Hybrid on-board generation of oxygen for aircraft passengers

Abstract

Provided herein is a hybrid system for generating oxygen on-board an aircraft for passengers and/or flight crew to breath. The system includes a first chemical oxygen generator component configured to promptly supply oxygen suitable for breathing upon an emergency situation arising and during an initial descent mode. Heat produced from the exothermic decomposition reactions inherent in several types of chemical oxygen generators can be harvested and feed to a second oxygen generator. The second oxygen generator is a solid electrolyte oxygen separation system that catalytically separates oxygen from air inside specialized ceramic materials at high temperatures, about 650 C. to 750 C., using electrical voltage. The ability to feed heat from the first oxygen generator to the second oxygen generator substantially reduces the lag time until the second ceramic oxygen generator is available to take over as the oxygen supply.

Claims

1. A hybrid system for providing supplemental oxygen for breathing for crew or passengers of an aircraft, comprising: an on-board oxygen generator that requires heating to reach an operational temperature; and a chemical oxygen generator configured to produce oxygen and heat; a heat exchange interface disposed between said on-board oxygen generator and said chemical oxygen generator to provide thermal communication between said chemical oxygen generator and said on-board oxygen generator, said chemical oxygen generator including a chemical oxygen generating composition that is at least partially coated on said heat exchange interface, wherein said heat exchange interface is operative to supply the heat produced by the chemical oxygen generator to said on-board oxygen generator to thereby expedite attainment of the operational temperature for said on-board oxygen generator.

2. The hybrid system of claim 1, wherein said chemical oxygen generating composition is coated in an array on said heat exchange interface.

3. The hybrid system of claim 1, wherein said chemical oxygen generating composition is scattered in a random pattern on said heat exchange interface.

4. The hybrid system of claim 1, wherein said on-board oxygen generator comprises a solid electrolyte oxygen separator having at least one membrane configured to receive heat from the chemical oxygen generator.

5. The hybrid system of claim 4, wherein the solid electrolyte oxygen separator comprises a ceramic oxygen generator and said at least one membrane is a ceramic membrane.

6. The hybrid system of claim 1, further comprising at least one breathing mask connected in a communicating relationship with said chemical oxygen generator and said on-board oxygen generator, and configured to receive oxygen from at least one of the chemical oxygen generator and the on-board oxygen generator; and a pulsed oxygen delivery subsystem connected to both the chemical oxygen generator and the on-board oxygen generator and configured to regulate a flow of oxygen to said at least one breathing mask based on a sensed breathing pattern.

7. The hybrid system of claim 1, further comprising a controller configured to control said on-board oxygen generator and said chemical oxygen generator.

8. A hybrid system for providing supplemental oxygen for breathing for crew or passengers of an aircraft, comprising: a first on-board oxygen generator configured to supply oxygen in an initial stage, said first on-board oxygen generator including a chemical oxygen generator configured to produce heat through exothermic chemical decomposition reactions; a second on-board oxygen generator configured to generate oxygen on-board an aircraft in a subsequent stage, said second on-board oxygen generator including a solid electrolyte oxygen separator configured to catalytically separate oxygen from a supply stream of air at a temperature of 650 C. to 750 C. by applying an electrical voltage; a heat exchange interface disposed between said second on-board oxygen generator and said chemical oxygen generator of said first on-board oxygen generator to provide thermal communication between said chemical oxygen generator and said second on-board oxygen generator, said chemical oxygen generator including a chemical oxygen generating composition that is at least partially coated on said heat exchange interface, wherein said heat exchange interface is operative to supply the heat produced in the exothermic chemical decomposition reactions of the chemical oxygen generator to the second on-board oxygen generator to increase a rate at which the supply stream of air reaches an operating temperature of 650 C. to 750 C.; and a controller configured to control the first on-board oxygen generator and the second on-board oxygen generator.

9. The hybrid system of claim 8, wherein said chemical oxygen generating composition is coated in an array on said heat exchange interface.

10. The hybrid system of claim 8, wherein said chemical oxygen generating composition is scattered in a random pattern on said heat exchange interface.

11. The hybrid system of claim 8, wherein the solid electrolyte oxygen separator comprises a ceramic material configured to catalytically separate oxygen from the supply stream of air.

12. The hybrid system of claim 8, further comprising at least one breathing mask in a communicating relationship with the first on-board oxygen generator and the second on-board oxygen generator, whereby said at least one breathing mask is configured to receive oxygen from at least one of the first on-board oxygen generator and the second on-board oxygen generator; and a pulsed oxygen delivery subsystem connected to both the first on-board oxygen generator and the second on-board oxygen generator and configured to regulate flow of oxygen to said at least one breathing mask based on a sensed breathing pattern.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a schematic diagram of a first embodiment of a system for providing regulated flow of oxygen, including for flight crew or passengers on-board an aircraft.

(2) FIG. 2 is schematic diagram of an enlarged portion of the system of FIG. 1 for heating an on-board oxygen generator with a chemical oxygen generator.

(3) FIG. 3 is a flow chart illustrating a method for providing regulated flow of oxygen, including for flight crew or passengers on-board an aircraft, in accordance with an embodiment of the present invention.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

(4) Ceramic oxygen generator (COG) systems utilize solid electrolyte oxygen separation (SEOS) technology in which oxygen is catalytically separated from air inside specialized ceramic materials at high temperatures, about 650 C. to 750 C., using electrical voltage. While this process produces substantially pure oxygen gas product at pressure and suitable for breathing at any altitude, including higher altitudes over 30,000 feet, the drawback is that the oxygen is not promptly available upon powering on the device because the device has to reach the high required operating temperature first. Due to the high operational temperature requirement, there is typically a time lag before full oxygen capacity from a ceramic oxygen generator or solid electrolyte oxygen separator can be fully utilized.

(5) Provided herein is a hybrid system and method for generating, supplying and maintaining adequate reserves of oxygen. One preferred application for the present invention is to provide oxygen for passengers and flight crew on-board an aircraft including at high altitudes above 30,000 feet, during descent, and at holding altitudes at or below 30,000 feet, on flight paths over variable terrain, and on flights of any duration. The present invention offers several advantages for providing oxygen to passengers and crew on both business jets and commercial aircrafts.

(6) Maintaining adequate reserves of oxygen may be accomplished by storing excess oxygen generated for future use through refilling emergency reserves. Conservation of available oxygen by more closely matching oxygen supplied from the system to oxygen demand by passengers and crew also assists with maintenance of adequate reserves.

(7) Accordingly, as is shown in FIG. 1, which is provided for purposes of illustration by way of example, and not by way of limitation, the present invention provides for a system for providing regulated flow of oxygen rapidly and intermittently as needed, in aircraft. Referring to FIG. 1, in a first presently preferred embodiment, the system 100 for providing regulated flow of oxygen rapidly and intermittently as needed, in aircraft, includes a controller or control system 102 in electronic communication with a chemical oxygen generator 112 through line 106. The controller is also in electronic communication with a pulsed oxygen delivery subsystem 122 through line 105. Additionally, the controller is in electronic communication with an on-board oxygen generator 114 of the ceramic oxygen generator (COG) or solid electrolyte oxygen separator (SEOS) type through line 108. The chemical oxygen generator 112 is in thermal communication 113 with the on-board oxygen generator 114. Thermal communication may be achieved through any feasible means known in the art. The zone of thermal communication may include a heat exchange interface 115 so that heat generated through the exothermic chemical decomposition reactions of the chemical oxygen source constituents 150 (e.g. sodium chlorate 152, sodium perchlorate 154, lithium perchlorate 156, and the like) can thereby be harnessed and delivered to the on-board oxygen generator 114 to heat the ceramic membranes and accelerate attainment of operational temperature, 650 C. to 750 C. Typically, an alkali metal chlorate, alkali metal perchlorate, and/or mixtures thereof can be used as the oxygen source. The oxygen generating compositions of the invention can also include about 0.5-15% by weight of a metal powder such as tin powder or iron powder, or a combination of the two powders, for example, to supply the heat to sustain the decomposition of the oxygen source, although other metal powders such as titanium, copper, aluminum, magnesium, and combinations thereof may also be suitable.

(8) The decomposition reaction of the chemical oxygen generator typically produces at least about 3.5 liters (L) of oxygen and 4,220 calories of heat for every 10 grams of sodium chloride at ambient conditions, although the heat produced is typically larger due to the action of additional ingredients such as metal powders that upon oxidation facilitate the decomposition reaction of the chemical oxygen generator constituents.

(9) Continuing with reference to FIG. 1, the chemical oxygen generator 112 is in fluid communication with the pulsed oxygen delivery subsystem 122 through feed line 118. The on-board oxygen generator 114 is also in fluid communication with the pulsed oxygen delivery subsystem 122 through feed line 120. The pulsed oxygen delivery subsystem 122, in turn, is in fluid communication with one or more breathing masks 132, 134, 136, and 138 which can be provided for passengers and crew members through low pressure tubing 124, 126, 128, and 130. Optionally, one or more sensors 140 or detectors in electronic communication with the controller and/or the pulsed oxygen delivery subsystem may be provided in any of the breathing masks, the pulsed oxygen delivery subsystem, the oxygen sources, or along the feed lines or low pressure tubing through which oxygen is supplied for sensing air pressure and/or flow and communicating a corresponding sensor signal indicating air pressure and/or flow to the controller, as will be further explained below.

(10) With regard to FIG. 1, different types of sensors or detectors may be provided for each of the oxygen sources, the feed lines, the pulsed oxygen delivery subsystem, and in the breathing masks. As used herein, reference numeral 140 refers generally and broadly to any type of sensor or detector in any of these locations and need not be the same across the various locations. For example, the sensors or detectors represented by reference numeral 140 may be for measuring pressure, flow rate, temperature, volume, concentration of constituent gases in a gaseous mixture, oxygen usage rates, and the like.

(11) Referring to FIG. 2, in addition to the zone of thermal communication 113 between the chemical oxygen generator 112 and the on-board oxygen generator 114 so that heat from the chemical oxygen generator can be used to heat the on-board oxygen generator, other elements to effectuate this transfer of heat can also be provided. For example, the heat exchange interface 115 may be provided within the zone of thermal communication, as part of the chemical oxygen generator or as a separate element of the system between the chemical oxygen generator and the heat-dependent on-board oxygen generator. The chemical constituents of the chemical oxygen generator responsible for the exothermic decomposition reactions may be combined into a distributed oxygen generating formulation to cover the interface 115 and thereby more effectively transfer heat. For example, the chemical constituents (e.g. sodium chlorate) that decompose to give off heat and the metal powders (e.g. iron oxide) that catalyze or enhance this process may be coated in an array or scattered in a random pattern across the heat exchange interface. The heat exchange interface may include a filter through which the heat given off upon decomposition can be harnessed for delivery to the heat-dependent solid electrolyte oxygen separator type of on-board oxygen generator (OBOG). The chemical oxygen generator 112 typically also includes one or more accompanying igniters or sequencers or a chemical oxygen generator initiation device (not shown).

(12) The on-board oxygen generator (OBOG) 114 preferably includes a solid electrolyte oxygen separator (SEOS). One example of this solid electrolyte oxygen separator is a ceramic oxygen generator device. The ceramic oxygen generator type of device provides the advantages of producing highly enriched oxygen gas (substantially 100% O.sub.2) at pressure suitable for breathing, thereby reducing or eliminating the need for compressors which take up space and add weight.

(13) Referring to FIG. 3, the steps of a method 200 in accordance with an embodiment of the present invention are illustrated. A method for providing regulated flow of oxygen, including for flight crew or passengers on-board an aircraft, includes the step 202 of activating a first system to initiate rapid flow of oxygen from a first on-board oxygen supplier, a chemical oxygen generator, typically at high altitudes greater than 30,000 feet. Then, heat from the exothermic decomposition reaction of the first system is supplied to a second system including an on-board oxygen generator having a solid electrolyte oxygen separator at step 204. At step 206, the second system is activated to initiate flow of oxygen from an on-board oxygen generator after the second system has reached operational temperature of 650 C. to 750 C. Highly enriched oxygen gas from the second system is integrated with oxygen supplied from the first system at step 208 to supply oxygen for breathing at altitudes typically of 30,000 feet or lower. Subsequently, at step 210 the first system can be deactivated when the second system is able to meet oxygen demands. At step 212, a breathing pattern of a passenger or a flight crew member is sensed, and at step 214 the flow of oxygen to a breathing mask of a passenger or a flight crew member is regulated by delivering oxygen to the mask from the first system or the second system through a pulsed oxygen supplier configured to vary a flow rate of oxygen based on a sensed breathing pattern and/or physiological requirements.

(14) During an initial stage, for example immediately after an emergency situation arises, a stream of gas highly enriched with oxygen is provided from the first on-board oxygen supplier (e.g. the chemical oxygen generator). The initial stage typically exists when the aircraft is at an altitude greater than 30,000 feet. An emergency signal may be used to initiate flow during the first stage which lasts around three to seven minutes before oxygen from the heat-dependent on-board generator is available. In a subsequent stage, oxygen is supplied from a second on-board oxygen supplier, the on-board oxygen generator. The second on-board oxygen supplier includes an on-board oxygen generator that produces oxygen enriched gas on-board the aircraft. The subsequent stage typically exists after the aircraft has completed an initial descent and reached a holding altitude. However, when the on-board generator is of the ceramic oxygen generator type, given the high purity of the oxygen gas produced thereby, it is suitable for breathing at altitudes over 30,000 feet as well. After the initial three to seven minute heating period during which the chemical oxygen generator is the sole oxygen supplier the on-board generator is generally ready to takeover.

(15) The on-board oxygen generator may be a ceramic oxygen generator. Ceramic membranes for separating oxygen from a supply stream of air rely on the catalytic properties of the interior surfaces of specialized ceramic materials to ionize and then separate oxygen. As applied on aircrafts, the supply stream of air for the ceramic oxygen generator type on-board oxygen generator device is typically engine bleed air. However, the supply gas for the ceramic oxygen generator type on-board oxygen generator device may come from other sources. For example, the supply gas may come from the product stream of another on-board oxygen generator device positioned upstream, including a ceramic oxygen generator or molecular sieve oxygen generator (MSOG).

(16) The oxygen ionization process at high surface temperatures is partly responsible for generation of a product gas from the ceramic membrane systems that is virtually 100% pure oxygen with no possibility for the presence of biological or toxic chemical components. Ceramic operating temperatures are around 700 C. and the electrical potential difference across the membrane is on the order of a volt. Ceramic membrane oxygen generators are one preferred subset of ion transport membrane (ITM) technologies.

(17) The highly enriched oxygen gas produced by the ceramic oxygen generator device is suitable for breathing at higher altitudes above 30,000 feet whereas more moderately enriched oxygen gas produced by other types of on-board oxygen generator devices, including molecular sieve oxygen generator devices, is not suitable for breathing at higher altitudes and requires compressors to pressurize it before it is suitable for breathing at lower altitudes. Highly enriched oxygen gas from the ceramic oxygen generator device may be used directly for breathing at any altitude after waiting for attainment of the high temperature requirement necessary to the production of such gas.

(18) The standby availability of the ceramic oxygen generator device on-board the aircraft reduces reliance on pressurized gas cylinders and chemical oxygen generators. Smaller pressurized gas cylinders, or none at all, may be provided if ceramic oxygen generator type on-board oxygen generator devices are available. Additionally, the excess oxygen generated by the ceramic oxygen generator devices might be used to refill the smaller pressurized cylinders in the air, thereby reducing maintenance costs from refilling or replacing pressurized gaseous cylinders on the ground.

(19) By incorporating this ceramic oxygen generator device and existing solid electrolyte oxygen separation technology as a component in a system with other components that can supply oxygen sooner and managing the supply of oxygen among the components, the present invention overcomes the drawback of delays encountered with ceramic oxygen generator and solid electrolyte oxygen separation devices. Embodiments of the present invention also overcome the delay drawback by expediting the heating process to reduce the time required for the ceramic oxygen generator devices to reach operational temperature.

(20) For example, chemical oxygen generators that produce highly oxygen enriched gas (about 99% oxygen and above) may supply oxygen for about the first three to seven minutes upon an emergency situation arising. After the first three to seven minutes it is likely that the on-board oxygen generator will have attained operating temperature (650-750 C.) and sufficiently cycled to be able to take over as the oxygen supply.

(21) The controller may be used to coordinate the supply of oxygen from the various sources to the one or more pulsed oxygen suppliers (not shown) of the pulsed oxygen delivery subsystem that feed one or more individual breathing masks. The controller is able to determine what quality of oxygen is required based on altitude and what sources of oxygen are available. The controller manages the oxygen supplies as necessary to meet the demands of passengers and crew while maintaining adequate reserves.

(22) For example, upon an emergency situation arising at high altitude greater than 30,000 feet, if oxygen from a ceramic oxygen generator device is not promptly available because the ceramic oxygen generator device was not turned on until the emergency situation arose, the controller can direct a chemical oxygen generator to promptly supply oxygen. Upon the ceramic oxygen generator device attaining operation temperature of 650 C. to 750 C. and cycling, the controller can sense the presence of highly enriched oxygen available from the ceramic oxygen generator device, infiltrate this into the supply stream from the chemical oxygen generator, and phase out supply from the chemical oxygen generator once the ceramic oxygen generator type on-board oxygen generator device is able to adequately meet demand.

(23) One way in which the system may provide regulated flow of oxygen rapidly and intermittently, as needed in aircraft, is through the pulsed oxygen delivery subsystem, which can conserve oxygen, such as by regulating oxygen flow to the breathing mask of a passenger or a flight crew member during an exhalation phase of the breathing cycle and resuming flow of oxygen to the breathing mask during an inhalation phase.

(24) For example, one or more sensors 140 may be provided in fluid communication with each breathing mask for detecting an inhalation phase or an exhalation phase of a breathing cycle of a passenger or a flight crew member and then communicating this information to the controller. The controller, in turn, directs the pulsed oxygen delivery subsystem and the oxygen sources accordingly to conserve, decrease, stop, increase, or resume the flow of oxygen as needed to better manage oxygen supplies while meeting the demands of passengers and flight crew members.

(25) Other components may be incorporated in different embodiments but are not required. For example, these other components may be a main cabin decompression relay, one or more additional relays, an electrically operated on/off inlet valve between each oxygen source and each of the feed lines from the oxygen source to each breathing mask, one or more pressure transducers, and the like.

(26) Other components of the system may also include cooling or heating devices, for example along the feed lines, to ensure enriched oxygen gas from the oxygen generators (especially the very high temperature ceramic oxygen generator device) is supplied to the breathing masks of passengers or cabin flight crew at the appropriate temperature compatible with physiological preferences or requirements. Cooling devices for cooling the oxygen enriched gas from the chemical oxygen generator may be configured to perform dual functions, also harnessing the heat removed from the product oxygen stream for redirecting to heat the solid electrolyte oxygen separator so that it attains operational temperature more rapidly than otherwise and at lower heating cost. Cooling or heating devices, for example along the feed lines, may also be provided to ensure inert gas is delivered to the fuel tank at the appropriate temperature in embodiments that include this feature.

(27) Additionally, the pulsed oxygen delivery subsystem 122 may include one or more pulsed oxygen suppliers (not shown) for intermittently providing flow of oxygen to the individual breathing masks. The breathing masks may each include a reservoir bag. The pulsed oxygen suppliers may be utilized to further distribute and regulate supply of oxygen to passengers throughout the aircraft.

(28) In alternative embodiments, as part of the control system, in addition to the controller, one or more sensors 140 or detectors at each of the oxygen sources may be provided to determine volume available and oxygen concentration. Another sensor or detector (not shown) in a communicating relationship with the controller may read altitude. Additional sensors 140 and detectors may be provided within individual breathing masks, within the pulsed oxygen delivery subsystem, or along any of the lines to or from the breathing masks or the pulsed oxygen delivery subsystem to monitor other variables including oxygen usage rates.

(29) In still other embodiments, the controller may be in electrical communication with each oxygen source and a main cabin decompression relay (not shown). More specifically, the controller may be in communication with an electrically operated on/off inlet solenoid valve (not shown) between each oxygen source and each breathing mask, or between each oxygen source and the pulsed oxygen delivery subsystem supplying oxygen to the masks, or between the pulsed oxygen delivery subsystem and each mask.

(30) In further embodiments, given the ability of ceramic oxygen generator type on-board oxygen generator devices to perform better with input streams more highly concentrated in oxygen, it may be particularly advantageous to have another on-board oxygen generator device upstream of the ceramic oxygen generator device. This upstream on-board oxygen generator would serve to increase the oxygen concentration in the supply stream fed to the ceramic oxygen generator device beyond the oxygen concentration of an alternative air supply stream, for example engine bleed air.

(31) As a further alternative, oxygen produced by the chemical oxygen generator generally has to be cooled before it is suitable for breathing and the heat removed in the cooling process could be used to provide heat for the second generator of the hybrid system. The second generator is the solid electrolyte oxygen separator, typically a ceramic oxygen generator, that depends upon substantial heating to reach operational temperatures in excess of 600 C.

(32) The present invention is not limited to the embodiments described above. Various changes and modifications can, of course, be made, without departing from the scope and spirit of the present invention. Additional advantages and modifications will readily occur to those skilled in the art. Accordingly, various modifications may be made without departing from the spirit or scope of the general inventive concept as defined by the appended claims and their equivalents.