CN201277095Y - Fuel oil reversal valve in engine control system - Google Patents

Fuel oil reversal valve in engine control system Download PDF

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Publication number
CN201277095Y
CN201277095Y CNU2008200966587U CN200820096658U CN201277095Y CN 201277095 Y CN201277095 Y CN 201277095Y CN U2008200966587 U CNU2008200966587 U CN U2008200966587U CN 200820096658 U CN200820096658 U CN 200820096658U CN 201277095 Y CN201277095 Y CN 201277095Y
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CN
China
Prior art keywords
valve
armature
pole shoe
fuel oil
control system
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.)
Expired - Fee Related
Application number
CNU2008200966587U
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Chinese (zh)
Inventor
苗建中
徐国勇
龚锐
申波
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.)
Guizhou Honglin Machinery Co Ltd
Original Assignee
Guizhou Honglin Machinery Co Ltd
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 Guizhou Honglin Machinery Co Ltd filed Critical Guizhou Honglin Machinery Co Ltd
Priority to CNU2008200966587U priority Critical patent/CN201277095Y/en
Application granted granted Critical
Publication of CN201277095Y publication Critical patent/CN201277095Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model provides a fuel reversing valve whose structure is improved, and comprises a valve body 1, a pole shoe 2, a coil component 3, a keeper 4, a keeper tube 5, an ejector pin 6, an aprons 7, a guide seat 8, a valve 9, a spring 10 and a spring seat 11 and the like, wherein one end of the ejector pin 6 is pressed in the keeper 4 to form a keeper component, the guide seat 8 is pressed in the pole shoe 2 to form a pole shoe component, the keeper component and the pole shoe component are commonly arranged in the keeper tube 5, an opening end of the keeper tube 5 is embedded in a groove of the pole shoe 2 through squeezing a nosing to form a valve core component, then an electromagnet is formed after a coil 3 is arranged, the spring seat 11, the spring 10 and a valve 9 are orderly arranged in the valve body 1, the spring 10 is fixed in the spring seat 11, and a slide valve matching part is combined and formed after the aprons 7 is sealed. When assembling, the spring seat 11 is put from the left end, the electromagnet and the slide valve matching part are connected through thread, thereby guaranteeing the whole sealing performance of products.

Description

Fuel oil selector valve in the engine control system
Technical field
The present invention relates to a kind of fuel oil selector valve, particularly relate to the fuel oil selector valve in the aeroengine control system.
Background technique
In aeroengine control system, fuel oil selector valve originally, as shown in Figure 1, there is following defective in this selector valve:
Old-fashioned selector valve slide valve couple spare is an integral body with electromagnet, because this valve required precision height, the apolegamy size is many, is not easy to assembling and debugging, causes up-to-standard rate lower; The fitting surface of old-fashioned valve armature and armature pipe is right cylindrical, and armature and armature pipe surface of contact are big, and frictional force is big; Old-fashioned in addition valve armature pipe adopts two ends to close up, and sealing is relatively poor, and the manufacturability during the spring seat assembling also is difficult to guarantee.
Summary of the invention
In order to overcome the above shortcoming of old-fashioned valve, the invention provides a kind of fuel oil selector valve (see figure 2) of architecture advances.This selector valve comprises: valve body 1, pole shoe 2, coil block 3, armature 4, armature pipe 5, push rod 6, cushion rubber 7, guide holder 8, valve 9, spring 10, spring seat 11 component such as grade.One end of push rod 6 is pressed in the armature 4 and forms armature component, guide holder 8 is pressed in the pole shoe 2 and forms pole shoe member, armature component and pole shoe member are packed in the armature pipe 5 jointly, by the extruding closing in opening end of armature pipe 5 is embedded in the groove of pole shoe 2, form mangetic core assembly, load onto coil 3 backs then and form electromagnet, in design, armature 4 front ends are designed to certain angle [alpha], form the air guide angle, when avoiding armature 4 motions with armature pipe 5 generation vacuum; There is one section supporting part P at armature 4 middle parts, and armature 4 is conical surface M with the counterface of pole shoe 2, and has increased guide holder 8 in pole shoe 4, move in armature pipe 5 flexibly and the power of reducing friction to guarantee armature 4; With spring seat 11, spring 10 and valve 9 valve body 1 of packing into successively, spring 10 is fixed in the spring seat 11, constitute slide valve couple spare, in order to guarantee that spring seat 11 is connected with the reliable of valve body 1, be designed to the right-hand member of valve body 1 step-like, during assembling, spring seat 11 is put into from left end, the joint N of electromagnet and slide valve couple spare is with being threaded, by cushion rubber 7 sealings, in order to prevent to become flexible, after qualified to the performance adjustment of fuel oil selector valve, to also rivet between the large end face of pole shoe in the mangetic core assembly and the valve body end face, thereby guaranteed the overall tightness of product.
Fuel oil selector valve of the present invention is a kind of two position three way directional control valve.(see shown in Figure 2) during no electric circuit, the elastic force that spring 10 produces is pushed valve 9 and armature 4 to the left side, the right side at the B mouth, valve body and valve form opening D, on the left side of B mouth, valve body and valve form lap E simultaneously, and (seeing shown in Figure 3) seals, fuel oil advanced the A mouth from the B mouth and went out as seen from Figure 2 this moment; During energising, coil block 3 produces electromagnetic force, and electromagnetic force drives armature 4, and armature 4 is drawn onto the limit on the right-right-hand limit position, by push rod 6, overcome the elastic force of return spring 8, promote valve 9 and move right, on the left side of B mouth, valve body and valve form certain opening, simultaneously form certain lap at B mouth right side valve body and valve, seal, fuel oil advances the C mouth from the B mouth and goes out at this moment.
In order to improve the sealing of valve body, armature pipe 5 adopts overall structure, an end opening (seeing shown in Figure 5) only, only opening end is closed up during assembling, changed the structure that all closes up in armature pipe two ends in the past, slide valve couple spare and electromagnet be with being threaded, and with cushion rubber 7 sealings (seeing shown in Figure 2), after performance adjustment is qualified.
Description of drawings
Fig. 1 is the structural representation of old-fashioned selector valve.
Fig. 2 is the structural representation of selector valve of the present invention.
Fig. 3 is the valve body and the valve cooperating structure schematic representation of selector valve of the present invention.
Fig. 4 is the mangetic core assembly structural representation of selector valve of the present invention.
Fig. 5 is the armature pipe structural representation.
Among the figure: 1-valve body, 2-pole shoe, 3-coil block, 4-armature, the 5-armature pipe, 6-push rod, 7-cushion rubber, 8-guide holder, the 9-valve, 10-spring, 11-spring seat, the A-fuel outlet, B-fuel inlet, C-fuel outlet, open part between D-valve body and valve, the lap between E-valve body and valve, the counterface of M-armature and pole shoe, the joint L-push rod of N-electromagnet and slide valve couple spare exceeds the length of guide holder right side, the supporting part at P-armature middle part, α-air guide angle.
Embodiment
Now with the example that is designed to of the fuel oil selector valve in certain aeroengine control system.As shown in Figure 2, this valve comprises valve body 1, pole shoe 2, coil block 3, armature 4, armature pipe 5, push rod 6, cushion rubber 7, guide holder 8, valve 9, spring 10, spring seat 11 component such as grade.The air guide angle α of armature 4 front ends is set at 15 °, the supporting part P at armature 4 middle parts is set at 2.5mm, armature 4 is 90 ° with the conical surface M that cooperates of pole shoe 2, one end of push rod 6 is pressed in the armature 4 and forms armature component, guide holder 8 is pressed in the pole shoe 2 forms pole shoe member, armature component and pole shoe member are packed in the armature pipe 5 jointly, embed in the groove of pole shoe 2 by the extruding opening end that makes armature pipe 5 that closes up, form the mangetic core assembly (see figure 4), load onto coil 3 backs then and form electromagnet.During no electric circuit, push rod 6 can not exceed the right side of guide holder 8, and during energising, push rod 6 need exceed the right side of guide holder 8, and its length L=0.6 ± 0.01mm, this value are exactly the stroke of valve.With spring seat 11, spring 10 and valve 9 valve body 1 of packing into successively, spring 10 is fixed in the spring seat 11, after cushion rubber 7 sealings, constitute slide valve couple spare, the right side by reconditioning valve body 1 and the left side of valve 9 guarantee the following requirement of slide valve couple spare: when the valve no electric circuit, for flow and the sealing that guarantees valve, valve body 1 and D (the be opening value)=0.5 ± 0.1mm (see shown in Figure 3) of valve 9 in the formation of the right side of oil outlet, E (the being lap)=0.08~0.1mm that forms on the left side; When valve is switched on, electromagnet promotes valve 9 toward moving right, D (being the opening value)=0.5 ± 0.1mm that valve body 1 and valve 9 are formed on the left side of oil outlet, E (the being lap)=0.1~0.2mm that forms on the right side, thus reach valve commutation and dependable flow and sealing requirements under energising or cold situation.

Claims (5)

1, fuel oil selector valve in a kind of engine control system, it is characterized in that: one section of this fuel oil selector valve push rod (6) is pressed into formation armature component in the armature (4), guide holder (8) is pressed into and forms pole shoe member in the pole shoe (2), armature component and pole shoe member are packed in the armature pipe (5) jointly, by the extruding closing in opening end of armature pipe (5) is embedded in the groove of pole shoe (2), form mangetic core assembly, load onto coil (3) back then and form electromagnet, with spring seat (11), spring (10) and valve (9) valve body (1) of packing into successively, after cushion rubber (7) sealing, constitute slide valve couple spare, electromagnet and slide valve couple spare are with being threaded.
2, the fuel oil selector valve in the engine control system according to claim 1 is characterized in that: the front end of armature (4) has an air guide angle (α), and there is one section supporting section (P) at the middle part.
3, the fuel oil selector valve in the engine control system according to claim 1 is characterized in that: the right-hand member of valve body (1) becomes step-like.
4, the fuel oil selector valve in the engine control system according to claim 1 is characterized in that: armature (4) is the conical surface with the counterface of pole shoe (2).
5, the fuel oil selector valve in the engine control system according to claim 1 is characterized in that: armature pipe (5) adopts overall structure, only an end opening.
CNU2008200966587U 2008-09-22 2008-09-22 Fuel oil reversal valve in engine control system Expired - Fee Related CN201277095Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNU2008200966587U CN201277095Y (en) 2008-09-22 2008-09-22 Fuel oil reversal valve in engine control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNU2008200966587U CN201277095Y (en) 2008-09-22 2008-09-22 Fuel oil reversal valve in engine control system

Publications (1)

Publication Number Publication Date
CN201277095Y true CN201277095Y (en) 2009-07-22

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CNU2008200966587U Expired - Fee Related CN201277095Y (en) 2008-09-22 2008-09-22 Fuel oil reversal valve in engine control system

Country Status (1)

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CN (1) CN201277095Y (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102287268A (en) * 2011-08-05 2011-12-21 中国南方航空工业(集团)有限公司 State transition valve and system
CN102588583A (en) * 2012-03-18 2012-07-18 上海沪工汽车电器有限公司 Vehicular gear electromagnet
CN108131470A (en) * 2017-12-20 2018-06-08 中国航发贵州红林航空动力控制科技有限公司 A kind of two position and four-way reversing valves for fuel regulator
CN108131469A (en) * 2017-12-20 2018-06-08 中国航发贵州红林航空动力控制科技有限公司 The normally opened fuel solenoid valve of two-bit triplet
CN109555629A (en) * 2018-11-23 2019-04-02 中国航发北京航科发动机控制系统科技有限公司 A kind of wide scope allocation proportion governor valve
CN114382916A (en) * 2022-01-23 2022-04-22 徐州博安科技发展有限责任公司 Novel large-flow ejector rod type reversing valve

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102287268A (en) * 2011-08-05 2011-12-21 中国南方航空工业(集团)有限公司 State transition valve and system
CN102287268B (en) * 2011-08-05 2013-10-30 中国南方航空工业(集团)有限公司 State transition valve and system
CN102588583A (en) * 2012-03-18 2012-07-18 上海沪工汽车电器有限公司 Vehicular gear electromagnet
CN108131470A (en) * 2017-12-20 2018-06-08 中国航发贵州红林航空动力控制科技有限公司 A kind of two position and four-way reversing valves for fuel regulator
CN108131469A (en) * 2017-12-20 2018-06-08 中国航发贵州红林航空动力控制科技有限公司 The normally opened fuel solenoid valve of two-bit triplet
CN109555629A (en) * 2018-11-23 2019-04-02 中国航发北京航科发动机控制系统科技有限公司 A kind of wide scope allocation proportion governor valve
CN114382916A (en) * 2022-01-23 2022-04-22 徐州博安科技发展有限责任公司 Novel large-flow ejector rod type reversing valve

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
EE01 Entry into force of recordation of patent licensing contract

Assignee: Guizhou red forest Electric Control Technology Co Ltd

Assignor: Guizhou Honglin Machinery Corporation Ltd.

Contract fulfillment period: 2009.9.1 to 2014.8.31

Contract record no.: 2009520000019

Denomination of utility model: Fuel oil reversal valve in engine control system

Granted publication date: 20090722

License type: Exclusive license

Record date: 20091202

LIC Patent licence contract for exploitation submitted for record

Free format text: EXCLUSIVE LICENSE; TIME LIMIT OF IMPLEMENTING CONTACT: 2009.9.1 TO 2014.8.31; CHANGE OF CONTRACT

Name of requester: GUIZHOU HONGLIN VEHICLE ELECTRONIC CONTROL TECHNOL

Effective date: 20091202

CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20090722

Termination date: 20170922

CF01 Termination of patent right due to non-payment of annual fee