CN214930726U - Automatic measurement aircraft tank service truck - Google Patents
Automatic measurement aircraft tank service truck Download PDFInfo
- Publication number
- CN214930726U CN214930726U CN202121477906.4U CN202121477906U CN214930726U CN 214930726 U CN214930726 U CN 214930726U CN 202121477906 U CN202121477906 U CN 202121477906U CN 214930726 U CN214930726 U CN 214930726U
- Authority
- CN
- China
- Prior art keywords
- oil
- aircraft
- controller
- gun
- control valve
- 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.)
- Active
Links
Images
Landscapes
- Loading And Unloading Of Fuel Tanks Or Ships (AREA)
Abstract
The application provides an automatic measurement aircraft tank service truck relates to aviation fuel feeding technical field, and wherein, this automatic measurement aircraft tank service truck includes: the oil delivery system comprises a vehicle body, an oil delivery pipe, an oil filling gun, a control valve, an oil gauge, a controller and a display, wherein one end of the oil delivery pipe is connected to an oil inlet of the vehicle body, and the other end of the oil delivery pipe is used for being connected to a ground well; one end of the oil gun is connected with an oil outlet connected to the vehicle body, and the other end of the oil gun is used for being connected to a preset oil filling interface of the airplane; the oil inlet of the vehicle body is communicated with the oil outlet of the vehicle body through an oil conveying passage formed in the vehicle body; the control valve is arranged at the other end of the oil gun, and the oil meter is arranged at the other end of the oil gun; the controller is connected to the control valve, and the controller sends a valve opening control signal to the control valve to control the control valve to open to deliver oil to the aircraft through the predetermined fueling interface. Through adopting above-mentioned automatic measurement aircraft tank service truck, make things convenient for the filler to refuel the aircraft, effectively improved filler's work efficiency.
Description
Technical Field
The application relates to the technical field of aviation fuel feeding, in particular to an automatic metering aircraft refueling truck.
Background
The refueling amount required by takeoff needs to be checked with crew members during refueling, the refueling amount is calculated after the refueling amount required by takeoff is confirmed, the 737-plus 800 series is divided into a left oil tank, a right oil tank, a middle oil tank, a left oil tank, a middle oil tank, a right oil tank, wheel gear residual oil amounts are manually checked by the refueling personnel and are respectively recorded, the maximum capacity of each oil tank is combined after recording (the aircraft oil tank with long years cannot be added to the maximum capacity upper limit, otherwise, oil can be spilled out during flight), and the refueling amount required by each tank is manually calculated according to the refueling amount required by takeoff. In the refueling process, a refueling operator is required to manually check the measured value of the fuel gauge and manually control the starting and ending of the refueling process, so that the working efficiency of the refueling operator is low.
SUMMERY OF THE UTILITY MODEL
In view of the above, embodiments of the present application provide an automatic metering aircraft refueling truck to overcome at least one of the above-mentioned disadvantages.
The application mainly comprises the following aspects:
in a first aspect, an embodiment of the present application provides an automatic metering aircraft refueling truck, including: the device comprises a vehicle body, an oil delivery pipe, an oil filling gun, a control valve, an oil gauge, a controller and a display. One end of the oil pipeline is connected to an oil inlet of the vehicle body, and the other end of the oil pipeline is used for being connected to a ground well; one end of the oil gun is connected with an oil outlet connected to the vehicle body, and the other end of the oil gun is used for being connected to a preset oil filling interface of the airplane; the oil inlet of the vehicle body is communicated with the oil outlet of the vehicle body through an oil conveying passage formed in the vehicle body; the control valve is arranged at the other end of the oil gun, and the oil meter is arranged at the other end of the oil gun; the controller is connected to the control valve, and sends a valve opening control signal to the control valve so as to control the control valve to be opened to convey oil liquid to the airplane through a preset oiling interface; the oil gauge is connected to the controller, and the oil gauge sends the detected oil quantity value of the oil delivered to the airplane to the controller; the controller sends a valve closing control signal which is generated by comparing the oil quantity value with the total oil filling amount and indicates that the oil quantity value reaches the total oil filling amount to the control valve so as to control the control valve to be closed; the controller is connected to the display and sends the total fuel load and fuel load values to the display for display.
In one possible embodiment, the controller of the automated metered aircraft fuelling vehicle is an onboard controller of the automated metered aircraft fuelling vehicle.
In one possible embodiment, the controller of the automatic metering aircraft fuelling vehicle is a portable terminal, the automatic metering aircraft fuelling vehicle further comprising an onboard controller;
the portable terminal is connected to the control valve, the fuel gauge and the display via the vehicle-mounted controller.
In one possible embodiment, the fuel gauge of the automated metering aircraft fuelling vehicle is disposed between the control valve and the other end of the fuelling gun.
In one possible embodiment, the automated metered aircraft refueller further comprises a communication module. The communication module is connected with the airplane information platform and sends the flight information of the airplane acquired from the airplane information platform to the controller, wherein the flight information comprises the predicted flight mileage of the airplane and the residual oil amount of the airplane; and the controller determines the difference between the estimated oil quantity and the residual oil quantity calculated according to the flight mileage as the total fuel filling quantity.
In one possible embodiment, the automated metered aircraft refueller further comprises at least one physical key, the at least one physical key disposed on an outer surface of the portable terminal, the at least one physical key coupled to the portable terminal, the at least one physical key comprising at least one of: number key, confirm key, delete key.
In one possible embodiment, the display of the automatic metering aircraft fuelling vehicle is a touch screen, the display being provided separately or the display being integrated with the controller.
In one possible embodiment, the automatic metering aircraft fuelling vehicle is adapted for an aircraft comprising a left fuel tank, an intermediate fuel tank and a right fuel tank, and the predetermined fuelling interface is one of a left fuelling interface to the left fuel tank, an intermediate fuelling interface to the intermediate fuel tank, and a right fuelling interface to the right fuel tank.
In one possible embodiment, the other end of the fuel nozzle of the automated metering aircraft fuelling vehicle is provided with a protective cover to cover the fuel outlet of the fuel nozzle.
In one possible embodiment, the fueling guns of the autometering aircraft fueling vehicle are single barrel fueling guns.
The utility model provides an automatic measurement aircraft tank service truck acquires fluid to the automobile body in from the ground well through defeated oil pipe in, the rethread nozzle inputs fluid to the aircraft, the one end of nozzle is provided with control valve and fuel gauge, when the controller received valve opening control signal, the control valve is opened, refuel to the aircraft, the fuel gauge statistics output's oil mass value simultaneously, when the required oil mass of next flight is satisfied to the oil mass in the aircraft, then the control valve is closed, stop refueling. By the aid of the mode, automatic control of the fuel quantity of the aircraft refueling truck for refueling the aircraft is achieved, and working efficiency of a refueling worker is improved.
In order to make the aforementioned objects, features and advantages of the present application more comprehensible, preferred embodiments accompanied with figures are described in detail below.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings that are required to be used in the embodiments will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present application and therefore should not be considered as limiting the scope, and for those skilled in the art, other related drawings can be obtained from the drawings without inventive effort.
FIG. 1 is a schematic structural diagram illustrating an automatic metering aircraft fuelling vehicle according to an embodiment of the present application;
fig. 2 shows a schematic structural diagram of an intelligent aviation fuel system according to an embodiment of the present application.
Description of the main element symbols:
in the figure:
101-a ground well; 102-an oil conveying pipe; 103-a vehicle body; 104-a fuel nozzle; 105-a controller; 106-a control valve; 107-a display; 108-oil gauge; 109-aircraft reservation fueling interface.
Detailed Description
To make the purpose, technical solutions and advantages of the embodiments of the present application clearer, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it should be understood that the drawings in the present application are for illustrative and descriptive purposes only and are not used to limit the scope of protection of the present application. Additionally, it should be understood that the schematic drawings are not necessarily drawn to scale. The flowcharts used in this application illustrate operations implemented according to some embodiments of the present application. It should be understood that the operations of the flow diagrams may be performed out of order, and that steps without logical context may be performed in reverse order or concurrently. One skilled in the art, under the guidance of this application, may add one or more other operations to, or remove one or more operations from, the flowchart.
In addition, the described embodiments are only a part of the embodiments of the present application, and not all of the embodiments. The components of the embodiments of the present application, generally described and illustrated in the figures herein, can be arranged and designed in a wide variety of different configurations. Thus, the following detailed description of the embodiments of the present application, presented in the accompanying drawings, is not intended to limit the scope of the claimed application, but is merely representative of selected embodiments of the application. All other embodiments, which can be derived by a person skilled in the art from the embodiments of the present application without making any creative effort, shall fall within the protection scope of the present application.
To enable those skilled in the art to utilize the present disclosure, the following embodiments are presented in conjunction with a specific application scenario "737-.
Before the present application is provided, in the existing scheme, an oil filler needs to check the oil filling amount required for takeoff with a crew member during the oil filling process, the oil filling amount is calculated after the oil filling amount required for takeoff is confirmed, because 737-plus-800 series are divided into left, right, middle and middle oil tanks, the oil filler needs to manually check the residual oil amount of wheel gears of the left, middle and right oil tanks, record the residual oil amount respectively, combine the maximum capacity of each oil tank after recording (the aircraft oil tank which is long in years cannot be increased to the maximum capacity upper limit, otherwise, oil can be spilled out during the flight), and manually calculate the oil filling amount of each oil tank according to the oil filling amount required for takeoff. In the refueling process, a refueling operator is required to manually check the measured value of the fuel gauge and manually control the starting and the ending of the refueling process, so that the operation of the refueling operator is complicated, and the working efficiency is low.
In view of the above problems, embodiments of the present application provide an automatic metering aircraft fuelling vehicle, which is described below by way of example.
For the convenience of understanding of the present application, the technical solutions provided in the present application will be described in detail below with reference to specific embodiments.
Example one
Fig. 1 provides a schematic diagram of an automatic metering aircraft fuelling vehicle. As shown in fig. 1, the automatic metering aircraft fuelling vehicle provided by the embodiment of the present application comprises an oil delivery pipe 102, a vehicle body 103, a fuelling gun 104, a controller 105, a control valve 106, a display 107 and a fuel gauge 108.
Wherein, one end of the oil pipeline 102 is connected to an oil inlet of the vehicle body 103, the other end of the oil pipeline 102 is used for being connected to the ground well 101, one end of the oil gun 104 is connected to an oil outlet of the vehicle body 103, the other end of the oil gun 104 is used for being connected to a preset oil filling interface of the airplane, and the oil inlet of the vehicle body 103 is communicated with the oil outlet of the vehicle body 103 through an oil transportation channel formed inside the vehicle body 103. For example, the automatic metering aircraft fuelling vehicle may further comprise an oil pump (not shown) disposed on the oil delivery pipe 102, wherein oil in the ground well 101 is pumped by the oil pump through the oil delivery pipe 102, is delivered from an oil inlet to the vehicle body 103, is communicated to an oil outlet through an oil delivery passage inside the vehicle body 103, and is finally delivered through the fuelling gun 104. The other end of the fuel gun 104 is connected to a predetermined fueling interface of the aircraft (i.e., an aircraft predetermined fueling interface 109), which is typically provided on the right wing of the aircraft, for fueling the fuel tanks within the aircraft.
The control valve 106 is arranged at the other end of the fuel nozzle 104, and the control valve 106 realizes the on-off of the oil path through the control of a control signal. The fuel gauge 108 is disposed at the other end of the fuel gun 104, and the fuel gauge 108 is used for counting the fuel amount of the oil input into the aircraft by the fuel gun 104.
The controller 105 may be connected to the oil pump to control the start and stop of the oil pump, the controller 105 is further connected to the control valve 106, and the controller 105 sends a valve opening control signal to the control valve 106 to control the control valve 106 to open to deliver oil to the aircraft through a predetermined fueling interface. The fuel gauge 108 is connected to the controller 105, and the fuel gauge 108 sends the detected amount of fuel for the aircraft to the controller 105. The controller 105 sends a valve-closing control signal indicating that the oil amount value reaches the total fuel amount, generated by comparing the oil amount value with the total fuel amount, to the control valve 106 to control the control valve 106 to close.
Specifically, in the complete refueling process, after the refueling gun 104 and the airplane preset refueling interface are connected, a refueling command can be sent to the controller 105 by operating a physical key or a virtual key displayed on a display, the controller 105 generates a valve opening control signal to control the opening of the control valve 106, oil is delivered into the airplane through the refueling gun 104, meanwhile, the oil gauge 108 on the refueling gun 104 counts the oil mass value of the oil delivered by the airplane, and when the oil mass value is equal to the total refueling volume of the current refueling, the controller 105 generates a valve closing control signal to stop refueling the airplane.
The controller 105 is connected to a display 107, and the controller 105 sends the total fuel amount and the fuel amount value to the display 107 to be displayed. The display 107 displays the total fuel required by the aircraft, which may be the total fuel to be added calculated from the difference between the total fuel required for the current flight of the aircraft and the remaining fuel in the aircraft tanks, or the fuel required for the fuel tanks allocated to the respective fuel tanks, and the fuel quantity value already delivered to the aircraft. Correspondingly, the fuel quantity value can be a total fuel quantity value in a one-time refueling project, or a fuel tank transported fuel quantity value of a corresponding fuel tank is input, and the total fuel quantity value and the transported fuel quantity values of the fuel tanks can be displayed simultaneously, so that refueling workers can conveniently refuel the airplane, and the working efficiency of the refueling workers is improved.
Here, for the 737-800 series aircraft including the left and right middle three fuel tanks, after the total fuel charge for the current flight of the aircraft is determined, the fuel charges for the three fuel tanks may be determined based on the total fuel charge. The specific oil quantity distribution principle is as follows: the method comprises the steps of obtaining maximum capacity values of left and right fuel tanks of the airplane, wherein the maximum capacity values of the left and right fuel tanks of the airplane are normally set as default capacity values (namely, the capacity values of the fuel tanks when the airplane leaves a factory), and for airplanes which run for a long time, an oiler can manually input actual capacity values of the left and right fuel tanks, and the input actual capacity values are determined as the maximum capacity values. The maximum capacity values of the left and right fuel tanks are compared, the smaller one is selected as the maximum capacity value common to the left and right fuel tanks, that is, the maximum capacity values of the two fuel tanks are the same, and the predetermined input fuel quantity of the middle fuel tank is calculated from the difference between the total fuel supply quantity and the predetermined input fuel quantity of the left and right fuel quantities. Wherein the preset input oil quantity of the left oil quantity and the right oil quantity is the sum of the maximum capacity value of the left oil tank and the maximum capacity value of the right oil tank. In other words, in the fuel distribution process, the fuel quantity values of the left and right fuel tanks after refueling are equal, so as to ensure the balance of the airplane during the flight.
In the embodiment, oil is obtained from a ground well 101 through an oil delivery pipe 102 and is delivered into a vehicle body 103, then the oil is delivered into an aircraft through a fuel nozzle 104, one end of the fuel nozzle 104 is provided with a control valve 106 and an oil meter 108, when a controller 105 receives a valve opening control signal, the control valve 106 is controlled to be opened, the aircraft is refueled, meanwhile, the oil meter 108 counts the output oil quantity value, and when the oil quantity in the aircraft meets the oil quantity required by the next flight, the control valve 106 is controlled to be closed, and the refueling is stopped. By adopting the mode, the oiling amount of each oil tank is automatically distributed when the airplane is oiled, the condition that the needed oiling amount of the airplane is calculated by manpower to cause errors is avoided, and the working efficiency of an oiler is improved.
In one case, the controller 105 is an onboard controller that automatically meters an aircraft refueling truck. The controller 105 is integrated with an onboard controller of the body of the vehicle body 103, which controls the fuelling vehicle and at the same time measures and controls the fuelling.
In another case, the controller 105 is a portable terminal, and the automatic metering aircraft refueling truck further comprises an onboard controller, and the portable terminal is respectively connected to the control valve 106, the fuel gauge 108 and the display 107 via the onboard controller. The portable terminal is provided separately and can communicate with an onboard controller of a refueling truck, which is connected to the control valve 106, the fuel gauge 108, and the display 107, respectively.
Specifically, the portable terminal can be carried by a refueling person and can also be fixed on an airplane refueling truck through a fixing frame to facilitate operation.
Further, an oil gauge 108 is provided between the control valve 106 and the other end of the fuel gun 104. The other end of the fuel nozzle 104 is used to connect with a predetermined fueling interface of the aircraft, and the fuel gauge 108 is disposed therebetween, so as to accurately gauge the total amount of oil delivered by the fuel nozzle 104 into the aircraft.
Further, the automatic metering aircraft fuelling vehicle further comprises a communication module, the communication module is connected with the aircraft information platform and sends the flight information of the aircraft acquired from the aircraft information platform to the controller 105, wherein the flight information comprises the predicted flight mileage of the aircraft and the residual oil quantity of the aircraft, and the controller 105 determines the difference between the predicted oil quantity and the residual oil quantity calculated according to the flight mileage as the total fuelling quantity.
Specifically, the automatic metering aircraft refueling truck comprises a communication module, and the communication module can be connected with an aircraft information platform to acquire flight information of an aircraft and send the flight information to the controller 105. The flight information comprises the predicted flight mileage of the aircraft and the remaining oil amount of the aircraft, the predicted flight mileage of the aircraft is the next flight mileage to be taken by the aircraft, and the total oil amount (i.e. the predicted oil amount) required by the predicted flight mileage of the aircraft can be converted and calculated through the predicted flight mileage of the aircraft. The remaining oil quantity of the aircraft is the oil quantity remaining in the oil quantity after the last flight of the aircraft is finished, wherein the remaining oil quantity can be the oil quantity in each oil tank or the sum of the remaining oil quantities in all the oil tanks. The total fuel filling amount required to be conveyed to the airplane in the present refueling can be obtained by estimating the difference between the fuel amount and the residual fuel amount.
Further, the automatic metering aircraft refueling truck further comprises at least one physical key, the at least one physical key is disposed on an outer surface of the portable terminal, the at least one physical key is connected to the portable terminal, and the at least one physical key comprises at least one of the following items: number key, confirm key, delete key.
Specifically, the automatic metering aircraft refueling truck is provided with at least one physical key, the at least one physical key can be arranged on the outer surface of the portable terminal, the at least one physical key is connected with the portable terminal, and the portable terminal receives a signal of the physical key and sends the signal to the controller 105. The at least one physical key includes at least one of a number key, a confirmation key, and a delete key, and the fueling worker can modify the total fueling amount displayed on the display 107 of the portable terminal by the physical key.
Further, the display 107 is a touch screen, the display 107 is provided separately, or the display 107 is integrated with the controller 105.
Specifically, the display 107 of the automatic metering aircraft refueling truck can be integrated with the controller 105, can be independently arranged, can be placed on the vehicle body 103, and can be conveniently observed when a refueling worker refuels, the refueling worker can observe the oil quantity of the currently added aircraft in real time, so that the inaccurate oil quantity addition of the aircraft is avoided, and accidents are prevented.
Furthermore, the airplane comprises a left oil tank, a middle oil tank and a right oil tank, and the preset oiling interface is one of a left oiling interface communicated with the left oil tank, a middle oiling interface communicated with the middle oil tank and a right oiling interface communicated with the right oil tank.
Specifically, the automatic measurement aircraft refuelling truck that this embodiment provided is applicable to 737 and give other good luck 800 civil aviation transportation and uses the aircraft, and the aircraft includes left oil mass, middle oil tank and right oil tank, sets up three interface and corresponds three oil tank respectively, and left refuels interface and left oil tank intercommunication, middle refuels interface and middle oil tank intercommunication, and right refuels interface and right oil tank intercommunication.
Further, the other end of the fuel gun 104 is provided with a protective cover to cover the fuel outlet of the fuel gun 104.
Specifically, the other end of the fueling gun 104 is provided with a protective cover, and when fueling is not performed, the protective cover is installed at the other end of the fueling gun 104 to cover the fuel outlet of the fueling gun 104, protect the fueling gun 104, and prevent dust from entering into contaminated oil, thereby affecting the flight of the aircraft.
Further, the fuel nozzle 104 is a single tube fuel nozzle 104.
Example two
Fig. 2 is a schematic structural diagram of an intelligent aviation fuel system. As shown in fig. 2, an embodiment of the present application further provides an intelligent aviation fuel system, which includes: dispatch order terminal, connect order terminal and automatic measurement aircraft tank service truck.
The dispatcher sends the refueling work order through the order sending terminal, the order sending terminal calculates the total input oil quantity and the corresponding refueling amount of each oil tank according to the acquired flight information, the maximum capacity values of the three oil tanks in the left, middle and right and the respective residual oil quantity value of the oil tank in the left, middle and right of the airplane, a task order is generated, and the order sending terminal sends the task order to the order receiving terminal held by the designated refueling operator. Illustratively, the fueling worksheet may include mission information (e.g., at least one of an aircraft model of the aircraft to be fueled, a fuel tank model, a default maximum capacity of the fuel tank, a fueling time, a fueling location, a mission sheet number), flight information (e.g., a predicted flight mileage of the aircraft and a remaining fuel capacity of the aircraft), and fueling vehicle information (e.g., a parking location or a license plate number of the fueling vehicle).
The refueling operator receives the task list through the order receiving terminal, can inquire the corresponding task list number on the display 107 of the automatic metering aircraft refueling truck, the controller 105 of the automatic metering aircraft refueling truck obtains the task information corresponding to the task list number, the respective corresponding refueling amount and total input oil amount of the left, middle and right three oil tanks are analyzed, and the corresponding refueling amount and the total input oil amount are used as comparison objects with the oil amount value to control the on-off of the control valve 106, so that the precise control of the aircraft refueling amount is realized.
Exemplary types of aircraft fuel gauges include pound and kilogram gauges. The order dispatching terminal can be converted based on the types of different aircraft fuel gauges, and calculation errors caused by non-uniform calculation units are avoided.
The above description is only for the specific embodiments of the present application, but the scope of the present application is not limited thereto, and any person skilled in the art can easily conceive of the changes or substitutions within the technical scope of the present application, and shall be covered by the scope of the present application. Therefore, the protection scope of the present application shall be subject to the protection scope of the claims.
Claims (10)
1. An automatic metering aircraft refueling truck is characterized by comprising a truck body, an oil delivery pipe, a refueling gun, a control valve, an oil meter, a controller and a display;
one end of the oil pipeline is connected to an oil inlet of the vehicle body, and the other end of the oil pipeline is used for being connected to a ground well;
one end of the oil gun is connected to an oil outlet of the vehicle body, and the other end of the oil gun is used for being connected to a preset oiling interface of the airplane;
the oil inlet of the vehicle body is communicated with the oil outlet of the vehicle body through an oil conveying passage formed in the vehicle body;
the control valve is arranged at the other end of the oil gun, and the oil meter is arranged at the other end of the oil gun;
the controller is connected to the control valve, and the controller sends a valve opening control signal to the control valve to control the control valve to open so as to deliver oil to the aircraft through the predetermined fueling interface of the aircraft;
the oil gauge is connected to the controller, and the oil gauge sends the detected oil quantity value for conveying oil to the aircraft to the controller;
the controller sends a valve closing control signal which is generated by comparing the oil quantity value with the total oil filling amount and indicates that the oil quantity value reaches the total oil filling amount to the control valve so as to control the control valve to close;
the controller is connected to the display, and the controller sends the total fueling amount and the fuel amount value to the display for display.
2. The automated metered aircraft refuelling vehicle of claim 1, wherein the controller is an onboard controller of the automated metered aircraft refuelling vehicle.
3. The automated metered aircraft refuelling vehicle of claim 1, wherein the controller is a portable terminal, the automated metered aircraft refuelling vehicle further comprising an onboard controller;
the portable terminal is connected to the control valve, the fuel gauge, and the display via the onboard controller, respectively.
4. An autometering aircraft fuelling vehicle according to claim 1, wherein the fuel gauge is disposed between the control valve and the other end of the fuelling gun.
5. The automated metered aircraft refuelling vehicle of claim 1, further comprising a communication module;
the communication module is connected with an airplane information platform and sends the flight information of the airplane acquired from the airplane information platform to the controller, wherein the flight information comprises the predicted flight mileage of the airplane and the residual oil amount of the airplane;
and the controller determines the difference between the estimated oil quantity obtained by calculating according to the flight mileage and the residual oil quantity as the total oil filling quantity.
6. The automated metered aircraft refuelling vehicle of claim 3, further comprising:
at least one physical key disposed on an outer surface of the portable terminal, the at least one physical key being connected to the portable terminal, the at least one physical key including at least one of: number key, confirm key, delete key.
7. The automated metered aircraft fuelling vehicle of claim 1, wherein the display is a touch screen, the display being provided separately or integrated with the controller.
8. The automated metered aircraft refuelling vehicle of claim 1, wherein the aircraft includes a left fuel tank, an intermediate fuel tank, and a right fuel tank, and the predetermined refuelling interface of the aircraft is one of a left refuelling interface communicated to the left fuel tank, an intermediate refuelling interface communicated to the intermediate fuel tank, and a right refuelling interface communicated to the right fuel tank.
9. An automatic metering aircraft fuelling vehicle according to claim 1 wherein the other end of the fuelling gun is provided with a protective cover to cover an oil outlet from the fuelling gun.
10. The automatic metering aircraft refuelling vehicle of claim 1, wherein the refuelling gun is a mono-tube refuelling gun.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121477906.4U CN214930726U (en) | 2021-06-30 | 2021-06-30 | Automatic measurement aircraft tank service truck |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121477906.4U CN214930726U (en) | 2021-06-30 | 2021-06-30 | Automatic measurement aircraft tank service truck |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214930726U true CN214930726U (en) | 2021-11-30 |
Family
ID=79075056
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121477906.4U Active CN214930726U (en) | 2021-06-30 | 2021-06-30 | Automatic measurement aircraft tank service truck |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214930726U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114818222A (en) * | 2022-05-23 | 2022-07-29 | 北京中航油工程建设有限公司 | Airport aircraft refueling ground well position design method |
| CN115953954A (en) * | 2023-03-15 | 2023-04-11 | 中国航空油料有限责任公司天府机场分公司 | Oil filling amount prompt system for oil pipeline vehicle |
| CN116187672A (en) * | 2022-12-27 | 2023-05-30 | 中国航空油料有限责任公司 | Method and device for generating oiling task |
-
2021
- 2021-06-30 CN CN202121477906.4U patent/CN214930726U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114818222A (en) * | 2022-05-23 | 2022-07-29 | 北京中航油工程建设有限公司 | Airport aircraft refueling ground well position design method |
| CN114818222B (en) * | 2022-05-23 | 2024-04-12 | 北京中航油工程建设有限公司 | Airport aircraft refueling well position design method |
| CN116187672A (en) * | 2022-12-27 | 2023-05-30 | 中国航空油料有限责任公司 | Method and device for generating oiling task |
| CN115953954A (en) * | 2023-03-15 | 2023-04-11 | 中国航空油料有限责任公司天府机场分公司 | Oil filling amount prompt system for oil pipeline vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN214930726U (en) | Automatic measurement aircraft tank service truck | |
| CN101346280B (en) | Aircraft auxiliary fuel tank system and method | |
| CN103038133B (en) | A refuel control system and method of refuelling | |
| CN102128667B (en) | Test device for oil volume calibration of large oil tank | |
| RU2327611C1 (en) | Fuel flow meter system with fuel temperature compensation | |
| RU2327614C1 (en) | Airborne aircraft fuel flow meter system with fuel dielectric permeability compensation | |
| WO2018028824A1 (en) | Method and device for detecting an amount of gas in a calibration-capable manner | |
| CA3052170C (en) | Mobile distribution station having onboard fluid storage tank | |
| CN214057913U (en) | Device for oil mixing between airplanes | |
| CA3051988C (en) | Mobile distribution station having auxiliary delivery system | |
| CN111377062A (en) | Integrated aviation oil supply equipment | |
| CN113232874B (en) | Automatic control device for aircraft pressure refueling | |
| CN211919027U (en) | Integrated aviation oil supply equipment | |
| CN108313293A (en) | A kind of unmanned plane and automobile | |
| CN201647987U (en) | Oil gun with flowmeter | |
| RU2327613C1 (en) | Airborne aircraft fuel flow meter system with fuel temperature and dielectric permeability compensation | |
| CN219046499U (en) | Aircraft refueling monitoring system | |
| RU101677U1 (en) | MOBILE FUEL FILLING ITEM | |
| US20180300971A1 (en) | Electronic aircraft data capture for refueling | |
| CN219807774U (en) | Fuel storage and transportation filling system | |
| CN214693302U (en) | Can realize measurement tank service truck pipe-line system who refuels | |
| RU2327610C1 (en) | Fuel flow meter system with temperature compensation of maneuverable aircraft | |
| CN220391524U (en) | Unmanned aerial vehicle ground pressure refueling system and unmanned aerial vehicle comprising same | |
| RU2317228C1 (en) | Maneuverable aircraft onboard fuel gaging and flow-metering system at fuel temperature and dielectric permeability compensation | |
| AU2016397049B2 (en) | Fuelling method |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |