CN104406338B - A kind of annular multiinjector ejection structure - Google Patents

A kind of annular multiinjector ejection structure Download PDF

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Publication number
CN104406338B
CN104406338B CN201410753222.0A CN201410753222A CN104406338B CN 104406338 B CN104406338 B CN 104406338B CN 201410753222 A CN201410753222 A CN 201410753222A CN 104406338 B CN104406338 B CN 104406338B
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China
Prior art keywords
nozzle
ejection structure
multiinjector
ring
injection
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CN201410753222.0A
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Chinese (zh)
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CN104406338A (en
Inventor
吴京泽
郑文远
包亚强
赵鹏涛
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Jincheng Nanjing Electromechanical Hydraulic Pressure Engineering Research Center Aviation Industry Corp of China
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Jincheng Nanjing Electromechanical Hydraulic Pressure Engineering Research Center Aviation Industry Corp of China
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Priority to CN201410753222.0A priority Critical patent/CN104406338B/en
Publication of CN104406338A publication Critical patent/CN104406338A/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B41/00Fluid-circulation arrangements

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)

Abstract

The present invention is a kind of novel ejection structure, and the model used of the most having installed mostly is concentration injection type structure.The injector of this kind of form has simple in construction, intensity high, but shortcoming is that injection ratio is relatively low, slightly inferior properties.The technical solution of the present invention is that ejection structure is divided into nozzle ring, rear seal ring and bump joint, and three kinds of parts, all by integrated machine add-on type, are then passed through being welded to form eductor.This arrangement enhances injection performance, avoid the problem that externally-hanging type nozzle strength is not enough, decrease weld seam quantity simultaneously, eliminate weak link, improve its global reliability.

Description

A kind of annular multiinjector ejection structure
Technical field
The present invention relates to a kind of ejection structure.
Background technology
Injector is applied relatively broad in air circulation refrigeration system.Traditional multiinjector injector injection Can still can, but due to structure and the problem of processing technique, during use, fault rate remains high, it is impossible to full Foot reliability requirement, is the most gradually substituted by slightly inferior properties but the higher centralized injector of reliability.
The model used of the most having installed mostly is concentration injection type structure.The injector of this kind of form has structure Simply, intensity high, but shortcoming is that injection ratio is relatively low, slightly inferior properties.
Summary of the invention
It is an object of the invention to provide a kind of novel ejection structure, this structure can be good at solving tradition ring Shape ejection structure and the problem of centralized ejection structure degraded performance, can well make up tradition multiinjector simultaneously The defect that ejection structure intensity, reliability are not enough.
A kind of annular multiinjector eductor structure for injector, it is characterised in that: include nozzle ring 1, after Seal ring 2 and bump joint 3, nozzle ring 1 is the multiinjector structure of global formation, and nozzle quantity and arrangement can roots Arrange in loop configuration according to performance need;Nozzle ring 1, rear seal ring 2 and bump joint 3 constitute airtight passage, Three passes through integrated machine add-on type, is then passed through being welded to form, and provides runner for injection air.
Advantageous Effects: compared with tradition ejection structure, this novel ejection structure driving nozzle is by outer cantilever Formula is improved to built-in, and processing technique is welded one by one by blast tube and is improved to overall machining, such as figure simultaneously Shown in.This new construction not only increases injection performance, avoids the problem that externally-hanging type nozzle strength is not enough, Decrease weld seam quantity simultaneously, eliminate weak link, improve its global reliability.
Accompanying drawing explanation
Fig. 1 is the structure composition schematic diagram of the present invention;
Fig. 2 is nozzle interior structural representation of the present invention;
Fig. 3 is tradition multiinjector ejection structure schematic diagram.
Detailed description of the invention
Below in conjunction with Figure of description, the present invention is described in further detail, refers to Figure of description 1-2, this The bright annular multiinjector eductor structure for injector, including nozzle ring 1, rear seal ring 2 and bump joint 3, nozzle ring 1 is the multiinjector structure of global formation, and nozzle quantity and arrangement can be according to performance need in annulars Arrange in structure;Nozzle ring 1, rear seal ring 2 and bump joint 3 constitute airtight passage, and three passes through integrated machine Add-on type, is then passed through being welded to form, and provides runner for injection air.

Claims (1)

1. the annular multiinjector eductor structure for injector, it is characterised in that: include nozzle ring (1), Rear seal ring (2) and bump joint (3), nozzle ring (1) is the multiinjector structure of global formation, nozzle number Amount and arrangement are arranged in loop configuration according to performance need;Nozzle ring (1), rear seal ring (2) and flange connect Head (3) constitutes airtight passage, and three passes through integrated machine add-on type, is then passed through being welded to form, empty for injection Air stripping is for runner.
CN201410753222.0A 2014-12-10 2014-12-10 A kind of annular multiinjector ejection structure Active CN104406338B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410753222.0A CN104406338B (en) 2014-12-10 2014-12-10 A kind of annular multiinjector ejection structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410753222.0A CN104406338B (en) 2014-12-10 2014-12-10 A kind of annular multiinjector ejection structure

Publications (2)

Publication Number Publication Date
CN104406338A CN104406338A (en) 2015-03-11
CN104406338B true CN104406338B (en) 2016-08-24

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CN201410753222.0A Active CN104406338B (en) 2014-12-10 2014-12-10 A kind of annular multiinjector ejection structure

Country Status (1)

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CN (1) CN104406338B (en)

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1751442A2 (en) * 1989-12-07 1992-07-30 Ленинградское высшее инженерное морское училище им.адм.С.О.Макарова Injector
RU2066404C1 (en) * 1994-04-26 1996-09-10 Владимир Анатольевич Калаев Spraying apparatus and method of its operation
RU2116521C1 (en) * 1996-06-05 1998-07-27 Акционерное общество открытого типа "Галион" Ejector
EP2194280A2 (en) * 2008-12-02 2010-06-09 Behr GmbH & Co. KG Ejector for a cooling circuit and manufacturing method
CN201771874U (en) * 2010-08-05 2011-03-23 无锡英威华耀科技有限公司 Air jetting amplifier
CN201926221U (en) * 2010-12-15 2011-08-10 大连海事大学 Ejector for ejection type refrigerating system
CN202621047U (en) * 2011-12-20 2012-12-26 中国航空工业集团公司金城南京机电液压工程研究中心 Ejection body of air ejector
CN102905975A (en) * 2010-04-09 2013-01-30 空中客车作业有限公司 Mixer assembly for an aircraft air conditioning system
CN103133430A (en) * 2012-12-28 2013-06-05 中国空气动力研究与发展中心设备设计及测试技术研究所 Efficient slotted multi-nozzle enhancing mixing ejector

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1751442A2 (en) * 1989-12-07 1992-07-30 Ленинградское высшее инженерное морское училище им.адм.С.О.Макарова Injector
RU2066404C1 (en) * 1994-04-26 1996-09-10 Владимир Анатольевич Калаев Spraying apparatus and method of its operation
RU2116521C1 (en) * 1996-06-05 1998-07-27 Акционерное общество открытого типа "Галион" Ejector
EP2194280A2 (en) * 2008-12-02 2010-06-09 Behr GmbH & Co. KG Ejector for a cooling circuit and manufacturing method
CN102905975A (en) * 2010-04-09 2013-01-30 空中客车作业有限公司 Mixer assembly for an aircraft air conditioning system
CN201771874U (en) * 2010-08-05 2011-03-23 无锡英威华耀科技有限公司 Air jetting amplifier
CN201926221U (en) * 2010-12-15 2011-08-10 大连海事大学 Ejector for ejection type refrigerating system
CN202621047U (en) * 2011-12-20 2012-12-26 中国航空工业集团公司金城南京机电液压工程研究中心 Ejection body of air ejector
CN103133430A (en) * 2012-12-28 2013-06-05 中国空气动力研究与发展中心设备设计及测试技术研究所 Efficient slotted multi-nozzle enhancing mixing ejector

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