CN103939070A - Injection device - Google Patents

Injection device Download PDF

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Publication number
CN103939070A
CN103939070A CN201410134124.9A CN201410134124A CN103939070A CN 103939070 A CN103939070 A CN 103939070A CN 201410134124 A CN201410134124 A CN 201410134124A CN 103939070 A CN103939070 A CN 103939070A
Authority
CN
China
Prior art keywords
injection device
fuel
cavity
ejector filler
filler panel
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.)
Granted
Application number
CN201410134124.9A
Other languages
Chinese (zh)
Other versions
CN103939070B (en
Inventor
梁枫
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.)
Zeng Guang
Original Assignee
Chengdu LVDI Technology 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 Chengdu LVDI Technology Co Ltd filed Critical Chengdu LVDI Technology Co Ltd
Priority to CN201410134124.9A priority Critical patent/CN103939070B/en
Publication of CN103939070A publication Critical patent/CN103939070A/en
Application granted granted Critical
Publication of CN103939070B publication Critical patent/CN103939070B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The invention discloses an injection device which comprises a propellant cavity, a spray orifice is formed in the propellant cavity, spray pipes are arranged between the propellant cavity and the spray orifice, the spray pipes are integrally connected with the spray orifice, the spray pipes are more than one in number, the propellant cavity is located on an injection device panel, embedded in the injection device panel and connected with the injection device panel through a weld joint, fuel nozzle components are arranged in the injection device panel, the fuel nozzle components are two in number, the two fuel nozzle components are arranged in the injection device panel in parallel, a fuel cavity is formed between the two fuel nozzle components, the top of the fuel cavity is communicated with the propellant cavity, air nozzles are arranged on the two sides of the fuel cavity, the two side faces of the air nozzles are connected with the fuel cavity and the fuel nozzle components respectively, and the bottom of the injection device panel is further provided with a sparking plug. According to the injection device, welding deformation is small, channeling cavity is avoided, process cycle is short, injection can be better conducted, parts of the injection device can be better protected, and endurance quality is good.

Description

Injection device
Technical field
The present invention relates to a kind of mechanical device, particularly a kind of injection device.
Background technology
Development along with automobile industry, constantly increasing of people's living standard, requirement to oil mass is day by day increased, but along with the development of oil field development, reservoir condition is increasingly sophisticated, and physical features is dangerous, be difficult to extract, crude oil volume increase becomes increasing, correspondingly, the requirement of oil field equipment and matched process technology is also being improved constantly.The steam injection generator of existing employing, can facilitate and better extract oil mass, oil circuit is exploited, injection device is wherein indispensable parts, can play key effect, but the pressure injecting to oil reservoir along with equipment is when constantly raise, its combustion pressure constantly increases, easily affect its spray effect, cause the impaired situation of injection device.
Summary of the invention
The technical problem to be solved in the present invention is: overcomes the problems referred to above, provides a kind of welding deformation little, avoided altering the situation in chamber, and short injection device of process-cycle.
To achieve these goals, the technical solution used in the present invention is such: injection device of the present invention, comprise propellant chamber, in propellant chamber, offer spray orifice, between propellant chamber and spray orifice, jet pipe is installed, jet pipe is connected with spray orifice one, and more than one of jet pipe, propellant chamber is positioned on ejector filler panel, and embed and be arranged on ejector filler panel, and with between ejector filler panel, by weld seam, be connected, fuel joint nozzle assembly is installed in ejector filler panel, fuel joint nozzle assembly is two, and two fuel joint nozzle assemblies are set in parallel in ejector filler panel, and offer fuel cavity between two fuel joint nozzle assemblies, fuel cavity top and propellant chamber are connected, fuel cavity both sides are provided with air and connect mouth, air connects mouth two sides and is connected with fuel cavity and fuel joint nozzle assembly respectively, ejector filler panel bottom is also provided with spark plug, spark plug is two, and be electrically connected between spark plug and fuel cavity.
Further, as a kind of concrete form of structure, air of the present invention connects mouth and fuel joint nozzle assembly all adopts O RunddichtringO to seal.
Further, as a kind of concrete form of structure, air of the present invention connects mouth top and is provided with edge.
Further, as a kind of concrete form of structure, jet pipe lateral surface of the present invention is provided with rib.
Compared with prior art, the invention has the advantages that: this injection device welding deformation is little, avoided altering the situation in chamber, and the process-cycle is short, can better carry out spray, can better protect each parts of ejector filler, endurance quality is good simultaneously.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the present invention is further described.
Fig. 1 is structural representation of the present invention;
In figure: 1. propellant chamber; 2. spray orifice; 3. jet pipe; 4. ejector filler panel; 5. weld seam; 6. fuel joint nozzle assembly; 7. fuel cavity; 8. air connects mouth; 9. spark plug.
The specific embodiment
In conjunction with the accompanying drawings, the present invention is further detailed explanation.These accompanying drawings are the schematic diagram of simplification, basic structure of the present invention is only described in a schematic way, so it only show the formation relevant with the present invention.
The preferred embodiment of injection device of the present invention as shown in Figure 1, comprise propellant chamber 1, in propellant chamber 1, offer spray orifice 2, between propellant chamber 1 and spray orifice 2, jet pipe 3 is installed, jet pipe 3 is connected with spray orifice 2 one, and more than one of jet pipe 3, propellant chamber 1 is positioned on ejector filler panel 4, and embed and be arranged on ejector filler panel 4, and with between ejector filler panel 4, by weld seam 5, be connected, fuel joint nozzle assembly 6 is installed in ejector filler panel 4, fuel joint nozzle assembly 6 is two, and two fuel joint nozzle assemblies 6 are set in parallel in ejector filler panel 4, and offer fuel cavity 7 between two fuel joint nozzle assemblies 6, fuel cavity 7 tops and propellant chamber 1 are connected, fuel cavity 7 both sides are provided with air and connect mouth 8, air connects mouth 8 two sides and is connected with fuel cavity 7 and fuel joint nozzle assembly 6 respectively, ejector filler panel 4 bottoms are also provided with spark plug 9, spark plug 9 is two, and electrical connection between spark plug 9 and fuel cavity 7, described air connects mouth 8 and fuel joint nozzle assembly 6 all adopts O RunddichtringO to seal, described air connects mouth 8 tops and is provided with edge, described jet pipe 3 lateral surfaces are provided with rib.
Injection device welding deformation of the present invention is little, avoided altering the situation in chamber, and the process-cycle is short, can better carry out spray, can better protect each parts of ejector filler simultaneously, and endurance quality is good.
The above-mentioned foundation desirable embodiment of the present invention of take is enlightenment, and by above-mentioned description, relevant staff can, within not departing from the scope of this invention technological thought, carry out various change and modification completely.The technical scope of this invention is not limited to the content on manual, must determine its technical scope according to claim scope.

Claims (4)

1. an injection device, comprise propellant chamber, it is characterized in that: in propellant chamber, offer spray orifice, between propellant chamber and spray orifice, jet pipe is installed, jet pipe is connected with spray orifice one, and more than one of jet pipe, propellant chamber is positioned on ejector filler panel, and embed and be arranged on ejector filler panel, and with between ejector filler panel, by weld seam, be connected, fuel joint nozzle assembly is installed in ejector filler panel, fuel joint nozzle assembly is two, and two fuel joint nozzle assemblies are set in parallel in ejector filler panel, and offer fuel cavity between two fuel joint nozzle assemblies, fuel cavity top and propellant chamber are connected, fuel cavity both sides are provided with air and connect mouth, air connects mouth two sides and is connected with fuel cavity and fuel joint nozzle assembly respectively, ejector filler panel bottom is also provided with spark plug, spark plug is two, and be electrically connected between spark plug and fuel cavity.
2. injection device according to claim 1, is characterized in that: described air connects mouth and fuel joint nozzle assembly all adopts O RunddichtringO to seal.
3. injection device according to claim 1, is characterized in that: described air connects mouth top and is provided with edge.
4. injection device according to claim 1, is characterized in that: described jet pipe lateral surface is provided with rib.
CN201410134124.9A 2014-04-04 2014-04-04 injection device Expired - Fee Related CN103939070B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410134124.9A CN103939070B (en) 2014-04-04 2014-04-04 injection device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410134124.9A CN103939070B (en) 2014-04-04 2014-04-04 injection device

Publications (2)

Publication Number Publication Date
CN103939070A true CN103939070A (en) 2014-07-23
CN103939070B CN103939070B (en) 2017-01-04

Family

ID=51186916

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410134124.9A Expired - Fee Related CN103939070B (en) 2014-04-04 2014-04-04 injection device

Country Status (1)

Country Link
CN (1) CN103939070B (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2377349Y (en) * 1999-03-25 2000-05-10 沈阳新光动力机械公司 Gas and steam producer for thermal recovery of viscous crude
CA2718811A1 (en) * 2008-03-19 2009-09-24 Heraldo Da Silva Couto Vitiated steam generator
CN102305404A (en) * 2011-07-19 2012-01-04 关兵 Re-combustion injector of combustor of re-combustion supercritical pressure gas-liquid phase fuel generator
CN102384463A (en) * 2011-07-19 2012-03-21 关兵 High-pressure and high-temperature resistant sealing device of after-burning super-critical pressure steam-injecting generator combustion chamber
RU2469185C1 (en) * 2011-07-08 2012-12-10 Открытое акционерное общество "Татнефть" имени В.Д. Шашина Development method of heavy oil or bitumen mine field with control of heat carrier pumped to well
CN203130282U (en) * 2013-03-15 2013-08-14 北京航天动力研究所 Integral injector
CN203879475U (en) * 2014-04-04 2014-10-15 雅克设计有限公司 Spraying and injecting device

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2377349Y (en) * 1999-03-25 2000-05-10 沈阳新光动力机械公司 Gas and steam producer for thermal recovery of viscous crude
CA2718811A1 (en) * 2008-03-19 2009-09-24 Heraldo Da Silva Couto Vitiated steam generator
RU2469185C1 (en) * 2011-07-08 2012-12-10 Открытое акционерное общество "Татнефть" имени В.Д. Шашина Development method of heavy oil or bitumen mine field with control of heat carrier pumped to well
CN102305404A (en) * 2011-07-19 2012-01-04 关兵 Re-combustion injector of combustor of re-combustion supercritical pressure gas-liquid phase fuel generator
CN102384463A (en) * 2011-07-19 2012-03-21 关兵 High-pressure and high-temperature resistant sealing device of after-burning super-critical pressure steam-injecting generator combustion chamber
CN203130282U (en) * 2013-03-15 2013-08-14 北京航天动力研究所 Integral injector
CN203879475U (en) * 2014-04-04 2014-10-15 雅克设计有限公司 Spraying and injecting device

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Legal Events

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C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C41 Transfer of patent application or patent right or utility model
CB03 Change of inventor or designer information

Inventor after: Zeng Guang

Inventor after: Li Jieke

Inventor after: Qi Molin

Inventor after: Zhang Bin

Inventor after: Li Peng

Inventor after: Ding Yan

Inventor before: Liang Feng

COR Change of bibliographic data
TA01 Transfer of patent application right

Effective date of registration: 20161123

Address after: Wenhui Street Xisi road 257000 in Shandong province Dongying city Dongying District No. 616 Dongsheng building

Applicant after: Zeng Guang

Address before: 610000 Jinjiang District, Chengdu, East Street, 18-32 No. 1, floor 5, layer 517,

Applicant before: Chengdu Lyudi Technology Co., Ltd.

C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20170104

Termination date: 20170404

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