Intermediate oil supply device of fuel system

A fuel supply device and fuel system technology, applied in the aviation field, can solve the problems of difficulty in meeting requirements, insufficient stability, simple structure, etc., and achieve the effects of high stability, ensuring normal and stable operation, and simple and reliable structure

Pending Publication Date: 2020-04-21
石家庄飞机工业有限责任公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, due to the simple structure and insufficient stability of the fuel system of the aviation piston engine, it is difficult to meet the requireme

Method used

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  • Intermediate oil supply device of fuel system
  • Intermediate oil supply device of fuel system
  • Intermediate oil supply device of fuel system

Examples

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Comparison scheme
Effect test

Embodiment 1

[0032] Such as Figure 1-3 As shown, the present invention provides a technical solution: comprising a tank body 2, an oil inlet 12 and an oil outlet 13 arranged on one side of the tank body, and a booster device and a fuel grid arranged inside the tank body 2 Blocking device 8;

[0033] The oil inlet 12 communicates with the tank 2; the booster device communicates with the oil outlet 13;

[0034] Said supercharging device comprises a first supercharging device 11 and a second supercharging device 14;

[0035] The first pressurization device 11 and the second pressurization device 14 are arranged vertically and staggered.

[0036] Specifically, the number of boosting devices is more than 2, and the model is ZC6-8 / RLB-82. The electric fuel booster pump has a pressure sensing function, which can transmit the pressure signal in the oil pump to the control motor, so as to Control the start and stop of the oil pump; the first supercharging device 11 and the second supercharging ...

Embodiment 2

[0041] Such as Figure 1-4 As shown, the present invention provides a technical solution: comprising a tank body 2, an oil inlet 12 and an oil outlet 13 arranged on one side of the tank body, and a booster device and a fuel grid arranged inside the tank body 2 Blocking device 8;

[0042] The oil inlet 12 communicates with the tank 2; the booster device communicates with the oil outlet 13;

[0043] Said supercharging device comprises a first supercharging device 11 and a second supercharging device 14;

[0044] The first pressurization device 11 and the second pressurization device 14 are arranged vertically and staggered.

[0045] Specifically, an anti-leakage device 6 is provided on the top of the box body 2; one end of the anti-leakage device 6 communicates with the outside of the box body; the other end of the anti-leakage device 6 communicates with the inside of the box body.

[0046] Specifically as Figure 4 As shown, the anti-leakage device 6 is a GF5500-401 float s...

Embodiment 3

[0050] Such as Figure 1-5 As shown, the present invention provides a technical solution: comprising a tank body 2, an oil inlet 12 and an oil outlet 13 arranged on one side of the tank body, and a booster device and a fuel grid arranged inside the tank body 2 Blocking device 8;

[0051] The oil inlet 12 communicates with the tank 2; the booster device communicates with the oil outlet 13;

[0052] Said supercharging device comprises a first supercharging device 11 and a second supercharging device 14;

[0053] The first pressurization device 11 and the second pressurization device 14 are arranged vertically and staggered.

[0054] Specifically, an alarm system is also included, and the alarm system includes an alarm device arranged on the top of the box body 2 , a controller 600 connected to the alarm device 7 , and an alarm indicator light 601 connected to the controller 600 . The alarm device 7 is an electronic liquid level sensor, which is connected to the cab controller 6...

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Abstract

The invention discloses an intermediate oil supply device of a fuel oil system, and belongs to the technical field of aviation. The intermediate oil supply device comprises a tank body, an anti-leakage device, an alarm device, an oil inlet, an oil outlet, a supercharging device, a fuel oil blocking device, a settling tank, an oil drain valve and a tank body mounting bracket. The intermediate oil supply device of the fuel oil system has the advantages of being simple and reliable in structure, high in stability and suitable for various flight conditions and flight attitudes, it can be guaranteed that the aircraft fuel oil system supplies oil to a turboprop engine more accurately and stably, and therefore normal and stable operation of the engine is guaranteed.

Description

technical field [0001] The patent of the invention relates to the field of aviation technology, in particular to an intermediate fuel supply device for a fuel system. Background technique [0002] The aircraft fuel system is also called the external fuel system, because there is another system on the engine that delivers the fuel to the combustion chamber, which is called the internal fuel system. The heart of the aircraft - the engine relies on the combustion of fuel to generate heat to do work and propel the aircraft to fly. Fuel is the energy of the aircraft, and the fuel system is the supply system of aircraft energy. [0003] The main functions of the fuel system are as follows: store fuel; safely and reliably deliver fuel to the engine and APU under specified flight conditions; adjust the center of gravity to maintain aircraft balance and wing structure stress. [0004] There are two main types of engines used in general aviation aircraft: aviation piston engines and...

Claims

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Application Information

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IPC IPC(8): B64D37/06B64D37/20B64D37/32B64D37/34B64D47/02
CPCB64D37/06B64D37/20B64D37/32B64D37/34B64D47/02
Inventor 张旺春徐皓阁李志强
Owner 石家庄飞机工业有限责任公司
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