Electromechanical regulator with primary and backup modes of operation for regulating passenger oxygen

An electromechanical regulator for regulating passenger oxygen for aircraft, comprising:

• an electromechanical regulator valve body including a supply inlet chamber and an outlet chamber;
• an oxygen supply inlet port for receiving oxygen from a source of oxygen, said oxygen supply inlet port being connected to said supply inlet chamber by a first supply channel;
• an oxygen outlet port connected to said outlet chamber;
• a balanced valve disposed in said electromechanical regulator valve body, said balanced valve including a valve channel defined in said electromechanical regulator valve body, a valve diaphragm separating said supply inlet chamber and said outlet chamber, said valve diaphragm including an opening forming a valve seat, and a valve member disposed in said valve channel and moveable therein between a valve closed position and a valve open position, said valve member being biased to engage said valve seat in the valve closed position;
• an electronic valve portion disposed in said electromechanical regulator valve body, said electronic valve portion being operative to control movement of said valve member between said open and closed positions responsive to sensed cabin pressure in the aircraft and sensed output pressure in said oxygen outlet port;
• a mechanical valve portion disposed in said electromechanical regulator valve body, said mechanical valve portion including a supply pressure sensing chamber, said mechanical valve portion being operative to move said valve member between said open and closed positions responsive to pressure in said supply pressure sensing chamber and pressure in said outlet chamber, wherein said supply pressure sensing chamber includes a wall having a surface defining an aneroid valve vent hole, an aneroid exposed to cabin pressure and mounted adjacent to said aneroid valve vent hole, said aneroid contracting to open said aneroid valve vent hole to vent pressure from the supply pressure sensing chamber, and lengthening to close said aneroid valve vent hole to trap pressure in the supply pressure sensing chamber, responsive to changes in cabin pressure;
• and
• a movable diaphragm separating said supply pressure sensing chamber from said outlet chamber, and wherein a pressure sensing spring is disposed in said supply pressure sensing chamber and biases said movable diaphragm toward said valve member.

An electromechanical regulator for regulating passenger oxygen for aircraft, comprising:

• an electromechanical regulator valve body including a supply inlet chamber and an outlet chamber;
• an oxygen supply inlet port for receiving oxygen from a source of oxygen, said oxygen supply inlet port being connected to said supply inlet chamber by a first supply channel;
• an oxygen outlet port connected to said outlet chamber;
• a balanced valve disposed in said electromechanical regulator valve body, said balanced valve including a valve poppet channel defined in said electromechanical regulator valve body, a valve diaphragm separating said supply inlet chamber and said outlet chamber, said valve diaphragm including an opening forming a valve seat, and a valve poppet member disposed in said valve poppet channel and moveable therein between a valve closed position and a valve open position, said valve poppet member being biased to engage said valve seat in the valve closed position;
• an electronic valve portion disposed in said electromechanical regulator valve body, said electronic valve portion being operative to control movement of said valve poppet member between said open and closed positions responsive to sensed cabin pressure in the aircraft and sensed output pressure in said oxygen outlet port;
• a mechanical valve portion disposed in said electromechanical regulator valve body, said mechanical valve portion including a supply pressure sensing chamber, said mechanical valve portion being operative to move said valve poppet member between said open and closed positions responsive to pressure in said supply pressure sensing chamber and pressure in said outlet chamber, wherein said supply pressure sensing chamber includes a wall having a surface defining an aneroid valve vent hole, an aneroid exposed to cabin pressure and mounted adjacent to said aneroid valve vent hole, said aneroid contracting to open said aneroid valve vent hole to vent pressure from the supply pressure sensing chamber, and lengthening to close said aneroid valve vent hole to trap pressure in the supply pressure sensing chamber, responsive to changes in cabin pressure;
• a movable diaphragm separating said supply pressure sensing chamber from said outlet chamber, and wherein a pressure sensing spring is disposed in said supply pressure sensing chamber and biases said movable diaphragm toward said valve poppet member;
• and
• a cabin pressure transducer sensing cabin pressure in the aircraft and generating a cabin pressure signal indicating cabin pressure, and an outlet pressure transducer sensing output pressure in said oxygen outlet port and generating an outlet port signal indicating pressure in said oxygen outlet port, said cabin pressure signal and said outlet port signal being received by said controller.