CN105545550A - Multifunctional fuel pump - Google Patents

Multifunctional fuel pump Download PDF

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Publication number
CN105545550A
CN105545550A CN201410588143.9A CN201410588143A CN105545550A CN 105545550 A CN105545550 A CN 105545550A CN 201410588143 A CN201410588143 A CN 201410588143A CN 105545550 A CN105545550 A CN 105545550A
Authority
CN
China
Prior art keywords
fuel
pump
oil
cores
design
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
Application number
CN201410588143.9A
Other languages
Chinese (zh)
Inventor
李小刚
牛量
王晓阳
刘苏彦
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Xian Aircraft Design and Research Institute of AVIC
Original Assignee
Xian Aircraft Design and Research Institute of AVIC
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Xian Aircraft Design and Research Institute of AVIC filed Critical Xian Aircraft Design and Research Institute of AVIC
Priority to CN201410588143.9A priority Critical patent/CN105545550A/en
Publication of CN105545550A publication Critical patent/CN105545550A/en
Pending legal-status Critical Current

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Abstract

The invention belongs to the technical field of fuel pumps, in particular to a multifunctional fuel pump. According to the multifunctional fuel pump, the split type single pump case and double pump core structure and design are adopted; pump cores are independently controlled, one pump core works in the normal fuel conveying process, and the other pump core is subjected to cold standby; when fuel needs to be conveyed simultaneously or drained emergently, the double pump cores work, the requirements of pressure and flow of the fuel conveying state and the emergent fuel draining state can be met, and the fuel conveying reliability is improved; by adopting the single pump case design, the occupied space can be reduced, and the weight can be reduced; the split type self-sealing valve design is adopted, when the pump cores are disassembled, the fuel in a fuel tank does not need to be drained, cables are prevented from entering the fuel tank, and the safety and the maintenance performance of a fuel system are improved.

Description

A kind of multifunction burning oil pump
Technical field
The invention belongs to fuel pump technical field, particularly a kind of multifunction burning oil pump.
Background technique
For installing space and weight demands higher aircraft fuel system design, raising system plyability function becomes a main trend, traditional aircraft fuel system design, oil transfer pump and fuel jettison pump independent design, installing space occupy-place is more, and the weight cost paid is comparatively large, and pump case pump core does not adopt split type self-styled valve design, maintainability is poor, cannot meet design requirement.
Summary of the invention
The object of the invention is, propose a kind of multifunction burning oil pump can saved space, be convenient to maintenance.
Technological scheme of the present invention is: described fuel pump comprises fuel oil suction port 1, self-styled valve 2, pump case 3, check valve 4, pump core 5, control switch 6, it is characterized by: in pump case 3, have two cover pump cores 5, fuel oil suction port 1 and self-styled valve 2, two cover fuel pumps share an oil outlet, are provided with two independently check valves 4 at oil outlet place;
Two cover fuel pumps control by control switch 6 is independent;
When extraction pump core 5, self-styled valve 2 realizes pump case 3 isolates with fuel oil.
Accompanying drawing explanation
Fig. 1 is schematic diagram of the present invention.
In figure: fuel oil suction port 1; Self-styled valve 2; Pump case 3; Check valve 4; Pump core 5; Pump core control switch 6; Wingbar 7.
Embodiment
A kind of multifunction burning oil pump, adopts single pump case double pump core structure designs, is made up of fuel oil suction port 1, self-styled valve 2, pump case 3, check valve 4, pump core 5, control switch 6.This invention is installed on fuel tank inboard wing beam 7, fuel oil by two independently fuel oil suction port 1 enter fuel pump through self-styled valve 2, through pump core 5 supercharging by collecting outflow after two independently check valve 4.Two fuel pump cores 5 control by control switch 6 is independent, during normal oil transportation, single pump core work, another pump core cold standby can improve oil transportation reliability, oil outlet set up two independently check valve 4 can prevent fuel oil from flowing backwards, interference; When needing fuel dump, double pump core works simultaneously, meets pressure and the traffic requirement of fuel dump.
This invention can meet pressure under oil transportation and fuel dump two kinds of working staties and traffic requirement, and reduce installing space, weight loss effect is obvious.Pump case 3 and pump core 5 adopt split type independent design, and cable is oil-feed tank not, and when pump core 5 needs to safeguard, fuel oil can be isolated by self-styled valve 2 automatically, without the need to releasing fuel oil in fuel tank, improves oil-fired system Security and maintainability.

Claims (3)

1. a multifunction burning oil pump, described fuel pump comprises fuel oil suction port (1), self-styled valve (2), pump case (3), check valve (4), pump core (5), control switch (6), it is characterized by: in pump case (3), have two cover pump cores (5), fuel oil suction port (1) and self-styled valve (2), two cover fuel pumps share an oil outlet, are provided with two independently check valves (4) at oil outlet place.
2. multifunction burning oil pump according to claim 1, is characterized by: two cover fuel pumps control by control switch (6) is independent.
3. multifunction burning oil pump according to claim 1 and 2, is characterized by: when extraction pump core (5), and self-styled valve (2) realizes pump case (3) isolates with fuel oil.
CN201410588143.9A 2014-10-28 2014-10-28 Multifunctional fuel pump Pending CN105545550A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410588143.9A CN105545550A (en) 2014-10-28 2014-10-28 Multifunctional fuel pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410588143.9A CN105545550A (en) 2014-10-28 2014-10-28 Multifunctional fuel pump

Publications (1)

Publication Number Publication Date
CN105545550A true CN105545550A (en) 2016-05-04

Family

ID=55825009

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410588143.9A Pending CN105545550A (en) 2014-10-28 2014-10-28 Multifunctional fuel pump

Country Status (1)

Country Link
CN (1) CN105545550A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114278612A (en) * 2021-12-28 2022-04-05 中国航空工业集团公司金城南京机电液压工程研究中心 Skin installation fuel pump with dismouting is from seal structure

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH11257175A (en) * 1998-03-06 1999-09-21 Keihin Corp Fuel pump device
CN1811158A (en) * 2004-11-30 2006-08-02 卡特彼勒公司 Variable discharge fuel pump
CN102295250A (en) * 2011-08-30 2011-12-28 陈海波 Dual pump converging energy-saving control system for hydraulic system of forklift truck
CN102673794A (en) * 2012-06-08 2012-09-19 中国航空工业集团公司西安飞机设计研究所 Overhead fuel drainage device using fuel supply pumps as power
CN203130672U (en) * 2012-12-05 2013-08-14 重庆市南川区富民科技推广中心 Double-pump oil supply system
CN103291462A (en) * 2013-01-05 2013-09-11 中国航空工业集团公司西安飞机设计研究所 Oil drainage method of split type fuel pump

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH11257175A (en) * 1998-03-06 1999-09-21 Keihin Corp Fuel pump device
CN1811158A (en) * 2004-11-30 2006-08-02 卡特彼勒公司 Variable discharge fuel pump
CN102295250A (en) * 2011-08-30 2011-12-28 陈海波 Dual pump converging energy-saving control system for hydraulic system of forklift truck
CN102673794A (en) * 2012-06-08 2012-09-19 中国航空工业集团公司西安飞机设计研究所 Overhead fuel drainage device using fuel supply pumps as power
CN203130672U (en) * 2012-12-05 2013-08-14 重庆市南川区富民科技推广中心 Double-pump oil supply system
CN103291462A (en) * 2013-01-05 2013-09-11 中国航空工业集团公司西安飞机设计研究所 Oil drainage method of split type fuel pump

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114278612A (en) * 2021-12-28 2022-04-05 中国航空工业集团公司金城南京机电液压工程研究中心 Skin installation fuel pump with dismouting is from seal structure

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PB01 Publication
C10 Entry into substantive examination
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WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20160504

WD01 Invention patent application deemed withdrawn after publication