An improved emergency aircraft oxygen respirator for passenger use in an aircraft providing a mask attached to a passenger by a head strap, the mask having a facial conforming inner liner forming an airtight seal to each various passenger, the mask further defining an oxygen line connection, a valve operated expired breathing opening, and at least one inlet filter to remove toxic fumes, chemical vapors and smoke during a fire or electrical malfunction in the airplane, the oxygen line connection engaging the plane's existing chemical oxygen generation system, replacing the oxygen mask for passengers in a plane, the replacement respirator deploying within the passenger compartment of the airplane in the same manner as the oxygen masks being replaced.

An oxygen system supplies either 100% oxygen to a demand valve in a or pulses of oxygen to the mask. Switching is automatic during a parachute descent. The system includes a valve manifold that is responsive to ambient pressure such that at low pressures it is configured to deliver gas from either an oxygen cylinder or an aircraft supply line to the mask demand valve and at higher pressures it is configured to deliver gas from the cylinder to a pulse gas delivery system. The mask also includes an inhalation valve that is closed if oxygen is supplied to the demand valve. Otherwise, the inhalation valve opens to allow ambient air to be drawn in and the pulse gas delivery system delivers a pulse of oxygen in response to the onset of inhalation.

An oxygen system supplies either 100% oxygen to a demand valve in a or pulses of oxygen to the mask. Switching is automatic during a parachute descent. The system includes a valve manifold that is responsive to ambient pressure such that at low pressures it is configured to deliver gas from either an oxygen cylinder or an aircraft supply line to the mask demand valve and at higher pressures it is configured to deliver gas from the cylinder to a pulse gas delivery system. The mask also includes an inhalation valve that is closed if oxygen is supplied to the demand valve. Otherwise, the inhalation valve opens to allow ambient air to be drawn in and the pulse gas delivery system delivers a pulse of oxygen in response to the onset of inhalation.

In one embodiment of an aircraft emergency oxygen delivery system, power can be generated by the flow of gas over a transducer disposed inside an oxygen delivery tube. A pressure differential gives rise to a temperature difference across the transducer, and the temperature difference can be converted to a voltage. The voltage can be quadratically dependent upon the Mach number M (e.g. flow velocities from 1 to 140 m/s) and proportional to a Seebeck coefficient of the transducer. The power thus generated may be used to operate LED indicators visible from the exterior of the tube, a variety of sensors, and wireless communication with a central control system. Oxygen flow to a mask may be adjusted based on ambient oxygen content and data collected from a passenger wearing the mask, including a blood oxygen saturation level, pulse or respiration rate.

In one embodiment of an aircraft emergency oxygen delivery system, power can be generated by the flow of gas over a transducer disposed inside an oxygen delivery tube. A pressure differential gives rise to a temperature difference across the transducer, and the temperature difference can be converted to a voltage. The voltage can be quadratically dependent upon the Mach number M (e.g. flow velocities from 1 to 140 m/s) and proportional to a Seebeck coefficient of the transducer. The power thus generated may be used to operate LED indicators visible from the exterior of the tube, a variety of sensors, and wireless communication with a central control system. Oxygen flow to a mask may be adjusted based on ambient oxygen content and data collected from a passenger wearing the mask, including a blood oxygen saturation level, pulse or respiration rate.

The inflatable harness assembly for an aircraft oxygen crew mask includes one or more inflatable tubes having an outer layer of fabric material with an airtight coating for inflating the inflatable harness assembly. The inflatable tubes include an inner core of resilient, elastic material fixedly connected between first and second ends of the inflatable tubes that biases the inflatable tubes to shorten when the tubes are deflated. Inflation of the tubes them to expand the outer layer of material radially outwardly and lengthen axially, to allow the harness assembly to be placed over the user's head. Deflation of the tubes causes the aircraft inflatable harness assembly to grip the user's head with a desired head tension.

The inflatable harness assembly for an aircraft oxygen crew mask includes one or more inflatable tubes having an outer layer of fabric material with an airtight coating for inflating the inflatable harness assembly. The inflatable tubes include an inner core of resilient, elastic material fixedly connected between first and second ends of the inflatable tubes that biases the inflatable tubes to shorten when the tubes are deflated. Inflation of the tubes them to expand the outer layer of material radially outwardly and lengthen axially, to allow the harness assembly to be placed over the user's head. Deflation of the tubes causes the aircraft inflatable harness assembly to grip the user's head with a desired head tension.

A system for the emergency oxygen supply of passengers in an aircraft includes at least one primary oxygen mask and at least one secondary oxygen mask arranged in the aircraft in a compartment above a seat, and a retaining receptacle arranged in the compartment. The at least one primary oxygen mask and at least one secondary oxygen mask are each connected to an oxygen source by way of a tube. The at least one primary oxygen mask drops out of the compartment before the at least one secondary oxygen mask when a flap of the compartment opens. The at least one secondary oxygen mask is arranged in the at least one retaining receptacle. The retaining receptacle is connected to the compartment by a first connector and to an activation device of the oxygen source by a second connector. The at least one primary oxygen mask can activate the oxygen source.

A system for the emergency oxygen supply of passengers in an aircraft includes at least one primary oxygen mask and at least one secondary oxygen mask arranged in the aircraft in a compartment above a seat, and a retaining receptacle arranged in the compartment. The at least one primary oxygen mask and at least one secondary oxygen mask are each connected to an oxygen source by way of a tube. The at least one primary oxygen mask drops out of the compartment before the at least one secondary oxygen mask when a flap of the compartment opens. The at least one secondary oxygen mask is arranged in the at least one retaining receptacle. The retaining receptacle is connected to the compartment by a first connector and to an activation device of the oxygen source by a second connector. The at least one primary oxygen mask can activate the oxygen source.

A communication assembly for avoiding interferences due to oxygen flow noise, including a) a breathing mask having a body having a face shell having a breathing cavity and a regulator delivering a breathing gas, b) a microphone configured to capture a sound signal in the breathing cavity, c) a test button for supplying the breathing cavity with breathing gas, d) an attenuation device, e) a sound monitoring system, f) a controller configured to the attenuation device operate in an active mode when a flow noise though the breathing cavity during inhalation by the user is detected, and an inactive mode when a vocal sound or a flow noise in the breathing cavity in a stowed configuration is detected, and g) a transmitter for transmitting an output signal.