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Gravity refueling type multifunctional integrated aviation oil filling device

A filling device and multi-functional technology, which is applied in the direction of liquid conveying device, etc., can solve the problem that fuel trucks are not suitable for airports with small and medium flow, and achieve the effects of improving convenience, compact structure and improving practicability.

Inactive Publication Date: 2016-07-20
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 oil depots and refueling trucks are not suitable for use in airports with small and medium flow rates, the present invention provides a gravity filling multifunctional integrated aviation fuel filling device, which can collect oil, refuel, send oil, store and The stirring function is integrated, which reduces the construction and maintenance costs of small and medium flow airports

Method used

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  • Gravity refueling type multifunctional integrated aviation oil filling device
  • Gravity refueling type multifunctional integrated aviation oil filling device
  • Gravity refueling type multifunctional integrated aviation oil filling device

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0074] Implementation of embodiment one oil collection function:

[0075] 1. 1A warehouse oil collection (medium 1)

[0076] The first connection joint A1-1 is connected to the oil outlet of the tanker, the valves A1-2, A1-4, A1-8, A1-10, A1-14, A1-16 are opened, and the valves A2-1, A2-3, A3 -15 off,

[0077] Start the pump A1-5 to collect oil, and adjust the opening of the valve A1-6 to adjust the flow of the pump.

[0078] The medium 1 is transported by the pump A1-5, filtered and separated by the first filter separator A1-9, measured by the flow meter A1-12, and finally enters the storage tank A warehouse. It is not necessary to use a flow meter in the process of collecting oil in A warehouse.

[0079] 1. 2B warehouse oil collection (medium 2)

[0080] The first connection joint B1-1 is connected to the oil outlet of the tanker, the valves B1-2, B1-4, B1-8, B1-10, B1-14, B1-16 are opened, and the valves B2-1, B2-3, B3 -15 off,

[0081] Start the pump B1-5 to collect ...

Embodiment 2

[0083] The realization of embodiment two refueling function:

[0084] 2.1 Refueling in tank A (medium 1)

[0085] The fueling gun A4-10 is connected with the oil receiving port of the oil receiving equipment, and the valve A4-2 is opened.

[0086] Dispenser A4-4 controls start-up pump A4-1 to transport medium 1, medium 1 is transported by fuel pump A4-1, is metered and displayed by dispenser A4-4, and is filtered and separated by second filter separator A4-5. Then it enters the oil receiving equipment through the refueling reel A4-7, the pull-off valve A4-8, the refueling hose A4-9, and the refueling gun A4-10. After the refueling is completed, the refueling gun is closed, and the signal is fed back to the refueling machine, and the refueling machine controls the pump A4-1 to stop.

[0087] The fueling gun A4-14 is connected with the oil receiving port of the oil receiving equipment, and the valve A4-3 is opened.

[0088] Dispenser A4-4 controls start-up pump A4-1 to transp...

Embodiment 3

[0097] Implementation of Embodiment Three Stirring Function

[0098] 3. 1A warehouse stirring function (medium 1)

[0099] Valves A3-1, A3-3, A3-13, A3-15, A1-4, A1-8, A1-10, A1-14, A1-16 open, valves A3-9, A3-10, A3-6 (valve group), A3-16, A1-2, A1-13 closed,

[0100]Start the pump A1-5 for medium delivery, and adjust the opening of the valve A1-6 to adjust the flow of the pump.

[0101] Medium 1 comes out of bin A, transported by pump A1-5, filtered and separated by oil collection filter separator A1-9, and measured by flow meter A1-12 (A1-10, A1-14 can also be closed, A1- 13 open, without flow meter A1-12 measurement), into the storage tank A warehouse.

[0102] 3. Stirring function of bin 2B (medium 2)

[0103] Valves B3-1, B3-3, B3-13, B3-15, B1-4, B1-8, B1-10, B1-14, B1-16 open, valves B3-9, B3-10, B3-6 (valve group), B3-16, B1-2, B1-13 closed,

[0104] Start the pump B1-5 for medium delivery, and adjust the opening of the valve B1-6 to adjust the flow of the pump....

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Abstract

The invention belongs to the technical field of refueling in airports and discloses a gravity refueling type multifunctional integrated aviation oil filling device which solves the problem that existing oil depots and refueling vehicles are not suitable for small-and medium-flow airports.The device comprises a skid-mounted seat, an oil tank with oil chambers is arranged on the skid-mounted seat, each oil chamber is provided with a refueling pump, an oil collection mechanism and an oil filling mechanism.Each oil collection mechanism comprises a first connector for communication with a tank truck, each first connector is communicated with a pump which is communicated with an oil collection filter separator, and each oil collection filter separator is communicated with a flow meter which is communicated with the corresponding oil chamber of the oil tank.Each oil filling mechanism comprises an oil filling pump which is communicated with a first oil outlet pipe used for communication with the corresponding oil chamber, each first oil outlet pipeline is communicated with an oil filler which is connected with at least one oil filling filter separator, and each oil filling filter separator is provided with at least one oil gun.

Description

technical field [0001] The invention belongs to the technical field of refueling at aviation airports, and in particular relates to a gravity filling multifunctional integrated aviation fuel filling device. 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 on 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. PLC is connected to the power supply. The metering circuit and liquid crystal display, 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 device. [0003] The invention patent with the application number 201210330746.X discloses an aircraft refueling device in w...

Claims

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Application Information

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IPC IPC(8): B64F1/28
CPCB64F1/28
Inventor 戴钧
Owner SICHUAN FEIDA SOURCE ENERGY EQUIP MFG CO LTD
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