JP4345917B2 - Gas generation system and gas generation method - Google Patents

Description

  The present invention is a continuation of provisional application 60 / 391,086 filed with the US Patent and Trademark Department on June 25, 2002, the priority of which is required here.

  The present invention relates to an oxygen / inert gas generator that can be used in an aircraft, and in particular, the present invention relates to a combined type of an onboard oxygen generation system (OBOGS) and an onboard inert gas generation system (OBIGGS). .

  The present invention addresses the demand for oxygen-rich and nitrogen-rich gases on many aircraft. Oxygen is needed for passengers when the aircraft cabin may drop to a pressure equal to an altitude of 10,000 feet or more. Passengers with impaired lungs may need oxygen. Nitrogen is necessary to inactivate the space above the fuel in the fuel tank, also called ullage, to reduce the possibility of explosive conditions. Nitrogen is also used to extinguish a cargo compartment fire.

Two techniques are commonly used to supply oxygen-rich and nitrogen-rich gases on board from high pressure air that can be used for engine bleed. On-board oxygen generation system (OBOGS) and on-board inert gas generation system (OBIGGS) using molecular sieve and pressure swing adsorption process (PSA) as one technology to supply oxygen-rich gas and nitrogen-rich gas, respectively Have been widely used. The second technique for supplying a nitrogen-rich gas is generally referred to as a hollow fiber membrane ( HFM ) or permeable membrane (PM) technology.

  The molecular sieve and PSA process method is generally accepted as the best way to generate oxygen-rich gas on board when the oxygen purity requirement is about 95% or less. The PSA and HFM technologies used to generate nitrogen-rich gases are based on the aircraft air source used, the flow and purity of the desired nitrogen-rich gas, and the temperature, air supply pressure, ambient absolute pressure, altitude, etc. Depending on the conditions, it has advantages and disadvantages. Each parameter affects the performance of each technology differently. For example, PSA technology can generally be performed well at a temperature of about 70 degrees Fahrenheit, while HFM technology can be performed better at a temperature of about 160 degrees Fahrenheit. There are a number of parameters that must be considered when implementing these techniques most effectively from application to application.

  Apply on-board gas separation technology to generate oxygen-rich and nitrogen-rich gases with less engine bleed and power and / or to find synergies to reduce the size and weight of the gas separation system Attempts have been made. One successful attempt is the OBOGS / OBIGGS combination used on V-22 aircraft. The system uses two types of molecular sieves and the same PSA process to generate an occupant breathing oxygen-rich gas and a nitrogen-rich gas to deactivate the fuel tank ullage. This two-gas system has the advantage of simultaneously reducing size and weight by sharing common system components such as inlet filters, pressure reducers, PSA circulation valves, and control electronics.

  Each of the PSA technology for concentrating oxygen and the HFM technology for concentrating nitrogen has limits on the purity of the generated gas and the concentration of exhaust gas containing many other main components of air that is not desired as the concentrated product gas. For example, PSA-based OBOGS separates oxygen-rich gas for respiration, but at the same time must discharge nitrogen-rich gas that is discarded into the surrounding atmosphere. Similarly, HFM-based OBIGGS separates the nitrogen-rich gas for deactivation, but at the same time must discharge the oxygen-rich gas that is discarded into the surrounding atmosphere.

  It is desirable to increase the efficiency by using nitrogen-rich exhaust gas from OBOGS as an injection gas to HFM / OBIGGS or to increase the efficiency by using oxygen-rich exhaust gas from OBIGGS as an injection gas to PSA / OBOGGS Many people are thinking. However, each of the PSA and HFM technologies requires a pressure differential from their inlets to their outlets for best performance. In general, PSA-based OBOGS and OBIGGS processes should have an input air pressure of 20-60 psig and be vented to the surrounding atmosphere without pressure. The HFM / OBIGGS technology has an input air pressure of 25 psig to 100 psig, and higher pressures are preferred.

  The input air pressure available on board is typically 20 psig to 75 psig, but for most aircraft it is in the lower half of this range. Thus, a typical 30 psig aircraft air supply is quite good as a supply to OBOGS and OBIGGS technologies, respectively. However, connecting the OBOGS exhaust to the OBIGGS inlet reduces the performance of the OBOGS. This means that the exhaust gas cannot be discharged without applying pressure during the PSA process, while the input pressure to the HFM / OBIGGS is lowered. Only about 15 psig of energy can be used to run each process. This is well below the optimum pressure desired for each process to achieve near optimum performance.

  A compressor can be added between the OBOGS exhaust and the OBIGGS inlet to increase the effective pressure differential for each gas separation process. Patent Document 1 discloses an integrated system that generates an inert gas and a breathing gas on an aircraft, and pressurizes the gas emitted from one gas generator using a compressor before entering the other gas generator. Is disclosed. However, the size, weight and cost of the compressor are sacrificed more than offsetting the benefits gained from gas separation performance.

Patent Document 2 discloses a gas generation system that has a first gas separation device that separates an oxygen-rich gas from a supply gas and leaves the remaining gas, and generates oxygen and the remaining gas. The first oxygen-rich gas from the first gas separation device is put into the second gas separation device and further separates the oxygen gas from the first oxygen-rich gas. The second gas separator generates a highly oxygen-rich product gas and the remaining gas, and at least one of the first and second gas separators has a ceramic membrane that diffuses gas ions. .
US Pat. No. 4,681,602 US Pat. No. 6,319,305

It is an object of the present invention to provide an oxygen / inert gas generator that can be used in aircraft, and in particular, a combination of an aircraft on- board oxygen generation system (OBOGS) and an aircraft on- board inert gas generation system (OBIGGS). It is an object of the present invention to provide a mold.

  One aspect of the invention is that one or more OBOGS is installed to generate oxygen, one or more OBIGS are installed to generate an inert gas, and the exhaust gas from the one or more OBOGS is: Used as an auxiliary inert gas source.

The gas generation system of the present invention is an aircraft gas generation system including a passenger cabin, a fuel tank, and a cargo compartment, and is installed so as to generate oxygen by receiving a first air flow branched from the extracted air flow. At least one aircraft on- board oxygen generation system (OBOGS) and at least one aircraft installed to generate an inert gas in response to a second air stream branched from the extracted air stream In- machine inert gas generation system (OBIGGS),
Connected to the on-board inert gas generation system (OBIGGS) and connected to the fuel tank and the cargo compartment, respectively, the first and second supply paths are connected, and usually the first supply path for guiding the inert gas to the fuel tank. A selection valve that is open to, closes the first supply path in an emergency or when necessary, and opens a second supply path that leads the inert gas to the cargo compartment;
Connected to the on-board oxygen generation system (OBOGS) exhaust gas, and the third and fourth supply passages are connected to the fuel tank and the cargo compartment, and are normally open to release the exhaust gas. A control valve that closes the release upon deactivation and opens one of a third supply path that leads exhaust gas to the fuel tank or a fourth supply path that leads to the cargo compartment;
The first air stream and the second air stream are characterized in that the ratio of oxygen to nitrogen is substantially the same.

The gas generation method of the present invention is a gas generation method used for an aircraft including a passenger cabin, a fuel tank and a cargo compartment.
Oxygen is generated from a first air stream branched from an air stream extracted by at least one aircraft on- board oxygen generation system (OBOGS), and at least one aircraft on- board inert gas generation system (OBIGGS) Generating an inert gas from the second air stream branched from the air stream extracted at
Is connected to the on-board inert gas generation system (OBIGGS), also a selection valve first and second supply channel for guiding each of the fuel tank and cargo are connected, the normally lead to inert gas into the fuel tank 1 Open in the supply line, close the selection valve to the first supply path in case of emergency or necessary, and open the selection valve to the second supply path to guide the inert gas to the cargo compartment is connected to an exhaust gas oxygen generation system (OBOGS), also the control valve the third and fourth supply passage respectively to the fuel tank and cargo are connected, it has opened to release the normal exhaust gas, the fuel tank or When the cargo compartment is deactivated, the control valve is closed and the control valve to either the third supply passage leading the exhaust gas to the fuel tank or the fourth supply passage leading to the cargo compartment It is characterized by opening.

  In the above system and method, at least one on-board oxygen generation system (OBOGS) has two OBOGS and at least one on-board inert gas generation system (OBIGGS) has two OBIGGS. Can do.

  Further, in the above system and method, the inert gas is nitrogen and an auxiliary oxygen source can be installed.

  In the above system and method, a first control valve and a second control valve can be installed, and the first control valve selectively emits at least one OBOGS exhaust gas to the atmosphere or to the second control valve. The second control valve delivers at least one OBOGS exhaust gas to one of two locations.

  In the system and method described above, at least one heat exchanger can be placed to receive air at a first temperature and exit to both the OBOGS and the OBIGGS at a second temperature.

  In the system and method described above, at least one filter / water separator can be placed to receive air and provide filtered air with reduced moisture to both the OBOGS and the OBIGGS.

  In the systems and methods described above, the auxiliary oxygen source can be at least one compressed oxygen tank.

The gas generation system of the present invention is an aircraft gas generation system including a passenger cabin, a fuel tank and a cargo compartment,
And extracted the first at least one group onboard oxygen generating system of the oxygen generating oxygen upon receiving an air flow was established so as to supply to the passenger compartment of an aircraft which is branched from the airflow (OBOGS), bleed Receiving at least one second air stream branched from the generated air stream to generate an inert gas, and supplying the inert gas to an aircraft fuel tank or cargo compartment; A gas generation system (OBIGGS);
A first supply that is connected to the on-board inert gas generation system (OBIGGS) and that is connected to first and second supply passages that lead to the fuel tank and the cargo compartment, respectively, and that normally leads the inert gas to the fuel tank. A selection valve that is open to the road, closes the first supply path in case of an emergency or when necessary, and opens a second supply path that leads the inert gas to the cargo compartment;
Connected to the exhaust gas of the on-board oxygen generation system (OBOGS) and connected to the fuel tank and the cargo compartment respectively, the third and fourth supply passages are connected and are normally open to release the exhaust gas. A control valve that closes the discharge when the cargo compartment is inactivated and opens one of the third supply path leading the exhaust gas to the fuel tank or the fourth supply path leading to the cargo compartment;
The ratio of the first air stream and the second air stream oxygen to nitrogen is substantially the same.

The gas generation method of the present invention is a gas generation method used for an aircraft including a passenger cabin, a fuel tank and a cargo compartment.
At least one on-board oxygen generation system (OBOGS) installed to generate oxygen from a first air stream branched from the extracted air stream and supply the oxygen to a passenger cabin of the aircraft; and the extracted air At least one on-board inert gas generation system installed to generate an inert gas from a second air stream branched from the stream and to supply the inert gas to an aircraft fuel tank or cargo compartment ( OBIGGS)
A selection valve connected to the on-board inert gas generation system (OBIGGS) and connected to the fuel tank and the cargo compartment, respectively, is connected to the selection valve , usually leading the inert gas to the fuel tank. Open to the first supply path, close the selection valve to the first supply path in an emergency or when necessary, and open the selection valve to the second supply path to guide the inert gas to the cargo compartment A control valve connected to the exhaust gas of the on-board oxygen generation system (OBOGS) and connected to the fuel tank and the cargo compartment, respectively, connected to the third and fourth supply passages is opened to release the normal exhaust gas. When the fuel tank or cargo compartment is inactivated, the control valve is closed and the control to either the third supply path leading exhaust gas to the fuel tank or the fourth supply path leading to the cargo compartment It is characterized by opening the valve.

  In the above system and method, at least one on-board oxygen generation system (OBOGS) has two OBOGS and at least one on-board inert gas generation system (OBIGGS) has two OBIGGS. Can do.

  Furthermore, in the above system and method, the inert gas is nitrogen and can be provided with an auxiliary oxygen source.

  In the above system and method, a first control valve and a second control valve can be provided, and the first control valve selectively emits at least one OBOGS exhaust gas to the second control valve, and the second control valve Delivers at least one OBOGS exhaust gas to either the fuel tank or the cargo compartment.

  In the above system and method, at least one heat exchanger can be placed, receiving air at a first temperature and exiting to both OBOGS and OBIGGS at a second temperature.

  In the system and method described above, at least one filter / water separator can be placed to receive air and provide reduced moisture to both OBOGS and OBIGGS.

  In the above system and method, the auxiliary oxygen source is at least one compressed oxygen tank.

  A better understanding can be obtained by reading the following detailed description of the embodiments and the appended claims with reference to the accompanying drawings disclosing the present invention. While the disclosures described and depicted above and below are primarily directed to illustrating embodiments of the present invention, this is illustrative and exemplary, and the present invention is not limited thereby. The spirit and technical scope of the present invention are limited only by the terms used in the claims.

  Before beginning the detailed description of the subject invention, the following is stated. Reference numerals and letters are used to identify the same, corresponding or similar parts in different figures. Further, in the following detailed description, exemplary sizes / formats / values / ranges are described, but the present invention is not limited thereto. Specific details have been set forth to illustrate examples of embodiments of the invention, which may be practiced by those skilled in the art with variations or modifications to the specific details. Is clear. Finally, it is clear that embodiments of the present invention can be embodied by changing the combination of hardware control circuitry and software instructions, ie, the present invention is not limited to any specific combination of hardware and software .

  A new way in which synergy is realized is whether the exhaust gas from one type of separator can be used to meet the requirements of other gases without recompression. It is generally understood that as the product flow rate increases, the oxygen purity from the PSA based OBOGS oxygen concentrator decreases. Laboratory tests show that the oxygen concentration in the exhaust gas decreases as the amount of oxygen product increases. A conventional OBOGS oxygen concentrator based on PSA generates respiratory oxygen with a product purity of about 50% to 95% and exhaust gas with an oxygen purity of about 13% to 20%. Laboratory tests of PSA-based OBOGS oxygen concentrators show that increasing the oxygen product to exceed approximately 50%, which is generally considered the practical lower limit of oxygen concentration, reduces the exhaust gas oxygen concentration to approximately 11%. It was done. The HFM / OBIGGS separation process can generate product gas with oxygen concentration of 1-12%, which helps to deactivate the fuel tank or cargo compartment, but the oxygen purity of the exhaust gas is about 30% -40% It is.

  The oxygen concentration of the HFM exhaust gas is close to the practical oxygen concentration supplied to the aircraft passenger mask when the cabin is depressurized and the aircraft pressure drops to an altitude just above 10,000 feet. However, the exhaust gas from the HFM separator may contain these compounds because carbon monoxide, carbon dioxide and water pass through the fibers along with oxygen. If the gas is intended for respiration, the feed air must be made respirable before being exhausted into the HFM. A PSA-based oxygen concentrator removes these impurities from the oxygen product stream and discharges them out of the machine.

  Fuel tank ullage should have oxygen concentration below about 10% to prevent the formation of potentially explosive fuel-air mixture, cargo compartment should have oxygen below about 12% to prevent reignition after extinguishing. Is generally accepted by the aviation industry. This indicates that the exhaust gas from PSA / OBOGS has an oxygen concentration of 11-13%, which itself is too much oxygen to meet the final requirement of deactivating the cargo compartment or fuel tank for the required time. I am doing it. However, since the flow rate of air entering PSA / OBOGS is large and the ratio of exhaust gas is high, which can reduce the consumption of air, the fuel tank and cargo compartment can be reduced from 20.8% even if the oxygen concentration is 13%. It can be used effectively to promote inactivation to lower values. Exhaust gas from a correctly conditioned PSA oxygen concentrator is more effective than the HIM performed at about 2: 1 in the weight base factor of the system to initially deactivate the fuel tank in the initial allowed hours.

  After the first 30 minutes of the aircraft rising and flying at cruising speed, the amount of inert gas required to keep the tank inert is usually less than 50% of the amount required to initially deactivate the tank. is there. Therefore, OBOGS can be used to supply emergency oxygen to passengers, reducing the weight of OBIGGS by about 20%.

  Even if the exhaust gas from OBOGS is too much oxygen to make the tank completely inert, it can be used effectively at the beginning of the tank deactivation time according to computer analysis. Show. By combining with HEM / OBIGGS, the OBOGS exhaust gas can accelerate the deactivation of the tank with OBIGGS having a smaller weight.

  FIG. 1 is a block diagram of a gas separation system that can provide inert gas for fuel tanks and cargo compartments, emergency oxygen for aircraft passengers, and oxygen for passengers in need of treatment. The OBOGS exhaust gas is also used to assist with the deactivation requirements described above. For example, the OBOGS exhaust gas can be used as a gas that inactivates the cargo tank after the fuel tank is inactivated or extinguished.

  The present invention assumes that neither OBOGS nor OBIGGS product gas is concurrent with other requirements. For example, inactivation of the fuel tank is necessary for each flight, but after the cargo compartment fire is extinguished, the inactivation of the cargo compartment has priority over the inactivation of the fuel tank. Therapeutic oxygen is needed for a limited number of passengers on many flights, but the emergency oxygen needed for all passengers takes precedence, and providing oxygen therapy to the first requesting passenger become.

  The OBIGGS and OBOGS units commonly use high-pressure air after passing through temperature, particle, and humidity control devices such as one or more heat exchangers, filters, and water separators. Each OBIGGS and OBOGS unit has a remotely controlled on-off valve that can only flow to equipment required by the particular scenario being implemented. For example, the flow rate of OBIGGS products is generally high to initially deactivate the fuel tank and low during the cruise and cruise mode. The OBOGS oxygen flow rate is somewhat lower for some passengers who need oxygen for treatment, but increases when the aircraft cabin pressure at aviation altitudes above 10,000 feet is reduced.

  The oxygen stored in the cylinder can be used to provide emergency oxygen to the passenger as soon as there is a vacuum in the aircraft cabin. This provides the time required to supply air to the OBOGS unit and begin the oxygen enrichment process. The OBOGS unit can supply emergency oxygen for a longer required time.

  The oxygen monitor is used to monitor the purity of oxygen-rich gas or nitrogen-rich gas used in response to demand. In this case, three product gas sources are envisaged, one monitor being used for each, or one monitor with a product gas sample valve can be used to monitor each desired gas.

  Referring to FIG. 1, the extracted air is passed through a heat exchanger 110 to reduce the temperature of the air to a temperature suitable for OBIGGS, and further to a temperature suitable for OBOGS through another heat exchanger 111. After passing through the heat exchanger 110, the air passes through the filter / water separator 120 to remove various impurities such as moisture and particulates.

The moistureless air filtered out of the filter / water separator 120 is then split into a first air stream and a second air stream, the second air stream to the OBIGGS units 130 , 140, and the first air stream is OBOGS. To units 170, 180 and 190, respectively . Although two OBIGGS units 130, 140 and three OBOGS units 170, 180, 190 are shown, it should be understood that the invention is not limited to the specific number of units described. Furthermore, on-off valves 155 and 125 are arbitrarily installed so that unnecessary OBIGGS and OBOGS can be closed separately.

  The inert gas (nitrogen gas) emitted from the OBIGGS units 130 and 140 is combined and passes through the check valve 270, the control valve 280, and the control orifices 290 and 310. The inert gas exiting the control orifices 290 and 310 is sent to the fuel tank 320 and the cargo compartment 330, respectively, to reduce the possibility of an explosion condition in the fuel tank 320 and to help extinguish the fire in the cargo compartment 330.

  Oxygen gas emitted from the OBOGS units 170, 180, 190 is combined and sent to the control valves 210, 230. The amount that comes out of the control valve 210 is sent to the emergency oxygen mask 340. The output from the control valve 230 passes through a control orifice 240, which can be fixed or variable in size.

  Further, the exhaust gas from the OBOGS units 170, 180, 190 is mainly nitrogen gas, and is sent to the control valve 250 through the control valve 160 and the check valve 165. The control valve 250 selectively discharges exhaust gas from the OBOGS units 170, 180, 190 to the fuel tank 320 or the cargo compartment 330.

  Oxygen tanks 350, 360 emit oxygen through respective regulators 355, 365, respective flow control units 370, 380, and respective check valves 390, 400 and are sent to emergency oxygen mask 340.

  The oxygen monitors 150, 260, and 200 measure the oxygen contents of the exhaust gas from the OBOGS units 170, 180, and 190, the nitrogen-rich gas from the OBIGGS units 130 and 140, and the oxygen-rich gas from the OBOGS units 170, 180, and 190, respectively. It will of course be understood that a single oxygen monitor and appropriate control valves can replace the three oxygen monitors 150, 260, 200.

  The system shown in FIG. 1 is operated in four basic operating modes. That is, the first is a fuel tank deactivation mode, the second is an emergency oxygen mode for passengers, the third is a cargo compartment deactivation mode, and the fourth is an oxygen therapy mode.

  Using the OBIGGS unit to deactivate the fuel tank is the most common mode of operation, and is used all the time if there is no emergency condition. When deactivation of the cargo compartment is required, the inert gas is directed to the cargo compartment 330. In the fuel tank deactivation mode, air entering the gas separation system is directed to the OBIGGS units 130, 140 and immediately pressure is applied to the input air to begin supplying the deactivation gas to the fuel tank 320. The inert gas flows to the fuel tank 320 through the check valve 270, the normally open product gas selection valve 280, and the flow control orifice 290. The initial deactivation is replenished using the OBOGS unit exhaust gas. The opening / closing valve 125 is opened and the OBOGS units 170, 180, 190 are started. The valve 230 is also opened, and a predetermined amount is supplied from the OBOGS units 170, 180, 190 so that the exhaust gas from the OBOGS units 170, 180, 190 is about 12% oxygen. The valve 160 operates so that the exhaust gas from the OBOGS units 170, 180, and 190 flows into the fuel tank 320 through the selection valve 250 and the gas from the OBIGGS units 130 and 140 can be replenished.

  In the emergency oxygen mode for passengers whose passenger cabin is depressurized, the flow rate control units 370 and 380 are operated to supply oxygen from the cylinders 350 and 360 while the OBOGS units 170, 180, and 190 are ready for operation. Initially, valve 210 is closed until the proper oxygen concentration is reached, and then opened to supply passengers with oxygen. The oxygen therapy mode can be arbitrarily selected, and gas from one or more of the OBOGS units 170, 180, 190 is used to supply oxygen rich gas to passengers undergoing oxygen therapy. The gas valves 125 and 210 are opened, air is introduced into the OBOGS, and the product gas from the OBOGS exits. This optional mode requires an additional valve 215 to prevent oxygen from flowing through all of the passenger mask. The purge valve 225 is used to discharge the gas remaining in the system at the initial stage of emergency oxygen to the passenger. The control orifice 220 releases a predetermined amount of gas to the start-up state. To simply let out the exhaust gas, valve 230 is closed and valve 160 is in the normally open position.

  In the cargo compartment inactive mode, the gas from the OBIGGS units 130 and 140 and the exhaust gas from the OBOGS units 170, 180 and 190 are flowed to the cargo compartment 330. The valve 280 operates to flow gas from the OBIGGS units 130, 140 to the cargo compartment 330, and the valve 250 operates to flow exhaust gas from the OBOGS units 170, 180, 190 to the cargo chamber 330.

  Details of the OBIGGS units 130, 140 and the OBOGS units 170, 180, 190 are omitted for the sake of brevity. Details thereof are described in U.S. Pat. Nos. 4,870,960, 5,071,453, 5,766,310, 5,858,063, 6,063,169, and 6,394,089. The contents of these patents are all incorporated by reference.

  This completes the description illustrating the embodiment. Although the present invention has been described with reference to illustrating embodiments, many other variations and forms may be made within the scope of the present invention by those skilled in the art. It is. In particular, changes and modifications in the components and / or arrangements are possible within the scope of the foregoing disclosure, figures, and claims without departing from the spirit of the invention. Further, it will be apparent to those skilled in the art that alternatives can be used in addition to component and / or array changes and modifications.

1 is a block diagram of an oxygen / inert gas generator showing an embodiment of the present invention.

Claims (40)

An aircraft gas generation system including passenger cabins, fuel tanks and cargo compartments;
At least one aircraft on- board oxygen generation system (OBOGS) installed to receive a first air flow branched from the extracted air flow and generate oxygen, and a first branched from the extracted air flow At least one aircraft on- board inert gas generation system (OBIGGS) installed to receive two air streams to generate inert gas;
Connected to said on-board inert gas generation system (OBIGGS), also first directing each said cargo compartment and the fuel tank, the second supply path are connected, usually, the directing inert gas to the fuel tank and open to the first supply passage, and selector valve to open the emergency or closing the first supply path when necessary, the second supply passage for guiding the inert gas into the cargo hold,
Connected to said machine exhaust gas oxygen generation system (OBOGS), also the fuel tank and the cargo hold in the third, fourth supply passage is connected, it is open in order to release the normal exhaust gas, the fuel tank or closing the discharge upon inactivation of the cargo hold, the third supply passage for guiding the exhaust gas to the fuel tank or, and a control valve to open any one of the fourth supply passage leading to the cargo hold,
Gas generating system, wherein the second air stream with the first air flow ratio of oxygen and nitrogen are substantially the same.   2. The gas generation system according to claim 1, wherein the at least one on-board oxygen generation system (OBOGS) comprises two on-board oxygen generation systems (OBOGS).   2. The gas generation system according to claim 1, wherein the at least one on-machine inert gas generation system (OBIGGS) includes two on-machine inert gas generation systems (OBIGGS).   The gas generation system according to claim 1, wherein the inert gas is nitrogen.   The gas generation system of claim 1, further comprising an auxiliary oxygen source. The first control valve further includes a first control valve and a second control valve, wherein the first control valve selectively transmits exhaust gas from the at least one on-board oxygen generation system (OBOGS) to the atmosphere or to the second control valve. in out, the second control valve, claims, characterized in that to issue the exhaust gas from said at least one group airborne oxygen generating system (OBOGS) to one of two locations the cargo compartment and the fuel tank The gas generation system according to 1. Further comprises a heat exchanger for at least 1 group, receiving the bleed air flow at a first temperature, said to both the airborne oxygen generation system (OBOGS) and the on-board inert gas generation system (OBIGGS) The gas generation system according to claim 1, wherein the first air flow and the second air flow are output at a second temperature. In addition, it comprises at least one filter / water separator, receives the extracted air stream , and supplies filtered air with reduced moisture to the on-board oxygen generation system (OBOGS) and the on-board inert gas generation system (OBIGGS). The gas generation system according to claim 1 , wherein the first air flow and the second air flow are discharged to both.   6. The gas generation system according to claim 5, wherein the auxiliary oxygen source is at least one compressed oxygen tank.   The gas generation system according to claim 1, further comprising at least one oxygen monitor. A gas generation method used for aircraft including passenger cabins, fuel tanks and cargo compartments,
Oxygen is generated from a first air stream branched from an air stream extracted by at least one aircraft on- board oxygen generation system (OBOGS), and at least one aircraft on- board inert gas generation system (OBIGGS) Generating an inert gas from the second air stream branched from the air stream extracted at
It is connected to the on-board inert gas generation system (OBIGGS), also a selection valve first and second supply path that leads to each of the cargo compartment and the fuel tank is connected, usually the fuel tank with an inert gas It has opened the first supply passage leading to close the emergency or selection valve to the first supply path when necessary, the selection of the second supply path for guiding the inert gas into the cargo hold Open the valve
Is connected to the exhaust gas of the onboard oxygen generating system (OBOGS), also the control valve the third and fourth supply passage to each of the cargo compartment and the fuel tank is connected, open in order to release the normal exhaust gas Place the closed discharge control valve during deactivation of the fuel tank or the cargo bay, the third supply passage for guiding the exhaust gas to the fuel tank or, to any one of the fourth supply passage leading to the cargo hold A gas generation method characterized by opening a control valve.   12. The gas generation method according to claim 11, wherein the at least one on-board oxygen generation system (OBOGS) comprises two on-board oxygen generation systems (OBOGS).   12. The gas generation method according to claim 11, wherein the at least one on-machine inert gas generation system (OBIGGS) includes two on-machine inert gas generation systems (OBIGGS).   The gas generation method according to claim 11, wherein the inert gas is nitrogen.   The gas generating method according to claim 11, further comprising an auxiliary oxygen source. Furthermore an exhaust gas of the at least 1 group airborne oxygen generating system (OBOGS), characterized in that it comprises selectively out operations in any of the two places with the atmosphere or in the fuel tank the cargo hold The gas generation method according to claim 11. Receiving a further bleed air flow at a first temperature, the onboard oxygen generating system (OBOGS) and the on-board inert gas generation system (OBIGGS) said first airflow and said second airflow to both The gas generation method according to claim 11, further comprising an operation of taking out at a second temperature. Further, the filtered air, which has received the extracted air flow and reduced in water, is supplied to both the on-board oxygen generation system (OBOGS) and the on-board inert gas generation system (OBIGGS) . The gas generation method according to claim 11, comprising an operation of taking out as an air flow .   16. The gas generation method according to claim 15, wherein the auxiliary oxygen source supplies oxygen from at least one compressed oxygen tank.   The gas generation method according to claim 11, further comprising an operation of monitoring an oxygen concentration of at least one gas. An aircraft gas generation system including passenger cabins, fuel tanks and cargo compartments;
And extracted the first of the installed at least one group onboard oxygen generating system to receive a flow of air to generate oxygen for supplying the oxygen to the passenger compartment which is branched from the airflow (OBOGS), bled receiving a second air flow which is branched from the air flow to generate an inert gas, the on-board inert gas to the installed at least one group so as to supply the inert gas to the fuel tank or the cargo compartment Generation system (OBIGGS),
Connected to said on-board inert gas generation system (OBIGGS), also the first and second supply path that leads to each of the cargo compartment and the fuel tank is connected, usually, the directing inert gas to the fuel tank and open to the first supply passage, and selector valve to open the emergency or closing the first supply path when necessary, the second supply passage for guiding the inert gas into the cargo hold,
Connected to said exhaust gas onboard oxygen generating system (OBOGS), also the third and fourth supply passage for guiding the fuel tank and to each of the cargo compartment is connected, is open in order to release the normal exhaust gas, wherein close the released upon deactivation of the fuel tank or the cargo bay, the third supply passage for guiding the exhaust gas to the fuel tank or, and a control valve to open any one of the fourth supply passage leading to the cargo hold Prepared,
A gas generation system characterized in that the ratio of said first air stream and said second air stream oxygen and nitrogen are substantially the same.   The gas generation system according to claim 21, wherein the at least one on-board oxygen generation system (OBOGS) comprises two on-board oxygen generation systems (OBOGS).   22. The gas generation system according to claim 21, wherein the at least one on-machine inert gas generation system (OBIGGS) comprises two on-machine inert gas generation systems (OBIGGS).   The gas generation system according to claim 21, wherein the inert gas is nitrogen.   The gas generation system according to claim 21, further comprising an auxiliary oxygen source for selectively supplying oxygen to the passenger cabin.   The first control valve further includes a first control valve and a second control valve, the exhaust gas of the at least one on-board oxygen generation system (OBOGS) being selectively transmitted to the atmosphere or the second control valve. 23. The gas generation system according to claim 21, wherein the second control valve discharges the exhaust gas of the at least one on-board oxygen generation system (OBOGS) to either a fuel tank or a cargo compartment. Further comprises a heat exchanger for at least 1 group, receiving the bleed air flow at a first temperature, said to both the airborne oxygen generation system (OBOGS) and the on-board inert gas generation system (OBIGGS) The gas generation system according to claim 21, wherein the first air flow and the second air flow are output at a second temperature. In addition, it comprises at least one filter / water separator, receives the extracted air stream , and supplies filtered air with reduced moisture to the on-board oxygen generation system (OBOGS) and the on-board inert gas generation system (OBIGGS). The gas generation system according to claim 21, wherein the first air flow and the second air flow are discharged to both.   26. The gas generation system of claim 25, wherein the auxiliary oxygen source is at least one compressed oxygen tank.   The gas generation system according to claim 21, further comprising at least one oxygen monitor. A gas generation method used for aircraft including passenger cabins, fuel tanks and cargo compartments,
And extracted the first of the installed at least one group onboard oxygen generating system so that air flow oxygen is generated from feeding the oxygen into the passenger compartment which is branched from the airflow (OBOGS), bleed air flow second from the air flow to generate an inert gas, the installation has been at least a group onboard inert gas generation system to supply inert gas to the fuel tank or the cargo bay which is branched from the (OBIGGS )When,
The machine is connected to the inert gas generation systems (OBIGGS), and usually the selection valve first and second supply path that leads to each of the cargo compartment and the fuel tank are connected, the fuel tank with an inert gas It has opened the first supply passage leading to close the emergency or selection valve to the first supply path when necessary, the selection of the second supply path for guiding the inert gas into the cargo hold Open the valve
Connected to said exhaust gas onboard oxygen generating system (OBOGS), also open to release the third and fourth normal exhaust gas control valve supply passage is connected in guiding each of the cargo compartment and the fuel tank Place the closed discharge control valve during deactivation of the fuel tank or the cargo bay, the third supply passage for guiding the exhaust gas to the fuel tank or, to any one of the fourth supply passage leading to the cargo hold A gas generation method characterized by opening a control valve.   32. The gas generation method according to claim 31, wherein the at least one on-board oxygen generation system (OBOGS) comprises two on-board oxygen generation systems (OBOGS).   32. The gas generation method according to claim 31, wherein the at least one on-machine inert gas generation system (OBIGGS) comprises two on-machine inert gas generation systems (OBIGGS).   32. The gas generation method according to claim 31, wherein the inert gas is nitrogen.   32. The gas generation method according to claim 31, further comprising an auxiliary oxygen source for oxygen to be selectively supplied to the passenger cabin.   32. The gas according to claim 31, further comprising an operation of selectively discharging the exhaust gas of said at least one on-board oxygen generation system (OBOGS) to either the atmosphere or a fuel tank and a cargo compartment. How it occurs. Receiving a further bleed air flow at a first temperature, the onboard oxygen generating system (OBOGS) and the on-board inert gas generation system (OBIGGS) said first airflow and said second airflow to both the 32. The gas generation method according to claim 31, further comprising an operation of taking out at a second temperature. Further, the filtered air, which has received the extracted air flow and reduced in water, is supplied to both the on-board oxygen generation system (OBOGS) and the on-board inert gas generation system (OBIGGS) . 32. The gas generation method according to claim 31, further comprising an operation of taking out as an air flow .   36. The gas generation method according to claim 35, wherein the auxiliary oxygen source supplies oxygen from at least one compressed oxygen tank.   The gas generation method according to claim 31, further comprising an operation of monitoring an oxygen concentration of at least one gas.

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