CN107867404A - The apparatus and method of fuel tank inerting - Google Patents

The apparatus and method of fuel tank inerting Download PDF

Info

Publication number
CN107867404A
CN107867404A CN201711154585.2A CN201711154585A CN107867404A CN 107867404 A CN107867404 A CN 107867404A CN 201711154585 A CN201711154585 A CN 201711154585A CN 107867404 A CN107867404 A CN 107867404A
Authority
CN
China
Prior art keywords
fuel
fuel tank
hydrogen
heat exchanger
gas
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201711154585.2A
Other languages
Chinese (zh)
Inventor
李超越
冯诗愚
彭孝天
邵垒
刘卫华
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nanjing University of Aeronautics and Astronautics
Original Assignee
Nanjing University of Aeronautics and Astronautics
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nanjing University of Aeronautics and Astronautics filed Critical Nanjing University of Aeronautics and Astronautics
Priority to CN201711154585.2A priority Critical patent/CN107867404A/en
Publication of CN107867404A publication Critical patent/CN107867404A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00Arrangements in connection with fuel supply for power plant
    • B64D37/32Safety measures not otherwise provided for, e.g. preventing explosive conditions
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/40Application of hydrogen technology to transportation, e.g. using fuel cells

Abstract

The invention discloses fuel tank inerting unit and method, and the mixture of the air of fuel tanker gas-phase space and fuel vapor is produced into hydrogen and carbon dioxide in catalyst cracker by fuel vapor after dry filter, fuel oil refrigerated separation.Wherein hydrogen reacts generation water with oxygen in hydrogen-oxygen fuel cell, and collection can be used for flying Passenger On Board water after reaction is produced into water filtration, while fuel cell reaction can produce electric energy, and the electric energy available for the various electrical equipments of aircraft is fed.Have neither part nor lot in reaction inert gas such as carbon dioxide and nitrogen be passed through fuel tank gas-phase space can to fuel tank carry out inerting, ensure Flight Safety.The present apparatus, which has, to supply water, power supply and fuel tank inerting triple functions, and system flow is simple and reliable.

Description

The apparatus and method of fuel tank inerting
Technical field
The present invention relates to airplane equipment security fields, more particularly to the apparatus and method of fuel tank inerting.
Background technology
A large amount of aircraft accident analyses of causes are shown, fuel tanker catches fire to explode has great prestige to personnel and equipment safety The side of body, therefore how to reduce research emphasis of the fuel tanker explosion accident probability as aircraft safety problem.By largely testing Show with result of study, fuel tank inerting is a kind of fire-proof and explosion-proof mode of cost-effective fuel tank.
Fuel tank inerting refers to:Using inert gas such as nitrogen, carbon dioxide etc., fuel tank gas-phase space is filled with, is displaced The oxygen of gas-phase space, oxygen content is reduced, oxygen concentration is reached below Flammability limits.Therefore, even if running into outside igniting During source, blast on fire will not also occur for fuel tank.At present, airborne nitrogen inerting system processed is to use most extensive and ripe fuel tank inerting Technology, the technology utilize engine bleed, and by Middle hollow fiber membrane nitrogen and oxygen, the nitrogen-rich gas required for producing lead to Enter fuel tank gas-phase space, fuel tank gas-phase space oxygen concentration is reduced with this.But the technology requires very high, hollow fibre to bleed pressure The shortcomings of low efficiency, short life, easily block, pollution is produced to environment be present in dimension film nitrogen.
Therefore, there is atmospheric pressure requirement height in existing airborne nitrogen inerting system processed, and inerting effect is poor, the disagreeableness spy of environment Point.
The content of the invention
The invention provides fuel tank inerting unit and method, inerting can be carried out to airborne tank, without high-strength atmospheric pressure, And not generation environment pollutant.
To reach above-mentioned purpose, the present invention adopts the following technical scheme that:
Fuel tank inerting unit, including:Fuel tank(1), the first triple valve(2), oil eliminator(6), hydrogen-oxygen fuel cell(10), moisture From device(13), the second triple valve(205).
Fuel tank(1)Upper setting inert gas entrance, mixed gas outlet and fuel filler, the mixed gas outlet are passed through First triple valve(2), the first triple valve(2)Also connect atmospheric environment, the first triple valve(2)Connect oil eliminator(6), oil separation Device(6)Divide the connection fuel filler and fuel oil cracker(8), fuel oil cracker(8)And hydrogen-oxygen fuel cell (10)Anodic gas access road connection, the second triple valve(205)Connect hydrogen-oxygen fuel cell(10)Cathode gas inlet Passage, the second triple valve(205)Connect atmospheric environment, hydrogen-oxygen fuel cell(10)Mixed gas outlet passage connection water separation Device(13)Gas passage, the gas passage connects the inert gas entrance.
Further, the first triple valve(2)And oil eliminator(6)Between be sequentially connected first and be air-dried filter(3)、 Blower fan(4)And electronic cooler(5).
Further, oil eliminator(6)The first fuel pump is sequentially connected between the fuel filler(202)And check valve (201).
Further, oil eliminator(6)And hydrogen-oxygen fuel cell(10)Between be sequentially connected electronic heater(7), fuel oil Cracker(8), First Heat Exchanger(9).
Further, First Heat Exchanger(9)Provided with cold side aquaporin and hot side gas passage, the hot side gas passage connects Connect hydrogen-oxygen fuel cell(10), the cold side aquaporin passes through water pump(101)And separator(13)Aqueous water split tunnel Connection.
Further, hydrogen-oxygen fuel cell(10)And separator(13)Between be mounted with the second heat exchanger(12), second Triple valve(205)Connect and blast air to the second heat exchanger(12), the second heat exchanger(12)Connect air.
Further, the second triple valve(205)The front end of connection atmospheric environment sets gradually Filter dryer(203)And sky Air compressor(204).
Further, separator(13)And fuel tank(1)Between spark arrester is set(301).
Further, the first triple valve(2)And oil eliminator(6)Between be sequentially connected first and be air-dried filter(3)、 Blower fan(4)With the 3rd heat exchanger(14), the 3rd heat exchanger(14)Hot side gas passage be installed on blower fan(4)And oil eliminator (6)Gas passage between, the 3rd heat exchanger(14)Cold side gas channel inlet exports for ram-air, connects with atmospheric environment It is logical;
Oil eliminator(6)And First Heat Exchanger(9)Between set the 4th heat exchanger(15), the 4th heat exchanger(15)Cold side gas leads to Road is installed on oil eliminator(6)With fuel oil cracker(8)Between, the 4th heat exchanger(15)Hot side gas channel inlet and Two heat exchangers(12)Cold side gas path exit port connects, the 4th heat exchanger(15)Hot side gas path exit port connects with atmospheric environment It is logical.
Further, fuel oil injector(302)Outlet and fuel tank(1)Bottom connects, fuel oil injector(302)First enter Mouth and spark arrester(301)Outlet connection, fuel oil emitter(302)Second entrance and the second fuel pump(303)Outlet connection, second Fuel pump(303)Fuel filler and fuel tank(1)Bottom connects.
Further, fuel oil cracker(8)In catalyst be amorphous silicic aluminium and crystalline aluminosilicate Mixture.
Present invention also offers fuel tank inerting unit method, including:
S1, mixed gas are from fuel tank(1)Exit into the first triple valve(2)The tonifying Qi flowed into atmospheric ambient air is mixed Close;
S2, the first triple valve(2)Output mixed gas is passed through oil eliminator(6)Carry out Oil-gas Separation;
S3, oil eliminator(6)The mixed gas of output is passed through fuel oil cracker(8)Cracking reaction is carried out, obtains hydrogen, two Carbonoxide and unreacted nitrogen,
Hydrogen, carbon dioxide and unreacted nitrogen obtained by S4, S3 enter hydrogen-oxygen fuel cell(10)Anode, with hydrogen-oxygen fuel Battery(10)Air in negative electrode is reacted, and obtains vapor, carbon dioxide and nitrogen;
Water vapor condensation obtained by S5, S4 is in separator(13)Middle formation aqueous water, carbon dioxide and nitrogen pass through fuel tank(1) Inerting.
What the present invention had has the beneficial effect that:The present invention is by fuel catalytic cracking reaction by fuel tanker gas-phase space fuel oil It is steamed cracking to be decomposed into hydrogen and carbon dioxide, and electric energy and water are produced in hydrogen-oxygen fuel cell with oxygen using hydrogen, simultaneously Carbon dioxide enters fuel tank gas-phase space with having neither part nor lot in the nitrogen formation inert gas of reaction, and fuel tank gas-phase space oxygen is reduced with this Depth, fuel tank blast on fire is prevented, reach the purpose of protection fuel tank safety;The system can realize power supply, water supply and fuel tank inerting Triple functions;And whole system forms closed loop, avoids fuel vapor from being discharged directly into atmosphere pollution environment;In system not Engine bleed is needed, improves engine performance and energy utilization rate;To sum up, the present invention has simple in construction, using energy source Rate is high, it is environment-friendly the features such as.
Brief description of the drawings
Technical scheme in order to illustrate the embodiments of the present invention more clearly, it will use below required in embodiment Accompanying drawing is briefly described, it should be apparent that, drawings in the following description are only some embodiments of the present invention, for ability For the those of ordinary skill of domain, on the premise of not paying creative work, it can also be obtained according to these accompanying drawings other attached Figure.
Fig. 1 is the structure chart of embodiment one;
Fig. 2 is the structure chart of embodiment two;
Fig. 3 is the structure chart of embodiment three.
1- fuel tankers, the triple valves of 2- first, 3- first are air-dried filter, 4- blower fans, 5- electronic coolers, 6- oil Separator, 7 electronic heaters, 8- fuel oil crackers, 9- First Heat Exchangers, 10- hydrogen-oxygen fuel cells, 11- electrical equipments, The heat exchangers of 12- second, 13- separators, the heat exchangers of 14- the 3rd, the heat exchangers of 15- the 4th, 101- water pumps, 102, water filter, 103, storage tank, 201- check valves, 202 first fuel pumps, 203- the second air filtration driers, 204- air compressors, The triple valves of 205- second, 301- spark arresters, 302- fuel oil injectors, the fuel pumps of 303- second.
Embodiment
To make those skilled in the art more fully understand technical scheme, with reference to embodiment to this Invention is described in further detail.
Embodiment one
Fuel tank inerting unit, as shown in figure 1, including:Fuel tank 1, the first triple valve 2, first is air-dried filter 3, blower fan 4, Electronic cooler 5, oil eliminator 6, electronic heater 7, fuel oil cracker 8, First Heat Exchanger 9, hydrogen-oxygen fuel cell 10, Electrical equipment 11, the second heat exchanger 12, separator 13, water pump 101, water filter 102, storage tank 103, check valve 201, the One fuel pump 202, the second air filtration drier 203, air compressor 204, the second triple valve 205, spark arrester 301.
The mixed gas outlet of fuel tank 1 connects the first triple valve 2, and the first triple valve 2 also connects with atmospheric environment, and input is mixed Close gas and be air-dried filter 3 to first, remove the steam in mixed gas.
Mixed gas after water removal blasts electronic cooler 5 by blower fan 4, and the fuel oil vital qi in mixed gas is cooled to Liquid, 202 first fuel pumps are back to by the fluid oil passage of oil separation, then fuel tank 1 is returned to by check valve 201.
Mixed gas is passed through electronic heater 7 by the gas passage of oil eliminator 6 and preheated, and the gas of preheating flows into Fuel oil cracker 8 carries out catalytic cracking reaction, and hydrogen, carbon dioxide and nitrogen are produced after reaction.
Mixed gas is cooled by First Heat Exchanger 9, and the mixed gas after cooling is passed through the anode of hydrogen-oxygen fuel cell 10 In gas entrance passage, and the cathode gas inlet passage of hydrogen-oxygen fuel cell 10 air mixing, reaction obtain carbon dioxide, Vapor and nitrogen, and it is passed through the second heat exchanger 12.The electric energy output end mouth load electrical equipment 11 of hydrogen-oxygen fuel cell 10.
Second triple valve 205 is by the second air filtration drier 203, air compressor 204 and atmosphere, and the two or three The cathode gas inlet passage to hydrogen-oxygen fuel cell 10 and the second heat exchanger 12 blast air to port valve 205 respectively.
Mixed gas cools down in the second heat exchanger 12, and water vapor condensation is aqueous water, is separated by separator 13, stream Enter First Heat Exchanger 10, then water filter 9 is entered by First Heat Exchanger 10, finally flow into storage tank 103.
By the carbon dioxide and nitrogen of separator 13, spark arrester 301 is passed through, finally returns that the inert gas of fuel tank 1 Entrance.
The present embodiment additionally provides fuel tank inerting method, including:
S1, mixed gas are mixed from the tonifying Qi that fuel tank 1 exits into the first triple valve 2 with atmospheric ambient air flows into;
S2, the first triple valve 2 output mixed gas are passed through oil eliminator 6 and carry out Oil-gas Separation;
The mixed gas that S3, oil eliminator 6 export is passed through fuel oil cracker 8 and carries out cracking reaction, obtains hydrogen, titanium dioxide Carbon and unreacted nitrogen,
Hydrogen, carbon dioxide and unreacted nitrogen obtained by S4, S3 enter the anode of hydrogen-oxygen fuel cell 10, with hydrogen-oxygen fuel electricity Air in the negative electrode of pond 10 is reacted, and obtains vapor, carbon dioxide and nitrogen;
Water vapor condensation obtained by S5, S4 forms aqueous water in separator 13, and it is lazy that carbon dioxide and nitrogen are passed through fuel tank 1 Change.
Embodiment two
Fuel tank inerting unit, as shown in Fig. 2 including:Fuel tank 1, the first triple valve 2, first is air-dried filter 3, blower fan 4, 3rd heat exchanger 14, oil eliminator 6, the 4th heat exchanger 15, fuel oil cracker 8, First Heat Exchanger 9, hydrogen-oxygen fuel cell 10, electrical equipment 11, the second heat exchanger 12, separator 13, water pump 101, water filter 102, storage tank 103, check valve 201, the first fuel pump 202, the second air filtration drier 203, air compressor 204, the second triple valve 205, spark arrester 301。
The mixed gas outlet of fuel tank 1 connects the first triple valve 2, and the first triple valve 2 also connects with atmospheric environment, and input is mixed Close gas and be air-dried filter 3 to first, remove the steam in mixed gas.
Mixed gas after water removal blasts the 3rd heat exchanger 14 by blower fan 4, and the cold side gas passage of the 3rd heat exchanger 14 enters Mouth is ram-air, and outlet connects with atmospheric environment, is cooled down in mixed gas in the 3rd heat exchanger 14, fuel oil vital qi is cooled For liquid, 202 first fuel pumps are back to by the fluid oil passage of oil separation, then fuel tank 1 is returned to by check valve 201.
Mixed gas is passed through the 4th heat exchanger 15, the cold side gas of the 4th heat exchanger 15 by the gas passage of oil eliminator 6 Passage is installed between oil eliminator 6 and fuel oil cracker 8, the hot side gas channel inlet and second of the 4th heat exchanger 15 The cold side gas path exit port of heat exchanger 12 connects, and the hot side gas path exit port of the 4th heat exchanger 15 connects with atmospheric environment.Mixing Gas is preheated in the 4th heat exchanger 15, and the gas of preheating flows into fuel oil cracker 8 and carries out catalytic cracking reaction, instead Should after produce hydrogen, carbon dioxide and nitrogen.
Mixed gas is cooled by First Heat Exchanger 9, and the mixed gas after cooling is passed through the anode of hydrogen-oxygen fuel cell 10 In gas entrance passage, and the cathode gas inlet passage of hydrogen-oxygen fuel cell 10 air mixing, reaction obtain carbon dioxide, Vapor and nitrogen, and it is passed through the second heat exchanger 12.The electric energy output end mouth load electrical equipment 11 of hydrogen-oxygen fuel cell 10.
Second triple valve 205 is by the second air filtration drier 203, air compressor 204 and atmosphere, and the two or three The cathode gas inlet passage to hydrogen-oxygen fuel cell 10 and the second heat exchanger 12 blast air to port valve 205 respectively.
Mixed gas cools down in the second heat exchanger 12, and water vapor condensation is aqueous water, is separated by separator 13, stream Enter First Heat Exchanger 10, then water filter 9 is entered by First Heat Exchanger 10, finally flow into storage tank 103.
By the carbon dioxide and nitrogen of separator 13, spark arrester 301 is passed through, finally returns that the inert gas of fuel tank 1 Entrance.
The present embodiment additionally provides fuel tank inerting method, including:
S1, mixed gas are mixed from the tonifying Qi that fuel tank 1 exits into the first triple valve 2 with atmospheric ambient air flows into;
S2, the first triple valve 2 output mixed gas are passed through oil eliminator 6 and carry out Oil-gas Separation;
The mixed gas that S3, oil eliminator 6 export is passed through fuel oil cracker 8 and carries out cracking reaction, obtains hydrogen, titanium dioxide Carbon and unreacted nitrogen,
Hydrogen, carbon dioxide and unreacted nitrogen obtained by S4, S3 enter the anode of hydrogen-oxygen fuel cell 10, with hydrogen-oxygen fuel electricity Air in the negative electrode of pond 10 is reacted, and obtains vapor, carbon dioxide and nitrogen;
Water vapor condensation obtained by S5, S4 forms aqueous water in separator 13, and it is lazy that carbon dioxide and nitrogen are passed through fuel tank 1 Change.
Embodiment three
Fuel tank inerting unit, as shown in figure 3, including:Fuel tank 1, the first triple valve 2, first is air-dried filter 3, blower fan 4, 3rd heat exchanger 14, oil eliminator 6, the 4th heat exchanger 15, fuel oil cracker 8, First Heat Exchanger 9, hydrogen-oxygen fuel cell 10, electrical equipment 11, the second heat exchanger 12, separator 13, water pump 101, water filter 102, storage tank 103, check valve 201, the first fuel pump 202, the second air filtration drier 203, air compressor 204, the second triple valve 205, spark arrester 301, fuel oil injector 302, the second fuel pump 303.
The mixed gas outlet of fuel tank 1 connects the first triple valve 2, and the first triple valve 2 also connects with atmospheric environment, and input is mixed Close gas and be air-dried filter 3 to first, remove the steam in mixed gas.
Mixed gas after water removal blasts the 3rd heat exchanger 14 by blower fan 4, and the cold side gas passage of the 3rd heat exchanger 14 enters Mouth is ram-air, and outlet connects with atmospheric environment, is cooled down in mixed gas in the 3rd heat exchanger 14, fuel oil vital qi is cooled For liquid, 202 first fuel pumps are back to by the fluid oil passage of oil separation, then fuel tank 1 is returned to by check valve 201.
Mixed gas is passed through the 4th heat exchanger 15, the cold side gas of the 4th heat exchanger 15 by the gas passage of oil eliminator 6 Passage is installed between oil eliminator 6 and fuel oil cracker 8, the hot side gas channel inlet and second of the 4th heat exchanger 15 The cold side gas path exit port of heat exchanger 12 connects, and the hot side gas path exit port of the 4th heat exchanger 15 connects with atmospheric environment.Mixing Gas is preheated in the 4th heat exchanger 15, and the gas of preheating flows into fuel oil cracker 8 and carries out catalytic cracking reaction, instead Should after produce hydrogen, carbon dioxide and nitrogen.
Mixed gas is cooled by First Heat Exchanger 9, and the mixed gas after cooling is passed through the anode of hydrogen-oxygen fuel cell 10 In gas entrance passage, and the cathode gas inlet passage of hydrogen-oxygen fuel cell 10 air mixing, reaction obtain carbon dioxide, Vapor and nitrogen, and it is passed through the second heat exchanger 12.The electric energy output end mouth load electrical equipment 11 of hydrogen-oxygen fuel cell 10.
Second triple valve 205 is by the second air filtration drier 203, air compressor 204 and atmosphere, and the two or three The cathode gas inlet passage to hydrogen-oxygen fuel cell 10 and the second heat exchanger 12 blast air to port valve 205 respectively.
Mixed gas cools down in the second heat exchanger 12, and water vapor condensation is aqueous water, is separated by separator 13, stream Enter First Heat Exchanger 10, then water filter 9 is entered by First Heat Exchanger 10, finally flow into storage tank 103.
By the carbon dioxide and nitrogen of separator 13, spark arrester 301 is passed through.Gas is passed through combustion by spark arrester 301 Oily injector 302, the outlet of fuel oil injector 302 connect with the bottom of fuel tank 1, the second entrance of fuel oil injector 302 and the second fuel oil The outlet of pump 303 connection, the fuel filler of the second fuel pump 303 connect with the bottom of fuel tank 1, the inert gas in fuel oil injector 302 It is sufficiently mixed with fuel oil, and enters fuel tank 1, constantly fuel oil is washed, oxygen content in fuel oil can be reduced, and then can subtract Few fuel tank gas-phase space oxygen content, reach the purpose of inerting
The present embodiment additionally provides fuel tank inerting method, including:
S1, mixed gas are mixed from the tonifying Qi that fuel tank 1 exits into the first triple valve 2 with atmospheric ambient air flows into;
S2, the first triple valve 2 output mixed gas are passed through oil eliminator 6 and carry out Oil-gas Separation;
The mixed gas that S3, oil eliminator 6 export is passed through fuel oil cracker 8 and carries out cracking reaction, obtains hydrogen, titanium dioxide Carbon and unreacted nitrogen,
Hydrogen, carbon dioxide and unreacted nitrogen obtained by S4, S3 enter the anode of hydrogen-oxygen fuel cell 10, with hydrogen-oxygen fuel electricity Air in the negative electrode of pond 10 is reacted, and obtains vapor, carbon dioxide and nitrogen;
Water vapor condensation obtained by S5, S4 forms aqueous water in separator 13, and it is lazy that carbon dioxide and nitrogen are passed through fuel tank 1 Change.
What the present invention had has the beneficial effect that:The present invention is by fuel catalytic cracking reaction by fuel tanker gas-phase space fuel oil It is steamed cracking to be decomposed into hydrogen and carbon dioxide, and electric energy and water are produced in hydrogen-oxygen fuel cell with oxygen using hydrogen, simultaneously Carbon dioxide enters fuel tank gas-phase space with having neither part nor lot in the nitrogen formation inert gas of reaction, and fuel tank gas-phase space oxygen is reduced with this Depth, fuel tank blast on fire is prevented, reach the purpose of protection fuel tank safety;The system can realize power supply, water supply and fuel tank inerting Triple functions;And whole system forms closed loop, avoids fuel vapor from being discharged directly into atmosphere pollution environment;In system not Engine bleed is needed, improves engine performance and energy utilization rate;To sum up, the present invention has simple in construction, using energy source Rate is high, it is environment-friendly the features such as.
The foregoing is only a specific embodiment of the invention, but protection scope of the present invention is not limited thereto, any Those familiar with the art the invention discloses technical scope in, the change or replacement that can readily occur in, all should It is included within the scope of the present invention.Therefore, protection scope of the present invention should be defined by scope of the claims.

Claims (12)

1. fuel tank inerting unit, it is characterised in that including:Fuel tank(1), the first triple valve(2), oil eliminator(6), hydrogen-oxygen fuel Battery(10), separator(13), the second triple valve(205), fuel tank(1)Upper setting inert gas entrance, mixed gas outlet And fuel filler, the mixed gas outlet are passed through the first triple valve(2), the first triple valve(2)Also connect atmospheric environment, first Triple valve(2)Connect oil eliminator(6), oil eliminator(6)Divide the connection fuel filler and fuel oil cracker(8), combustion Oily cracker(8)And hydrogen-oxygen fuel cell(10)Anodic gas access road connection, the second triple valve(205)Connect hydrogen Oxygen fuel cell(10)Cathode gas inlet passage, the second triple valve(205)Connect atmospheric environment, hydrogen-oxygen fuel cell(10) Mixed gas outlet passage connection separator(13)Gas passage, the gas passage connects the inert gas and enters Mouthful.
2. fuel tank inerting unit according to claim 1, it is characterised in that the first triple valve(2)And oil eliminator(6)It Between be sequentially connected first and be air-dried filter(3), blower fan(4)And electronic cooler(5).
3. fuel tank inerting unit according to claim 1, it is characterised in that oil eliminator(6)With the fuel filler it Between be sequentially connected the first fuel pump(202)And check valve(201).
4. fuel tank inerting unit according to claim 1, it is characterised in that oil eliminator(6)And hydrogen-oxygen fuel cell (10)Between be sequentially connected electronic heater(7), fuel oil cracker(8), First Heat Exchanger(9).
5. fuel tank inerting unit according to claim 4, it is characterised in that First Heat Exchanger(9)Provided with cold side aquaporin With hot side gas passage, the hot side gas passage connects hydrogen-oxygen fuel cell(10), the cold side aquaporin passes through water pump (101)And separator(13)Aqueous water split tunnel connection.
6. fuel tank inerting unit according to claim 1, it is characterised in that hydrogen-oxygen fuel cell(10)And separator (13)Between be mounted with the second heat exchanger(12), the second triple valve(205)Connect and blast air to the second heat exchanger(12), the Two heat exchangers(12)Connect air.
7. fuel tank inerting unit according to claim 1, it is characterised in that the second triple valve(205)Connect atmospheric environment Front end set gradually Filter dryer(203)And air compressor(204).
8. fuel tank inerting unit according to claim 1, it is characterised in that separator(13)And fuel tank(1)Between set Put spark arrester(301).
9. fuel tank inerting unit according to claim 1, it is characterised in that the first triple valve(2)And oil eliminator(6)It Between be sequentially connected first and be air-dried filter(3), blower fan(4)With the 3rd heat exchanger(14), the 3rd heat exchanger(14)Hot side Gas passage is installed on blower fan(4)And oil eliminator(6)Gas passage between, the 3rd heat exchanger(14)Cold side gas passage enters Mouth exports for ram-air, is connected with atmospheric environment;
Oil eliminator(6)And First Heat Exchanger(9)Between set the 4th heat exchanger(15), the 4th heat exchanger(15)Cold side gas leads to Road is installed on oil eliminator(6)With fuel oil cracker(8)Between, the 4th heat exchanger(15)Hot side gas channel inlet and Two heat exchangers(12)Cold side gas path exit port connects, the 4th heat exchanger(15)Hot side gas path exit port connects with atmospheric environment It is logical.
10. fuel tank inerting unit according to claim 1, it is characterised in that fuel oil injector(302)Outlet and fuel tank (1)Bottom connects, fuel oil injector(302)First entrance and spark arrester(301)Outlet connection, fuel oil emitter(302) Two entrances and the second fuel pump(303)Outlet connection, the second fuel pump(303)Fuel filler and fuel tank(1)Bottom connects.
11. fuel tank inerting unit according to claim 1, it is characterised in that fuel oil cracker(8)In catalyst For amorphous silicic aluminium and the mixture of crystalline aluminosilicate.
12. fuel tank inerting unit method, it is characterised in that:Step is as follows
S1, mixed gas are from fuel tank(1)Exit into the first triple valve(2)The tonifying Qi flowed into atmospheric ambient air is mixed Close;
S2, the first triple valve(2)Output mixed gas is passed through oil eliminator(6)Carry out Oil-gas Separation;
S3, oil eliminator(6)The mixed gas of output is passed through fuel oil cracker(8)Cracking reaction is carried out, obtains hydrogen, two Carbonoxide and unreacted nitrogen,
Hydrogen, carbon dioxide and unreacted nitrogen obtained by S4, S3 enter hydrogen-oxygen fuel cell(10)Anode, with hydrogen-oxygen fuel Battery(10)Air in negative electrode is reacted, and obtains vapor, carbon dioxide and nitrogen;
Water vapor condensation obtained by S5, S4 is in separator(13)Middle formation aqueous water, carbon dioxide and nitrogen pass through fuel tank(1) Inerting.
CN201711154585.2A 2017-11-20 2017-11-20 The apparatus and method of fuel tank inerting Pending CN107867404A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711154585.2A CN107867404A (en) 2017-11-20 2017-11-20 The apparatus and method of fuel tank inerting

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711154585.2A CN107867404A (en) 2017-11-20 2017-11-20 The apparatus and method of fuel tank inerting

Publications (1)

Publication Number Publication Date
CN107867404A true CN107867404A (en) 2018-04-03

Family

ID=61754158

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711154585.2A Pending CN107867404A (en) 2017-11-20 2017-11-20 The apparatus and method of fuel tank inerting

Country Status (1)

Country Link
CN (1) CN107867404A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108639361A (en) * 2018-06-25 2018-10-12 南京航空航天大学 A kind of fuel-tank inert gas device of joint plasma and photocatalysis technology
CN109018387A (en) * 2018-09-03 2018-12-18 南京航空航天大学 A kind of fuel tanker inerting unit and its method using high pressure water separation regenerative air cycle cooling system
CN109441637A (en) * 2018-09-03 2019-03-08 北京航空航天大学 A kind of aircraft using nitrogen supercharging fuel tank is had more than needed electric integrated system and method
CN110053780A (en) * 2019-04-30 2019-07-26 南京航空航天大学 It is a kind of to flow to transform oxygen consumption type inerting system
CN111071465A (en) * 2020-01-06 2020-04-28 南京航空航天大学 Low-temperature refrigeration nitrogen-making oil tank inerting system and working method thereof
CN111140366A (en) * 2018-11-02 2020-05-12 通用电气公司 Fuel delivery system with fuel deoxygenation unit
CN111994289A (en) * 2020-09-02 2020-11-27 重庆交通大学 Aircraft fuel tank inerting system and inerting method
US11945600B2 (en) 2018-11-02 2024-04-02 General Electric Company Fuel delivery system having a fuel oxygen reduction unit

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005054888A1 (en) * 2005-11-17 2007-07-12 Airbus Deutschland Gmbh System useful in an aircraft, comprises an oxygen enrichment device for generating oxygen-enriched air, a fuel cell system with a fuel cell using the oxygen-enriched air, and a sensor that detects the oxygen in the oxygen-enriched air
CN104843189A (en) * 2015-04-22 2015-08-19 南京航空航天大学 Catalytic combustion inerting oil tank device and method thereof
RU2014141050A (en) * 2012-03-12 2016-05-10 Л'Эр Ликид, Сосьете Аноним Пур Л'Этюд Э Л'Эксплуатасьон Де Проседе Жорж Клод INERTING DEVICE, RESERVOIR AND AIRCRAFT EQUIPPED WITH SUCH A DEVICE AND THE RELATED METHOD
CN106741984A (en) * 2017-01-03 2017-05-31 南京航空航天大学 A kind of system and its method of work of catalytic reforming inerting aircraft fuel tank
CN106762270A (en) * 2016-12-27 2017-05-31 南京航空航天大学 A kind of air separates inerting automotive oil tank device and its method of work
US20170160251A1 (en) * 2015-12-03 2017-06-08 Zodiac Aerotechnics Aircraft Fuel Tank Inerting System Adapted To Compute The Quantity Of Oxygen Present In An Inerting Gas Injected Into Said Tank
CN208036635U (en) * 2017-11-20 2018-11-02 南京航空航天大学 The device of fuel tank inerting

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005054888A1 (en) * 2005-11-17 2007-07-12 Airbus Deutschland Gmbh System useful in an aircraft, comprises an oxygen enrichment device for generating oxygen-enriched air, a fuel cell system with a fuel cell using the oxygen-enriched air, and a sensor that detects the oxygen in the oxygen-enriched air
RU2014141050A (en) * 2012-03-12 2016-05-10 Л'Эр Ликид, Сосьете Аноним Пур Л'Этюд Э Л'Эксплуатасьон Де Проседе Жорж Клод INERTING DEVICE, RESERVOIR AND AIRCRAFT EQUIPPED WITH SUCH A DEVICE AND THE RELATED METHOD
CN104843189A (en) * 2015-04-22 2015-08-19 南京航空航天大学 Catalytic combustion inerting oil tank device and method thereof
US20170160251A1 (en) * 2015-12-03 2017-06-08 Zodiac Aerotechnics Aircraft Fuel Tank Inerting System Adapted To Compute The Quantity Of Oxygen Present In An Inerting Gas Injected Into Said Tank
CN106762270A (en) * 2016-12-27 2017-05-31 南京航空航天大学 A kind of air separates inerting automotive oil tank device and its method of work
CN106741984A (en) * 2017-01-03 2017-05-31 南京航空航天大学 A kind of system and its method of work of catalytic reforming inerting aircraft fuel tank
CN208036635U (en) * 2017-11-20 2018-11-02 南京航空航天大学 The device of fuel tank inerting

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108639361A (en) * 2018-06-25 2018-10-12 南京航空航天大学 A kind of fuel-tank inert gas device of joint plasma and photocatalysis technology
CN108639361B (en) * 2018-06-25 2023-09-26 南京航空航天大学 Fuel tank inerting device combining plasma and photocatalysis technologies
CN109018387A (en) * 2018-09-03 2018-12-18 南京航空航天大学 A kind of fuel tanker inerting unit and its method using high pressure water separation regenerative air cycle cooling system
CN109441637A (en) * 2018-09-03 2019-03-08 北京航空航天大学 A kind of aircraft using nitrogen supercharging fuel tank is had more than needed electric integrated system and method
CN109441637B (en) * 2018-09-03 2020-07-24 北京航空航天大学 Airplane surplus power integrated system and method for pressurizing oil tank by using nitrogen
CN111140366A (en) * 2018-11-02 2020-05-12 通用电气公司 Fuel delivery system with fuel deoxygenation unit
US11945600B2 (en) 2018-11-02 2024-04-02 General Electric Company Fuel delivery system having a fuel oxygen reduction unit
CN110053780A (en) * 2019-04-30 2019-07-26 南京航空航天大学 It is a kind of to flow to transform oxygen consumption type inerting system
CN110053780B (en) * 2019-04-30 2024-04-12 南京航空航天大学 Flow direction conversion type oxygen consumption inerting system
CN111071465A (en) * 2020-01-06 2020-04-28 南京航空航天大学 Low-temperature refrigeration nitrogen-making oil tank inerting system and working method thereof
CN111994289A (en) * 2020-09-02 2020-11-27 重庆交通大学 Aircraft fuel tank inerting system and inerting method

Similar Documents

Publication Publication Date Title
CN107867404A (en) The apparatus and method of fuel tank inerting
CN106741984B (en) A kind of system and its working method of catalytic reforming inerting aircraft fuel tank
CN104843188B (en) A kind of aircraft fuel-tank inert gas device based on catalytic oxidation technologies
CN104843189B (en) A kind of devices and methods therefor for being catalyzed burning inerting fuel tank
US8499567B2 (en) Hybrid fuel tank inerting system
US9102416B1 (en) Inert gas generating system
CN102755870B (en) Double-flow-mode fuel oil ground pre-washing method and device thereof
CN108045587B (en) Waste heat recovery system of oxygen consumption type inerting fuel tank based on thermoelectric generation technology
CN108639359B (en) Oxygen consumption type fuel tank inerting system with ion migration membrane
CN109018387A (en) A kind of fuel tanker inerting unit and its method using high pressure water separation regenerative air cycle cooling system
CN108945476A (en) A kind of airborne oxygen-nitrogen gas generating system processed based on chemical cycle air separation technology
CN207956079U (en) A kind of oxygen consumption type inerting fuel tank residual neat recovering system
CN107158914A (en) A kind of device for recovering oil and gas that Volatile Gas in Oil Tank is transformed into solid state gas hydrate
CN112937882A (en) Aircraft power supply and fuel tank inerting integrated system and aircraft fuel tank inerting method
CN208036635U (en) The device of fuel tank inerting
CN101767652B (en) Fuel washing device for aircraft refueling vehicle
CN106494779B (en) A kind of device and its working method of the inerting tank service truck oil tank that burns
CN201168455Y (en) Low-temperature condensation vapour recovery unit
CN208393638U (en) A kind of device based on photocatalytic oxidation inerting fuel tank
CN103456973A (en) Air supply system used for fuel cell and capable of strengthening safety discharge of hydrogen gas
CN108163215A (en) A kind of oxygen consumption type inerting fuel tank residual neat recovering system
CN218632200U (en) Battery thermal runaway flue gas adsorption equipment and battery
CN207909980U (en) A kind of improved fuel cell pipeline device
CN207965700U (en) The device of waste-heat power generation in a kind of fuel-tank inert gas system using aircraft
CN208530861U (en) A kind of fuel-tank inert gas device for combining plasma and photocatalysis technology

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination