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Control method of skid-mounted aviation oil refueling and storing device

A technology of a control method and a storage device, which is applied in the direction of a liquid delivery device, can solve problems such as inapplicability, and achieve the effects of improving practicability, strong mobility, and ensuring reliability

Active Publication Date: 2015-10-07
SICHUAN FEIDA SOURCE ENERGY EQUIP MFG CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0018] In order to solve the problem that the existing refueling methods are not suitable for general aviation airports and feeder airports, the present invention provides a control method for a skid-mounted aviation fuel refueling storage device, which integrates the functions of fuel storage and refueling, and reduces the construction cost of small and medium-sized airports. and maintenance costs

Method used

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  • Control method of skid-mounted aviation oil refueling and storing device
  • Control method of skid-mounted aviation oil refueling and storing device
  • Control method of skid-mounted aviation oil refueling and storing device

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0062] In this embodiment, pump 6 is used for oil collection: connecting joint 1 is connected to the oil outlet of the tanker (or oil depot), valves 2, 4, 5, 8, 37, 38 are opened, valves 42, 43, 44 are closed, valves 9, 10, 12, 15, 37, 36, and 77 are closed; the valve 37 and the solenoid valve 38 are connected to the oil tank 86, the valves 2, 4, and 5 are connected between the connection joint 1 and the pump 6, and the outlet of the pump 6 is connected to There is a valve 8, and a check valve 7 is installed between the valve 8 and the pump 6;

[0063] 1. When the filter separator 49 is used for oil collection: valves 18, 19, 52, 61 are closed, and valves 16, 17 are opened;

[0064] 1.1. Use flow meter 22 for measurement: valves 20, 24, and 26 are closed, and valves 21, 23 are opened;

[0065] 1.2. Use flow meter 25 for measurement: valves 20, 21, 23 are closed, and valves 26, 26 are opened.

[0066] 2. When the filter separator 57 is used for oil collection: valves 16, 17, ...

Embodiment 2

[0071] In this embodiment, the pump 13 is used for oil collection: the connecting joint 1 is connected to the oil outlet of the tanker (or oil depot), the valves 2, 4, 37, 38 are opened, the valves 42-44 are closed, and the valves 10, 11, 5, 8, 27, 36 closed;

[0072] 1. Use filter separator 49 to collect oil: valves 18, 19, 52, 61 are closed, and valves 16, 17 are opened;

[0073] 1.1. Use flow meter 22 for measurement: valves 20, 24, and 26 are closed, and valves 21, 23 are opened;

[0074] 1.2. Use flow meter 25 for measurement: valves 20, 21, 23 are closed, and valves 26, 26 are opened.

[0075] 2. Use filter separator 57 to collect oil: valves 16, 17, 60, 62, 63 are closed, valves 18, 19 are opened

[0076] 2.1. Use flow meter 22 for measurement: valves 20, 24, and 26 are closed, and valves 21, 23 are opened;

[0077] 2.2. Use the flow meter 25 for measurement: the valves 20, 21, and 23 are closed, and the valves 24, 26 are opened.

[0078] During the oil collection ...

Embodiment 3

[0081] When refueling, valves 41, 42 are opened, and valves 4, 43, 44, 20, 37, 77 are closed.

[0082] The present embodiment refuels the aircraft for gravity refueling, the gravity refueling joint 31 is connected to the aircraft fuel tank port for gravity refueling, the valve 27 is opened, and the valve 36 is closed;

[0083] 1. Pump 6 is used for refueling: valves 5 and 8 are opened, valve 9 is adjusted according to the flow rate, and valves 12, 15 and 11 are closed;

[0084] 1.1. Use filter separator 49 to refuel: valves 16 and 17 are opened, and valves 18, 19, 52 and 61 are closed;

[0085] 1.1.1. Measuring by flow meter 22: valves 21 and 23 are opened, valves 24 and 26 are closed;

[0086] 1.1.2. Measure with flowmeter 25: open valves 24 and 26, and close valves 21 and 23.

[0087] 1.2. Use filter separator 57 to refuel: valves 18 and 19 are opened, and valves 16, 17, 60, 62, and 63 are closed;

[0088] 1.2.1, use flowmeter 22 to measure: valves 21 and 23 are opened, v...

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Abstract

The invention belongs to the technical field of aircraft refueling, and discloses a control method of a skid-mounted aviation oil refueling and storing device. The control method solves the problem that a conventional refueling manner is not suitable for a general aviation airport and a general feeder airport. According to the control method disclosed by the invention, the skid-mounted aviation oil refueling and storing device comprises a skid-mounted base, wherein the skid-mounted base is provided with an oil tank, pumps, connecting connectors, filter separators, flowmeters, oil refueling rubber tubes and oil refueling connectors in a matching manner, and the oil refueling connectors are communicated with the oil refueling rubber tubes; a liquid level controller and electromagnetic valves are arranged in the oil tank, the electromagnetic valves are arranged between the flowmeters and the oil refueling connectors, and the liquid level controller and the electromagnetic valves are provided with a controller; an oil receiving pipeline is formed by the connecting connectors, the pumps, the filter separators, the flowmeters and the oil tank through a pipeline and valves. When the oil receiving pipeline receives oil, a liquid level signal and a temperature signal, about the oil tank, which are transmitted by the liquid level controller, are received and displayed by the controller, and when the liquid level of the oil tank rises to a set value, the controller sends a signal and closes the pumps and the electromagnetic valves arranged on the oil tank.

Description

technical field [0001] The invention belongs to the technical field of aircraft refueling at general aviation airports and regional airports, and in particular relates to a control method for a skid-mounted aviation fuel refueling storage device, which is mainly used for adding aviation fuel to aircraft at general aviation airports and regional airports. Background technique [0002] Aviation fuel provides the power for the aircraft to fly, and the aircraft will be refueled before taking off. There are also patents about aircraft refueling in the prior art. For example, the utility model patent with application number 201220645757.2 discloses a control system for aircraft refueling, including PLC and power supply. The metering circuit and liquid crystal display, and the PLC are respectively connected with the oil circuit control valve, the metering circuit and the liquid crystal display; the PLC is connected with a leakage monitoring and alarm circuit and a system setting de...

Claims

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Application Information

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IPC IPC(8): B64F1/28
Inventor 戴均
Owner SICHUAN FEIDA SOURCE ENERGY EQUIP MFG CO LTD
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