket motor case, wherein the first seal is maintained as the retaining ring moves relative to the rocket motor case and the retaining ring piece is stationarily attached to the motor case;
- and
- (b) an aft closure piece comprising a blast tube, the closure piece stationarily connected to a fixed location on the retaining ring piece, the closure piece having a distal face formed by a circular flange at the proximal end thereof, the distal face having a second seal to seal between the distal face and a proximal end face of the retaining ring, the proximal end face of the retaining ring in contact with the distal face of the closure piece;
- (c) wherein the proximal end face of the retaining ring piece that is sealed by the second seal is orthogonal to the outer surface of the retaining ring piece, and the second seal is maintained as the closure piece moves radially relative to the retaining ring piece;
- and
- (d) wherein the retaining ring piece is made from a material having a first coefficient of thermal expansion similar to the rocket motor case material, and the closure piece is made from a material having a second coefficient of thermal expansion that is different than the first coefficient of thermal expansion.
Dependencies are inferred from the claim text.