CN109367809A - Interplane fuel oil delivery method and its equipment - Google Patents
Interplane fuel oil delivery method and its equipment Download PDFInfo
- Publication number
- CN109367809A CN109367809A CN201810935736.6A CN201810935736A CN109367809A CN 109367809 A CN109367809 A CN 109367809A CN 201810935736 A CN201810935736 A CN 201810935736A CN 109367809 A CN109367809 A CN 109367809A
- Authority
- CN
- China
- Prior art keywords
- fuel
- oil
- aircraft
- interplane
- fuel oil
- 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
Links
- 239000000295 fuel oil Substances 0.000 title claims abstract description 80
- 238000002716 delivery method Methods 0.000 title claims abstract description 14
- 239000003921 oil Substances 0.000 claims abstract description 85
- 239000000446 fuel Substances 0.000 claims abstract description 63
- 238000005086 pumping Methods 0.000 claims abstract description 53
- 238000000605 extraction Methods 0.000 claims abstract description 28
- 238000000034 method Methods 0.000 claims abstract description 10
- 238000001514 detection method Methods 0.000 claims abstract description 8
- 239000002828 fuel tank Substances 0.000 claims description 25
- 238000011109 contamination Methods 0.000 claims description 16
- 230000000813 microbial effect Effects 0.000 claims description 16
- KFZMGEQAYNKOFK-UHFFFAOYSA-N Isopropanol Chemical compound CC(C)O KFZMGEQAYNKOFK-UHFFFAOYSA-N 0.000 claims description 6
- 230000001681 protective effect Effects 0.000 claims description 6
- 239000003599 detergent Substances 0.000 claims description 5
- 230000005540 biological transmission Effects 0.000 claims description 4
- 244000005700 microbiome Species 0.000 claims description 4
- 239000012153 distilled water Substances 0.000 claims description 3
- 239000010761 intermediate fuel oil Substances 0.000 claims description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 3
- 238000012423 maintenance Methods 0.000 abstract description 4
- 238000012797 qualification Methods 0.000 abstract 1
- 238000007689 inspection Methods 0.000 description 4
- 230000006378 damage Effects 0.000 description 3
- 239000002699 waste material Substances 0.000 description 3
- ZKHQWZAMYRWXGA-KQYNXXCUSA-J ATP(4-) Chemical compound C1=NC=2C(N)=NC=NC=2N1[C@@H]1O[C@H](COP([O-])(=O)OP([O-])(=O)OP([O-])([O-])=O)[C@@H](O)[C@H]1O ZKHQWZAMYRWXGA-KQYNXXCUSA-J 0.000 description 2
- ZKHQWZAMYRWXGA-UHFFFAOYSA-N Adenosine triphosphate Natural products C1=NC=2C(N)=NC=NC=2N1C1OC(COP(O)(=O)OP(O)(=O)OP(O)(O)=O)C(O)C1O ZKHQWZAMYRWXGA-UHFFFAOYSA-N 0.000 description 2
- TTWYZDPBDWHJOR-IDIVVRGQSA-L adenosine triphosphate disodium Chemical compound [Na+].[Na+].C1=NC=2C(N)=NC=NC=2N1[C@@H]1O[C@H](COP(O)(=O)OP(O)(=O)OP([O-])([O-])=O)[C@@H](O)[C@H]1O TTWYZDPBDWHJOR-IDIVVRGQSA-L 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000003208 petroleum Substances 0.000 description 2
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/28—Liquid-handling installations specially adapted for fuelling stationary aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/40—Maintaining or repairing aircraft
Abstract
The present invention provides a kind of interplane fuel oil delivery methods, comprising the following steps: (1) detection by the fuel qualities of oil pumping aircraft is confirmed whether that interplane fuel oil conveying can be carried out；(2) by oil pumping aircraft fuel oil quality it is up to standard after, it will be attached by the Fuel Bleed Valve of oil pumping aircraft with by the oiling valve of tanker aircraft, it is pumped to by oil pumping aircraft using pressure oil pumping mode, it is refueled simultaneously to by tanker aircraft using pressure filling mode, realizes the conveying of interplane fuel oil.The fuel oil conveying of two interplanes may be implemented in the method for the present invention, makes to be pumped and aircraft oil extraction and is refueled while being carried out by tanker aircraft, the airborne Fuel Remained of qualification can be put back into, improve the utilization rate of aircraft fuel oil, substantially reduce the operation cost of aircraft；For aircraft maintenance enterprise, it is not necessary to carry out oil extraction using proprietary aviation fuel vehicle and fuel feeding works, can reduce by two aircrafts simultaneously because of what oil extraction and fuel feeding worked and stop field time, reduce aircraft maintenance cost.
Description
Technical field
The present invention relates to a kind of interplane fuel oil delivery methods, and the invention further relates to what is conveyed for interplane fuel oil to set
It is standby.
Background technique
Airfield approach need to discharge the Fuel Remained in fuel tank when repairing, and the fuel oil of discharge is frequently as waste oil low price
Processing causes vast resources waste in this way.Meanwhile during discharging fuel oil, it is also necessary to be carried out using proprietary aviation fuel vehicle
Oil extraction, subsequent aircraft fuel feeding are also required to aviation fuel vehicle, increase a large amount of work and cost in this way.
Summary of the invention
First technical problem to be solved by this invention, is just to provide a kind of interplane fuel oil delivery method.
Second technical problem to be solved by this invention is just to provide a kind of interplane fuel oil for being exclusively used in the method
Conveying equipment.
Using method and apparatus of the invention, two interplane fuel oils may be implemented and directly transport, reduces fuel oil direct emission
Waste reduces the scheduling and use of the oil extraction of aviation fuel vehicle and oiling, reduces cost, while shortening the aircraft waiting time.
Above-mentioned first technical problem is solved, the technical solution adopted in the present invention is as follows:
A kind of interplane fuel oil delivery method, comprising the following steps:
(1) detection by the fuel qualities of oil pumping aircraft is confirmed whether that interplane fuel oil conveying can be carried out；
(2) by oil pumping aircraft fuel oil quality it is up to standard after, by by the Fuel Bleed Valve of oil pumping aircraft by fuel delivery apparatus with
It is attached, is pumped to by oil pumping aircraft using pressure oil pumping mode, while to being added by the oiling valve of tanker aircraft
Oily aircraft is refueled using pressure filling mode, realizes the conveying of interplane fuel oil.
Step (1) the intermediate fuel oil quality refers to fuel oil microbial contamination grade.
Further, the fuel oil microbial contamination grade is divided into slight pollution, general pollution and serious pollution.
Fuel oil microbial contamination grade is according to " the fuel tanker microbial contamination guide of International Air Transport Association (IATA)
Material " it is evaluated: 1, slight pollution: less than 1000RLU/ rise sample；2, general pollution: 1000-5000RLU/ rises sample；3,
Serious pollution: greater than 5000RLU/ rises sample.
Aviation Fuel microbial contamination detection principle be by be quantitatively evaluated sample in ATP (adenosine triphosphate) content,
To assess the pollution level of microorganism.Quantitative reading of the ATP in instrument shows as RLU value.
It is slight dirt that the fuel qualities that interplane fuel oil conveying can be carried out in the step (1), which are microbial contamination grade,
Dye.
Detection fuel qualities use Aviation Fuel microbial contamination detection device HY-LITE2017 in the step (1).
Step (2) the intermediate fuel oil conveying equipment is equipped with electrostatic line, and fuel delivery apparatus was being connect with aircraft valve
Cheng Zhong, while electrostatic line being connect with aircraft valve.
Before carrying out the conveying of interplane fuel oil in the step (2), carried out clearly with connector of the detergent to fuel delivery apparatus
It washes, the detergent is mixed by distilled water and isopropanol by the volume ratio of 1:3~4.
It is pumped by oil pumping aircraft using pressure in the step (2) and pressure filling detailed process is used such as by tanker aircraft
Under: it closes by all fuel pump of fuel tank of tanker aircraft, oiling mode is selected on aircraft refuelling-oil extraction panel, open target
The fuel oil threshold switch of oiling fuel tank closes the fuel oil threshold switch of other non-refuelling fuel tanks；By oil pumping aircraft refuelling-oil extraction
Oil extraction mode is selected on panel, opens and intersects supply valve valve, is opened by the centre tank the automatic control of pump system of oil pumping aircraft,
The fuel pump of target oil extraction fuel tank is opened, while being carried out by the oil pumping of oil pumping aircraft pressure and by tanker aircraft pressure filling, directly
Targeted fuel capacity is extremely reached by tanker aircraft target oiling fuel tank；It closes by the fuel oil of oil pumping Aircraft Targets oil extraction fuel tank
Pump is closed by the centre tank the automatic control of pump system of oil pumping aircraft；Refueled by tanker aircraft-oil extraction panel on select close
Mode, open mode protective device close target oiling fuel oil in fuel tank threshold switch, open fuel valve protective device.
Further, it in interplane fuel oil transmission process, is carried out to by the practical oil drain quantity of oil pumping aircraft and display oil drain quantity
Difference inspection, while difference inspection is carried out to by the practical volume read-out of tanker aircraft and display volume read-out.
Further, in interplane fuel oil transmission process, by the fuel pump outlet pressure of oil pumping Aircraft Targets oil extraction fuel tank
Power control is no more than 30PSI.
Further, the volume read-out by tanker aircraft according to by the maximum capacity of each fuel tank of tanker aircraft,
Always fuel capacity and total fuel remaining determination by oil pumping extension set.
Above-mentioned second technical problem is solved, the technical solution adopted in the present invention is as follows:
A kind of equipment for the conveying of above-mentioned interplane fuel oil, comprising:
One pipe and two connectors, the connector is connected by pipe, positioned at the both ends of pipe；It is described to connect first and quilt
The oil pumping valve connection of oil pumping aircraft, another connect with by the oiling valve of tanker aircraft.
Further, the connector is equipped with electrostatic line, and one end is connect with connector, and the other end is used for and work of pumping on aircraft
Door or the connection of oiling valve.Before the conveying of interplane fuel oil, electrostatic line is overlapped into connecing for aircraft connector and fuel delivery apparatus respectively
Head, for balancing and the electrostatic of aircraft connector.
Preferably, the connector is HJS-63A connector.
The invention has the following advantages:
(1) method of interplane fuel oil conveying of the present invention can put back into qualified airborne Fuel Remained, mention
The utilization rate of high aircraft fuel oil substantially reduces the operation cost of aircraft；
(2) the fuel oil conveying of two interplanes may be implemented in the method for the present invention, and make to be pumped aircraft oil extraction and by tanker aircraft
It refuels while carrying out, for aircraft maintenance enterprise, it is not necessary to carry out oil extraction using proprietary aviation fuel vehicle and fuel feeding works, can reduce simultaneously
Two aircrafts stop field time because of what oil extraction and fuel feeding worked, reduce aircraft maintenance cost.
Detailed description of the invention
The following further describes the present invention in detail with reference to the accompanying drawings and specific embodiments:
Fig. 1 is the schematic diagram of interplane fuel oil delivery method of the present invention；
Fig. 2 is the structural schematic diagram of interplane fuel delivery apparatus of the present invention；
Appended drawing reference in figure: 1- fuel feed pipe；2- connector；3- is by oil pumping aircraft；4- is by tanker aircraft；The conveying of 5- fuel oil
Equipment；6- Fuel Bleed Valve；7- oiling valve；8- intersects supply valve.
Specific embodiment
Fuel delivery apparatus 5 for the conveying of interplane fuel oil as shown in the figure, including fuel oil petroleum pipeline 1 and two connectors
2 compositions, connector 2 are set to 1 both ends of fuel oil petroleum pipeline, and a connector 2 is another for connecting with by the oil pumping valve of oil pumping aircraft
A connector 2 is connect with by the oiling valve of tanker aircraft, and connector 2 is HJS-63A connector, and each connector 2 is additionally provided with electrostatic line (figure
In do not show), one end is connect with connector 2, and the other end is used to connect with pump on aircraft valve or oiling valve.In interplane
Before fuel oil conveying, aircraft is pumped valve or oiling valve by electrostatic line, the overlapping splice with fuel delivery apparatus is used for
The electrostatic of balance and aircraft connector.
A kind of method of A320 type interplane fuel oil conveying comprising following steps:
(1) it is detected with Aviation Fuel microbial contamination detection device HY-LITE2017 by the fuel oil microorganism of oil pumping aircraft
The class of pollution, fuel oil microbial contamination grade are divided into slight pollution, general pollution and serious pollution, are by microbial contamination grade
Slight fuel oil carries out the conveying of interplane fuel oil.
Aviation Fuel microbial contamination detection principle be by be quantitatively evaluated sample in ATP (adenosine triphosphate) content,
To assess the pollution level of microorganism.Quantitative reading of the ATP in instrument shows as RLU value.Fuel oil microbial contamination grade root
It is evaluated according to " the fuel tanker microbial contamination guidelines " of International Air Transport Association (IATA): 1, slight pollution: small
Sample is risen in 1000RLU/；2, general pollution: 1000-5000RLU/ rises sample；3, serious pollution: greater than 5000RLU/ rises sample
Product.
(2) by 3 fuel oil microbial contamination of oil pumping aircraft it is up to standard after, the volume ratio of 1:4 is pressed with distilled water and isopropanol
The connector 2 of the detergent clean fuel oil conveying equipment 5 mixed will after the connector 2 of fuel delivery apparatus 5 is completely dried
One connector 2 of fuel delivery apparatus 5 is connect with by the Fuel Bleed Valve 6 of oil pumping aircraft 3, another connector 2 with by tanker aircraft 4
Oiling valve 7 be attached, while the electrostatic line on each connector 2 being connect with corresponding aircraft valve, it is ensured that fuel oil is defeated
Pipe 1 is sent not tense, pipeline is freely suspended on fuelling coupling, can prevent the tension of pipeline from fuel joint being caused to damage in this way
Bad and pipeline disengages, and causes injury to personnel or equipment damage.Record is started to carry out by after the initial Fuel On Board amount of oil pumping aircraft 3
The fuel oil of interplane conveys.
Pressure filling is carried out to by the progress pressure oil pumping of oil pumping aircraft 3 and to by tanker aircraft 4, detailed process is as follows: closing
It closes by all fuel pump of fuel tank of tanker aircraft 4, oiling mode is selected on aircraft refuelling-oil extraction panel, open target and refuel
The fuel oil threshold switch of fuel tank closes the fuel oil threshold switch of other non-refuelling fuel tanks；By 3 oiling of oil pumping aircraft-oil extraction face
Oil extraction mode is selected on plate, opens and intersects 8 valve of supply valve, is opened by the centre tank the automatic control of pump system of oil pumping aircraft 3,
The fuel pump of target oil extraction fuel tank is opened, the control of fuel pump outlet pressure is no more than 30PSI, while carrying out by oil pumping aircraft pressure
Power pumps and by tanker aircraft pressure filling；In interplane fuel oil transmission process, to by the practical oil drain quantity of oil pumping aircraft 3 and aobvious
Show that oil drain quantity carries out difference inspection, while carrying out difference inspection to by the practical volume read-out of tanker aircraft 4 and display volume read-out, so as to
The conveying of interplane fuel oil is normally carried out；After reaching Targeted fuel capacity by 4 target oiling fuel tank of tanker aircraft, closing is pumped
The fuel pump of 3 target oil extraction fuel tank of aircraft is closed by the centre tank the automatic control of pump system of oil pumping aircraft 3；It is being refueled
Close pattern is selected on 3 oilings of aircraft-oil extraction panel, open mode protective device is closed target oiling fuel oil in fuel tank valve and opened
It closes, opens fuel valve protective device, record fuel oil conveying capacity, is i.e. the conveying of completion interplane fuel oil.
Claims (10)
1. a kind of interplane fuel oil delivery method, which comprises the following steps:
(1) detection by the fuel qualities of oil pumping aircraft is confirmed whether that interplane fuel oil conveying can be carried out；
(2) by oil pumping aircraft fuel oil quality it is up to standard after, will by the Fuel Bleed Valve of oil pumping aircraft with by the oiling valve of tanker aircraft
It is attached, is pumped to by oil pumping aircraft using pressure oil pumping mode, while using pressure filling side to by tanker aircraft
Formula is refueled, and realizes the conveying of interplane fuel oil.
2. interplane fuel oil delivery method according to claim 1, which is characterized in that step (1) the intermediate fuel oil quality
Refer to fuel oil microbial contamination grade.
3. interplane fuel oil delivery method according to claim 2, which is characterized in that the fuel oil microbial contamination grade
It is divided into slight pollution, general pollution and serious pollution, the fuel qualities that can carry out interplane fuel oil conveying are that microorganism is slight
Pollution.
4. interplane fuel oil delivery method according to claim 1, which is characterized in that flown in the step (2) by oil pumping
The Fuel Bleed Valve of machine is connect with by the oiling valve of tanker aircraft by fuel delivery apparatus.
5. interplane fuel oil delivery method according to claim 4, which is characterized in that carry out aircraft in the step (2)
Between fuel oil conveying before, cleaned with connector of the detergent to fuel delivery apparatus, the detergent is by distilled water and isopropanol
It is mixed by the volume ratio of 1:3~4.
6. interplane fuel oil delivery method according to claim 1, which is characterized in that flown in the step (2) by oil pumping
Machine is pumped using pressure and using pressure filling, detailed process is as follows by tanker aircraft: being closed and is fired by all fuel tanks of tanker aircraft
Oil pump selects oiling mode on aircraft refuelling-oil extraction panel, opens the fuel oil threshold switch of target oiling fuel tank, closes it
The fuel oil threshold switch of his non-refuelling fuel tank；Oil extraction mode is selected on by oil pumping aircraft refuelling-oil extraction panel, is opened and is intersected confession
Valve valve is given, opens by the centre tank the automatic control of pump system of oil pumping aircraft, opens the fuel pump of target oil extraction fuel tank, together
Shi Jinhang is pumped by oil pumping aircraft pressure and by tanker aircraft pressure filling, until being reached by tanker aircraft target oiling fuel tank
Targeted fuel capacity；It closes by the fuel pump of oil pumping Aircraft Targets oil extraction fuel tank, closes and pumped by the centre tank of oil pumping aircraft
Automatic control system；Refueled by tanker aircraft-oil extraction panel on select close pattern, open mode protective device closes mesh
Oiling fuel oil in fuel tank threshold switch is marked, fuel valve protective device is opened.
7. interplane fuel oil delivery method according to claim 6, which is characterized in that in interplane fuel oil transmission process,
30PSI is no more than by the fuel pump outlet pressure control of oil pumping Aircraft Targets oil extraction fuel tank.
8. a kind of equipment for the described in any item interplane fuel oil conveyings of claim 1-7 characterized by comprising one
Pipe and two connectors, the connector is connected by pipe, positioned at the both ends of pipe；It is described connect first with by oil pumping aircraft
Valve of pumping connects, another connect with by the oiling valve of tanker aircraft.
9. the equipment of interplane fuel oil conveying according to claim 8, which is characterized in that the connector is equipped with electrostatic line,
One end is connect with connector, and the other end is used to connect with oil pumping valve or oiling valve on aircraft.
10. the equipment of interplane fuel oil conveying according to claim 9, which is characterized in that the connector connects for HJS-63A
Head.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810935736.6A CN109367809A (en) | 2018-08-16 | 2018-08-16 | Interplane fuel oil delivery method and its equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810935736.6A CN109367809A (en) | 2018-08-16 | 2018-08-16 | Interplane fuel oil delivery method and its equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109367809A true CN109367809A (en) | 2019-02-22 |
Family
ID=65403963
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810935736.6A Pending CN109367809A (en) | 2018-08-16 | 2018-08-16 | Interplane fuel oil delivery method and its equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109367809A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112455703A (en) * | 2021-01-06 | 2021-03-09 | 山东航空股份有限公司 | Device and method for mixing oil between airplanes |
| US20220324583A1 (en) * | 2021-03-31 | 2022-10-13 | ZeroAvia, Inc. | Managing hydrogen fuel in hydrogen fuel cell-powered aircraft |
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| CN2383761Y (en) * | 1999-07-09 | 2000-06-21 | 武进市腾飞航空油料设备配件厂 | Aeronautic pressure oiling joint |
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| CN101643769A (en) * | 2009-08-24 | 2010-02-10 | 成都飞机工业（集团）有限责任公司 | Test method of microorganism of aircraft fuel oil |
| CN202926581U (en) * | 2012-11-19 | 2013-05-08 | 武汉航达航空科技发展有限公司 | Test system for main fuel pump of airplane |
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| CN105083586A (en) * | 2015-08-12 | 2015-11-25 | 中国航空工业集团公司西安飞机设计研究所 | Device for testing aerial refueling adapter equipment |
-
2018
- 2018-08-16 CN CN201810935736.6A patent/CN109367809A/en active Pending
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|---|---|---|---|---|
| CN2383761Y (en) * | 1999-07-09 | 2000-06-21 | 武进市腾飞航空油料设备配件厂 | Aeronautic pressure oiling joint |
| US20030136874A1 (en) * | 2001-12-10 | 2003-07-24 | Gjerdrum David Michael | Method for safer mid-air refueling |
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| US20130119202A1 (en) * | 2010-07-29 | 2013-05-16 | Airbus Operations Limited | Refuel control system and method of refuelling |
| CN202926581U (en) * | 2012-11-19 | 2013-05-08 | 武汉航达航空科技发展有限公司 | Test system for main fuel pump of airplane |
| CN105083586A (en) * | 2015-08-12 | 2015-11-25 | 中国航空工业集团公司西安飞机设计研究所 | Device for testing aerial refueling adapter equipment |
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| Title |
|---|
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112455703A (en) * | 2021-01-06 | 2021-03-09 | 山东航空股份有限公司 | Device and method for mixing oil between airplanes |
| US20220324583A1 (en) * | 2021-03-31 | 2022-10-13 | ZeroAvia, Inc. | Managing hydrogen fuel in hydrogen fuel cell-powered aircraft |
| WO2022216474A1 (en) * | 2021-03-31 | 2022-10-13 | ZeroAvia, Inc. | Managing hydrogen fuel in hydrogen fuel cell-powered aircraft |
| US11858647B2 (en) * | 2021-03-31 | 2024-01-02 | ZeroAvia, Inc. | Managing hydrogen fuel in hydrogen fuel cell-powered aircraft |
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|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| CB03 | Change of inventor or designer information | ||
| CB03 | Change of inventor or designer information |
Inventor after: Wu Weizhi Inventor after: Fan Xiaobin Inventor after: Gao Du Inventor after: Li Fengxi Inventor after: Wang Boxin Inventor after: Ye Qingchao Inventor after: Shen Ce Inventor before: Wu Weizhi Inventor before: Fan Xiaobin Inventor before: Li Fengxi Inventor before: Wang Boxin Inventor before: Ye Qingchao Inventor before: Shen Ce |
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| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190222 |