Combined warm gas fin and reaction control servo

Claim 2

A reaction nozzle and movable fin servo system for providing reaction and fin directional control of a missile during low and high velocity flight phases, comprising: a gas generator having a stepped flow rate that is high shortly after ignition and low during sustaining operation, a plurality of independent actuator means each coupled to a movable fin for controlling the aerodynamic lift orientation of the latter, a control valve means for controlling gas flow to each actuator means, each actuator means including diversion valve means for controlling gas flow to reaction nozzles, a manifold having flow passages to duct gas from the gas generator to each control valve means and each diversion valve means, and a pressure responsive valve means controlling the gas flow through the flow passages connecting the gas generator and the diversion valve means, the pressure responsive valve means being open in response to relatively high manifold pressure during high gas flow rate permitting full flow to the diversion valve means and normally being closed during low gas flow rate.

Claim 3

A reaction nozzle and movable fin servo system according to claim 1, in which: each actuator means comprises a double acting piston housed within a cylinder, and each control valve means comprises a solenoid actuated ported valve having an inlet port, a cylinder port and a vent port, the ported valve being constructed and arranged to permit gas flow from the gas generator to the cylinder while blocking the vent port or to permit flow from the cylinder to the vent port while blocking the inlet port.

Claim 4

A reaction nozzle and movable fin servo system according to claim 1, in which: each actuator means comprises a double-acting piston housed within a cylinder, one end of the cylinder being in communication with the gas generator through the control valve means and the other end through a control valve means bypass passage whereby the latter end is pressurized continuously when the gas generator is operative, the piston area on the end of the piston acted upon by the pressurized gas entering the cylinder through the control valve means being proportioned relative to the area of the piston acted upon by the pressurized gas received through the bypass passage so that essentially equal force is obtainable in either direction of movement of the piston.

Claim 5

A reaction nozzle and movable fin servo system according to claim 3, in which: each control valve means comprises a solenoid actuated ported valve having an inlet port, a cylinder port and a vent port, the ported valve having a poppet positionable by a solenoid to permit gas flow from the gas generator through the inlet port and the cylinder port to the cylinder while blocking flow through the vent port or to permit flow from the cylinder through the cylinder port and vent port while blocking the inlet port.

Claim 6

A reaction nozzle and movable fin servo system according to claim 1, in which: each actuator means comprises a double-acting piston housed within a cylinder, each piston being coupled to a movable fin by a piston rod, the cylinder having a main chamber in which the piston is reciprocable and a cylindrical extension encompassing the piston rod for a substantial portion of the length of the latter, and the diversion valve means for each actuator means comprises spool valve means mounted on the piston rod within the cylindrical extension of the cylinder, the spool valve means being movable to block gas flow through the cylindrical extension to selected reaction nozzles in synchronism with the movement of the movable fins by the piston and piston rod.

Claim 7

A reaction nozzle and movable fin servo system according to claim 5, in which: one end of the main chamber of the cylinder is in communication with the gas generator through the control valve means and the other end through a control valve means bypass passage whereby the latter end is continuously pressurized when the gas generator is operative, the piston area on the piston end acted upon by the pressurized gas entering the cylinder through the control valve means being proportioned relative to the area of the piston end acted upon by the pressurized gas received through the bypass so that essentially equal force is obtainable in either direction of movement of the piston.

Claim 8

A reaction nozzle and movable fin servo system according to claim 6, in which: each control valve means comprises a solenoid actuated ported valve having an inlet port, a cylinder port and a vent port, the ported valve having a poppet positionable by a solenoid to permit gas flow from the gas generator sequentially through the inlet port and the cylinder port to the cylinder while blocking flow through the vent port or to permit gas flow from the cylinder sequentially through the cylinder port and vent port while blocking the inlet port.

Claim 9

A servo system for controlling the flight trajectory of a missile during its low and high velocity flight phases by selective operation of a plurality of reaction nozzles and pivotally mounted fin means, comprising: a stepped flow rate gas generator providing high pressure gas flow shortly after ignition and low pressure gas flow during sustaining operation, manifold means for distributing the gas through a plurality of primary and secondary passageways, a plurality of independent actuator means each in communication with a primary manifold passageway and linked to a movable fin means for controlling the missile steering orientation of the latter, and a control valve means in each primary passageway for controlling gas flow to the actuator means in communication with the latter, each actuator means including a diversion valve means for controlling gas flow from secondary passageways to the reaction nozzles, and a pressure responsive valve means controlling the gas flow from the gas generator simultaneously to all of the secondary passageways in communication with the diversion valves, the pressure responsive valve means being open during high gas flow rate whereby the reaction nozzles and movable fins coact to guide the missile during the low velocity flight phase and being closed during low gas flow rate whereby the missile is guided solely by the movable fins during the high velocity flight phase.

Claim 10

A servo system for controlling the flight trajectory of a missile during its low and high velocity flight phases by selective operation of a plurality of reaction nozzles and pivotally mounted fin means, comprising: a stepped flow rate gas generator providing high pressure gas flow shortly after ignition and low pressure gas flow during sustaining operation, manifold means for distributing the gas through a plurality of primary and secondary passageways, a plurality of independent actuator means each in communication with a primary manifold passageway and linked to a movable fin means for controlling the missile steering orientation of the latter, and a control valve means in each primary passageway for controlling gas flow to the actuator means in communication with the latter, each actuator means including a diversion valve means for controlling gas flow from secondary passageways to the reaction nozzles, and a pressure responsive valve means controlling the gas flow from the gas generator simultaneously to all of the secondary passageways in communication with the diversion valves, the pressure responsive valve means being open during high gas flow rate whereby the reaction nozzles and movable fins coact to guide the missile during the low velocity flight phase and being closed during low gas flow rate whereby the missile is guided solely by the movable fins during the high velocity flight phase.

Claim 11

A servo system according to claim 8, in which: each actuator means comprises a double acting piston housed within a cylinder, and each control valve means comprises a solenoid actuated ported valve having an inlet port, a cylinder port and a vent port, the ported valve being constructed and arranged to permit gas flow from the gas generator to the cylinder while blocking the vent port or to permit flow from the cylinder to the vent port while blocking the inlet port.

Claim 12

A servo system according to claim 8, in which: each actuator means comprises a double-acting piston housed within a cylinder, one end of the cylinder being in communication with the gas generator through a primary passageway and the control valve means associated therewith and the other end through a control valve means bypass passageway whereby the latter end is pressurized continuously when the gas generator is operative, the piston area on the end of the piston acted upon by the pressurized gas entering the cylinder through the primary passageway being proportioned relative to the area of the end of the piston acted upon by the pressurized gas received through the bypass passageway so that essentially equal force is obtained in either direction of movement of the piston when both ends of the piston are in unrestricted communication with the gas generator.

Claim 13

A servo system according to claim 10, in which: each control valve means comprises a solenoid actuated ported valve having an inlet port, a cylinder port and a vent port, the ported valve having a poppet positionable by a solenoid to permit gas flow from the gas generator through the inlet port and the cylinder port to the cylinder while blocking flow through the vent port or to permit flow from the cylinder through the cylinder port and vent port while blocking the inlet port.

Claim 14

A servo system according to claim 8, in which: each actuator means comprises a double-acting piston housed within a cylinder, each piston being coupled to a movable fin by a piston rod, the cylinder having a main chamber in which the piston is reciprocable and a cylindrical extension encompassing the piston rod for a substantial portion of the length of the latter, and the diversion valve means for each actuator means comprises spool valve means mounted on the piston rod within the cylindrical extension of the cylinder, the spool valve means being movable to block gas flow through the cylindrical extension to selected reaction nozzles in synchronism with the movement of the movable fins by the piston and piston rod.

Claim 15

A servo system according to claim 12, in which: one end of the main chamber of each cylinder is in communication with the gas generator through a primary passageway and a control valve means associated therewith and the other end through a bypass passageway whereby the latter end is continuously pressurized when the gas generator is operative, the piston area on the piston end acted upon by the pressurized gas entering the cylinder through the control valve means being proportioned relative to the area of the piston end acted upon the pressurized gas received through the bypass so that essentially equal force is obtainable in either direction of movement of the piston.

Claim 16

A servo system according to claim 13, in which: each control valve means comprises a solenoid actuated ported valve having an inlet port, a cylinder port and a vent port, the ported valve having a poppet positionable by a solenoid to permit gas flow from the gas generator sequentially through the inlet port and the cylinder port to the cylinder while blocking flow through the vent port or to permit gas flow from the cylinder sequentially through the cylinder port and vent port while blocking the inlet port.