CN206883464U - Composite ceramics blast nozzle - Google Patents

Composite ceramics blast nozzle Download PDF

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Publication number
CN206883464U
CN206883464U CN201720788634.7U CN201720788634U CN206883464U CN 206883464 U CN206883464 U CN 206883464U CN 201720788634 U CN201720788634 U CN 201720788634U CN 206883464 U CN206883464 U CN 206883464U
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CN
China
Prior art keywords
pressure inlet
pipe
rearward end
caliber
pore
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
CN201720788634.7U
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Chinese (zh)
Inventor
陆永明
朱晨红
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.)
Zhejiang Hong Taigao Industry Science And Technology Ltd
Original Assignee
Zhejiang Hong Taigao Industry Science And Technology Ltd
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Filing date
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Priority to CN201720788634.7U priority Critical patent/CN206883464U/en
Application granted granted Critical
Publication of CN206883464U publication Critical patent/CN206883464U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

A kind of composite ceramics blast nozzle, it is that nozzle body is made in sintering in high temperature environments after injection or compression molding by the ceramic material that zirconium oxide and alumina composite form, described nozzle body is made up of preceding first pressure inlet and the second pressure inlet to connect after, the first described pressure inlet is integrally formed by leading portion straight pipe and back segment conical horn shape collapsible tube, the second described pressure inlet is that the taper draw for growing section small-angle is formed, the second described pressure inlet front end small-caliber end portion is located in the heavy caliber pore of the first pressure inlet rearward end or with the heavy caliber pore of the first pressure inlet rearward end at a distance of many 15mm distances;First pressure inlet and the second pressure inlet are installed in the shell of derusting by sandblasting equipment and are wrapped;It has it is simple in construction, it is easy to make, cost of manufacture can be reduced, flow velocity is high, supercharging is fast, the features such as wear-resistant, corrosion-resistant, resistance to erosion, high temperature resistant.

Description

Composite ceramics blast nozzle
Technical field
A kind of composite ceramics blast nozzle is the utility model is related to, is mainly used in derusting by sandblasting equipment, belongs to abrasive blast equipment Parts technical field.
Background technology
At present, grow as equipment manufacture continues to develop, abrasive blast equipment purposes is more and more, on Chinese patent publication A kind of split boron carbide blast nozzle is disclosed, is made up of nozzle aperture, mouth body, wherein mouth body is made up of split one and split two, split One and split two be combined the boron carbide blast nozzle to form a whole, centre sets nozzle aperture;Although boron carbide is wear-resisting with its Resistant to elevated temperatures characteristic is widely used in the manufacturing of blast nozzle, but this boron carbide blast nozzle is used in abrasive blast equipment still The problem of anti-wear performance and inadequate resistance to elevated temperatures be present, easily reduce its service life because of high speed sandblasting, moreover, this The toughness of kind blast nozzle is also inadequate, easily causes to damage in use.Now with the continuous hair of zirconia ceramics material application Exhibition, has there is application of the ceramic sand jet in abrasive blast equipment, but existing ceramic sand jet although possess have it is enough strong Degree, but toughness is the absence of, it therefore, can equally cause to use upper rapid wear, reduce service life, and existing ceramic sand jet There is also unreasonable in structure, flow velocity is not high enough, thus the effect of derusting by sandblasting is not ideal enough.
The content of the invention
The purpose of this utility model is to overcome the shortcomings of the prior art, and provides a kind of simple in construction, making side Just, cost of manufacture can be reduced, flow velocity is high, supercharging is fast, wear-resistant, corrosion-resistant, resistance to erosion, resistant to elevated temperatures composite ceramics blast nozzle.
The purpose of this utility model is completed by following technical solution, a kind of composite ceramics blast nozzle, it be by The ceramic material that 25-35% zirconium oxide and 65-75% alumina composite form is after injection or compression molding in hot environment Nozzle body is made in lower sintering, and described nozzle body is made up of preceding first pressure inlet and the second pressure inlet to connect after, institute The first pressure inlet stated is integrally formed by leading portion straight pipe and back segment conical horn shape collapsible tube, and the second described pressure inlet is one The taper draw of long section small-angle is formed, and the second described pressure inlet front end small-caliber end portion is located at the first pressure inlet rearward end At a distance of many 15mm distances in heavy caliber pore or with the heavy caliber pore of the first pressure inlet rearward end.
As preferred:The length of first pressure inlet is 90-110mm, and the pipe range of back segment conical horn shape collapsible tube is 35—45mm;The caliber of leading portion straight pipe is 9-10mm;The maximum caliber of back segment conical horn shape collapsible tube is 23-27mm; The length of second pressure inlet is 55-65mm, and the second pressure inlet front end is connected on the pipe end bore of the first pressure inlet rearward end For 11-13mm, the pipe end bore of rearward end is 14-16mm.
As preferred:First pressure inlet and the second pressure inlet are installed in the shell of derusting by sandblasting equipment and wrapped Wrap up in, the heavy caliber pore of the second described small-bore end in pressure inlet front end and the first pressure inlet rearward end at a distance of 8-12mm away from From.
The utility model have it is simple in construction, it is easy to make, can reduce cost of manufacture, flow velocity is high, supercharging is fast, it is wear-resistant, The features such as corrosion-resistant, resistance to erosion, high temperature resistant.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model.
Embodiment
The utility model is described in detail below in conjunction with accompanying drawing:It is described in the utility model a kind of multiple shown in Fig. 1 Ceramic sand jet is closed, it is by injection or mould by the ceramic material that 25-35% zirconium oxide and 65-75% alumina composite form Nozzle body is made in sintering in high temperature environments after molded, and described nozzle body connects by preceding first pressure inlet 1 and after The second pressure inlet 2 form, the first described pressure inlet 1 is by 4 integral structure of leading portion straight pipe 3 and back segment conical horn shape collapsible tube Into the second described pressure inlet 2 is that the taper draw for growing section small-angle is formed, and the described front end of the second pressure inlet 2 is small-bore End is located in the heavy caliber pore 5 of the rearward end of the first pressure inlet 1 or the phase of heavy caliber pore 5 with the rearward end of the first pressure inlet 1 Away from many 15mm distances.
A kind of embodiment of the present utility model is:The length L1 of first pressure inlet 1 is 90-110mm, back segment taper The pipe range L2 of horn-like collapsible tube 4 is 35-45mm;The caliber R1 of leading portion straight pipe 3 is 9-10mm;Back segment conical horn shape is received The maximum caliber R2 of the draw 4 is 23-27mm;The length L3 of second pressure inlet 2 is 55-65mm, the front end of the second pressure inlet 2 The pipe end bore R3 for being connected on the rearward end of the first pressure inlet 1 is 11-13mm, and the pipe end bore R4 of rearward end is 14-16mm.
The pressure inlet 2 of first pressure inlet 1 and second described in the utility model is installed in the shell 6 of derusting by sandblasting equipment simultaneously Be wrapped, the heavy caliber pore 5 of the described small-bore end in the front end of the second pressure inlet 2 and the rearward end of the first pressure inlet 1 at a distance of 8- 12mm distances.
The utility model uses the toughened zirconium oxide ceramic of high intensity, using taper structure design and two sections of supercharging technologies, High speed sand grains enters in blast nozzle from derusting by sandblasting equipment high speed, is first pressurized by second segment pressure inlet, subsequently enters the After two sections of pressure inlets are pressurized again, sprayed from straight pipe high-speed straight-line above, due in the direction set of ejection, thus it is caused Sandblasting dynamics is more powerful, and the effect of derusting by sandblasting is more preferable.

Claims (3)

1. composite ceramics blast nozzle, it be by the ceramic material that zirconium oxide and alumina composite form after injection or compression molding Nozzle body is made in sintering in high temperature environments, it is characterised in that described nozzle body connects by preceding first pressure inlet and after The second pressure inlet composition, the first described pressure inlet is integrally formed by leading portion straight pipe and back segment conical horn shape collapsible tube, The second described pressure inlet is that the taper draw for growing section small-angle is formed, the second described pressure inlet front end small-caliber end position In in the heavy caliber pore of the first pressure inlet rearward end or with the heavy caliber pore of the first pressure inlet rearward end at a distance of many 15mm Distance.
2. composite ceramics blast nozzle according to claim 1, it is characterised in that the length of first pressure inlet be 90- 110mm, the pipe range of back segment conical horn shape collapsible tube is 35-45mm;The caliber of leading portion straight pipe is 9-10mm;Back segment taper The maximum caliber of horn-like collapsible tube is 23-27mm;The length of second pressure inlet is 55-65mm, before the second pressure inlet The pipe end bore that end is connected on the first pressure inlet rearward end is 11-13mm, and the pipe end bore of rearward end is 14-16mm.
3. composite ceramics blast nozzle according to claim 1 or 2, it is characterised in that first pressure inlet and the second supercharging Pipe is installed in the shell of derusting by sandblasting equipment and is wrapped, and the second described small-bore end in pressure inlet front end increases with first The heavy caliber pore of pressure pipe rearward end is at a distance of 8-12mm distances.
CN201720788634.7U 2017-07-03 2017-07-03 Composite ceramics blast nozzle Expired - Fee Related CN206883464U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720788634.7U CN206883464U (en) 2017-07-03 2017-07-03 Composite ceramics blast nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720788634.7U CN206883464U (en) 2017-07-03 2017-07-03 Composite ceramics blast nozzle

Publications (1)

Publication Number Publication Date
CN206883464U true CN206883464U (en) 2018-01-16

Family

ID=61298091

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720788634.7U Expired - Fee Related CN206883464U (en) 2017-07-03 2017-07-03 Composite ceramics blast nozzle

Country Status (1)

Country Link
CN (1) CN206883464U (en)

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180116

Termination date: 20190703