CN107899029A - Fibrous composite super-pressure inactivates nacelle - Google Patents
Fibrous composite super-pressure inactivates nacelle Download PDFInfo
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- CN107899029A CN107899029A CN201711390892.0A CN201711390892A CN107899029A CN 107899029 A CN107899029 A CN 107899029A CN 201711390892 A CN201711390892 A CN 201711390892A CN 107899029 A CN107899029 A CN 107899029A
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- Prior art keywords
- inactivation
- cabin body
- tube rolling
- fibrous composite
- pressure
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- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61L—METHODS OR APPARATUS FOR STERILISING MATERIALS OR OBJECTS IN GENERAL; DISINFECTION, STERILISATION OR DEODORISATION OF AIR; CHEMICAL ASPECTS OF BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES; MATERIALS FOR BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES
- A61L2/00—Methods or apparatus for disinfecting or sterilising materials or objects other than foodstuffs or contact lenses; Accessories therefor
- A61L2/02—Methods or apparatus for disinfecting or sterilising materials or objects other than foodstuffs or contact lenses; Accessories therefor using physical phenomena
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61L—METHODS OR APPARATUS FOR STERILISING MATERIALS OR OBJECTS IN GENERAL; DISINFECTION, STERILISATION OR DEODORISATION OF AIR; CHEMICAL ASPECTS OF BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES; MATERIALS FOR BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES
- A61L2/00—Methods or apparatus for disinfecting or sterilising materials or objects other than foodstuffs or contact lenses; Accessories therefor
- A61L2/26—Accessories or devices or components used for biocidal treatment
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61L—METHODS OR APPARATUS FOR STERILISING MATERIALS OR OBJECTS IN GENERAL; DISINFECTION, STERILISATION OR DEODORISATION OF AIR; CHEMICAL ASPECTS OF BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES; MATERIALS FOR BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES
- A61L2202/00—Aspects relating to methods or apparatus for disinfecting or sterilising materials or objects
- A61L2202/10—Apparatus features
- A61L2202/12—Apparatus for isolating biocidal substances from the environment
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- Health & Medical Sciences (AREA)
- Epidemiology (AREA)
- Life Sciences & Earth Sciences (AREA)
- Animal Behavior & Ethology (AREA)
- General Health & Medical Sciences (AREA)
- Public Health (AREA)
- Veterinary Medicine (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
The present invention provides the fibrous composite super-pressure inactivation nacelle that a kind of intensity is high, light-weight, including inactivation cabin body, inactivation cabin body interior set cylinder to be known as the blind hole for inactivating chamber；Inactivate cabin body peripheral winding fibrous composite.Cabin body peripheral winding fibrous composite is inactivated, is winding fabric composite material, winding fabric belt composite or winding fibre bundle composite material.Cabin body outer surface is inactivated as cylinder.Inactivation cabin body is cold tube rolling, and bottom plug is fixed in one end of cold tube rolling, forms inactivation cabin body of the outer surface for cylinder.Cabin body longitudinal section outer contour is inactivated in I-shaped.Inactivation cabin body includes cold tube rolling, and bottom plug is fixed in one end of cold tube rolling, and the both ends fixed flange of cold tube rolling, it is in I-shaped inactivation cabin body to form longitudinal section outer contour.Wound using fibrous composite and inactivate cabin body, fibrous composite light weight, small, easily movement under equality strength.
Description
Technical field
The invention belongs to field of medical device, and in particular to a kind of fibrous composite super-pressure inactivates nacelle.
Background technology
Ultra-high pressure sterilization inactivation technology, also known as superhigh pressure technique, high static pressure technology, refer to and are placed in the article with inactivation
The technology that processing sterilizes for a period of time under the high pressure of 100-1000MPa and certain temperature.Superhigh pressure technique needs to coordinate super
High-pressure installation could use, and ultra-high pressure apparatus includes ultrahigh pressure vessel and pressue device.Super-pressure inactivation cabin is superelevation pressure-volume
Device.Super-pressure inactivation cabin needs to bear super-pressure, ensures security, there is very high requirement to its structure.Integration superelevation at present
The structure of pressure inactivation nacelle is mostly cylindrical shape, the inactivation chamber for setting cylinder blind hole to form in it.Super-pressure inactivates the inactivation of nacelle
Chamber one end opening connection plunger rod, plunger rod can left and right or move up and down.Wherein, the superelevation of indirect weighting, that is, split type
The inactivation chamber other end of the super-pressure inactivation nacelle of pressure inactivation equipment also connects highly pressurised liquid manhole appendix, highly pressurised liquid manhole appendix with
Capstan is connected.In order to bear pressure, gusset, upper surface, the lower face wall thickness of super-pressure inactivation nacelle are very big, and entirely
Nacelle is made of steel construction, and weight is very heavy, and movement is very inconvenient.
The content of the invention
The object of the present invention is to provide a kind of high, the light-weight fibrous composite super-pressure of intensity to inactivate nacelle.
The present invention seeks to what is realized in the following manner：A kind of fibrous composite super-pressure inactivates nacelle, including inactivation
Cabin body, inactivation cabin body interior set cylinder to be known as the blind hole for inactivating chamber；Inactivate cabin body peripheral winding fiber composite material
Material.
Cabin body peripheral winding fibrous composite is inactivated, is winding fabric composite material, winding fabric band
Composite material or winding fibre bundle composite material.
Cabin body outer surface is inactivated as cylinder.
Inactivation cabin body is cold tube rolling, and bottom plug is fixed in one end of cold tube rolling, and it is cylindrical to form outer surface
Inactivate cabin body.
Cabin body longitudinal section outer contour is inactivated in I-shaped.
Inactivation cabin body includes cold tube rolling, and bottom plug is fixed in one end of cold tube rolling, and the both ends of cold tube rolling are fixed
Ring flange, it is in I-shaped inactivation cabin body to form longitudinal section outer contour.
Winding fabric composite material is to wrap up in volume cold with axial closely coated with wide fiber prepreg material of cold tube rolling
Steel rolling tube outer surface；Winding fabric belt composite or winding fibre bundle composite material refer to fiber prepreg material circumferential direction and twine
Around or be spirally wound on cold tube rolling outer surface.
The highly pressurised liquid manhole appendix connected with inactivation chamber is set on bottom plug..
The beneficial effects of the invention are as follows：Wound using fibrous composite and inactivate cabin body, fiber composite under equality strength
Quality of materials is light, small, easily mobile.Cold tube rolling can be used under this structure, and as inactivation cabin body, cost is low, fits
Close and produce in enormous quantities.
Brief description of the drawings
Fig. 1 is the embodiment of the present application one.Fig. 2 is the embodiment of the present application two.Fig. 3 is the embodiment of the present application three.Fig. 4 is this Shen
Please example IV.Fig. 5 is the embodiment of the present application five.Fig. 6 is the embodiment of the present application six.Fig. 7 is circumferential winding schematic diagram.Fig. 8 is
Spiral winding schematic diagram.Fig. 9 is the embodiment of the present application seven.Figure 10 is the embodiment of the present application eight.Figure 11 is the embodiment of the present application nine.
Figure 12 is the embodiment of the present application ten.Figure 13 is winding fabric composite material schematic diagram.
Wherein, 1 is inactivation cabin body, and 2 be inactivation chamber, and 3 be fibrous composite, and 4 be cold tube rolling, and 5 be bottom plug,
6 be ring flange, and 7 be highly pressurised liquid manhole appendix, and 8 be fiber prepreg material.
Embodiment
As shown in figures 1-13, a kind of fibrous composite super-pressure inactivation nacelle, including inactivation cabin body 1, inactivate cabin sheet
The inside of body 1 sets cylinder to be known as the blind hole for inactivating chamber 2.Inactivate 1 periphery of cabin body winding fibrous composite 3.Inactivate cabin sheet
1 periphery of body winds fibrous composite, is winding fabric composite material, winding fabric belt composite or winding
Fibre bundle composite material.Fiber is carbon fiber, glass fibre, aramid fiber or good compound of other light weights, stress performance
Material.Carbon fiber, glass fiber quality are light.Tensile strength is high, and processability is good, can make the product of different shape.
As shown in Fig. 1-3 and 9,1 outer surface of inactivation cabin body is four kinds of cylindrical embodiments.Fig. 1 is embodiment one, is gone out
Body 1 outer surface in cabin living is cylinder, and setting blind hole is inactivation chamber 2 in it.It is overall cylinder steel core to inactivate cabin body 1, overall
Cylindrical steel core inner directly bores blind hole and forms inactivation chamber 2.Overall cylinder steel core periphery winds fibrous composite 3.Embodiment
In two, as shown in Fig. 2, whole stainless steel structure systems before 1 its thickness ratio of inactivation cabin body of outside winding fibrous composite
Inactivation cabin 1 thickness of body of work is thin very much, can be made using cold tube rolling 4.In order to cost-effective, inactivation cabin body 1 can be with
For cold tube rolling 4, bottom plug 5 is fixed in one end of cold tube rolling 4, forms inactivation cabin body 1 of the outer surface for cylinder.Cold rolling
Bottom plug 5 is fixed in one end of steel pipe 4, is that one end internal thread of cold tube rolling 4 fixes the one of bottom plug 5 or cold tube rolling
End welding bottom plug 5.4 performance of cold tube rolling is good, it is cheap, suitable for producing in enormous quantities.The winding of 4 periphery of cold tube rolling is fine
Tie up composite material 3.Fig. 3 is embodiment three, is on bottom plug 5 that setting connects with inactivation chamber 2 with the difference of embodiment two
Logical high pressure paddle hole 7.This structure is suitable for the super-pressure inactivation equipment of indirect weighting.Fig. 9 is embodiment seven, with Fig. 1
The difference of embodiment one is：The bottom of inactivation cabin body 1 sets a high pressure paddle hole 7 connected with 2 chambers of inactivation,
It is adapted to split type super-pressure inactivation equipment.
As shown in Fig. 4-6,10-12, inactivation 1 longitudinal section outer contour of cabin body is in six kinds of I-shaped embodiments.Fig. 4 is real
Example four is applied, 1 longitudinal section outer contour of inactivation cabin body is in I-shaped, its interior inactivation chamber 2 set in blind hole.Inactivating cabin body 1 is
Longitudinal section outer contour is in I-shaped overall steel core, and in-between position diameter winds fibrous composite 3 compared with small column periphery.With
It is in I-shaped overall steel core that the steel column of cylinder, which is first processed into longitudinal section outer contour, and then blind hole is used as inactivation chamber 2 at boring.Figure
In 5, in embodiment five, inactivation cabin body 1 includes cold tube rolling 4, and bottom plug 5, cold tube rolling are fixed in one end of cold tube rolling 4
Both ends fixed flange 6, form longitudinal section outer contour be in I-shaped inactivation cabin body 1, blocked up using cold tube rolling 4, bottom
First 5, ring flange 6 can effectively reduce cost.Bottom plug 5 is fixed in one end of cold tube rolling 4, is one end of cold tube rolling 4
Internal thread fixes one end welding bottom plug 5 of bottom plug 5 or cold tube rolling 4.The both ends fixed flange of cold tube rolling 4
6, refer to the both ends of the surface of cold tube rolling 4 and welded with the bottom surface of ring flange 6.
In Fig. 6, embodiment six and the difference of embodiment 5 are：Set what is connected with inactivation chamber 2 on bottom plug 5
High pressure paddle hole 7.This structure is suitable for the split type super-pressure inactivation equipment of indirect weighting.Figure 10 is embodiment eight, with
Example IV difference is that the bottom for inactivating cabin body 1 sets a high pressure paddle hole 7 connected with inactivation chamber 2, fits
Equipment should be inactivated in split type super-pressure.When 1 longitudinal section outer contour of inactivation cabin body is in I-shaped, the two of inactivation cabin body 1
End radius is more than middle radius, and fibrous composite 3 is wrapped in the inactivation less cylindrical outer surface of 1 radius of cabin body.Figure 11 is
Embodiment nine, is with the difference of embodiment five：The outer circumference surface at the both ends of cold tube rolling 4 is welded with 6 inner surface of ring flange
Connect or be threadedly coupled, such ring flange 6 makes the intensity higher of inactivation cabin body 1 equivalent to reinforcing rib.Figure 12 is embodiment
Ten, it is to set the high pressure paddle hole 7 connected with inactivation chamber 2 on bottom plug 5 with the difference of embodiment nine.This knot
Structure is suitable for the split type super-pressure inactivation equipment of indirect weighting.
3 outer surface of fibrous composite of all embodiments can protect fibrous composite 3 with covering shell, shell
Structure, avoid damage to dust etc., appearance can also be made more good-looking.Shell can be plastics or stainless steel.Inactivate cabin
When 1 longitudinal section outer contour of body is in I-shaped, outer surface and 1 both ends of inactivation cabin body of the shell outside its fibrous composite 3
Cylindrical outer surface it is concordant.
As shown in Fig. 7,8,13, winding fabric composite material is and cold tube rolling 4（Embodiment two, three, five, six,
9th, ten）Axial same wide or overall cylinder steel core（Embodiment one, seven）It is axial to be subtracted with wide or 4 axial width of cold tube rolling
Ring flange 6 width in both ends is the same as wide（Embodiment ten）Or longitudinal section is I-shaped overall steel core mid diameter smaller portions cylinder
It is axial with wide（Example IV, eight）Fiber prepreg material 8 closely cladding wrap up in volume in cold tube rolling 4 or overall cylinder steel core or
The outer surface of person's entirety steel core.Winding fabric belt composite or winding fibre bundle composite material refer to fiber prepreg material
8 circumferential windings or the outer surface for being spirally wound on the corresponding band winding component of each embodiment.Close cladding, which is wrapped up in volume and referred to, is wrapping
Cover the tension force increased when wrapping up in volume.Fig. 7 is the circumferential winding schematic diagram of fiber prepreg material 8.Circumferential direction winding：Component to be wound is around itself
Axis rotates, and conductive filament head does parallel and axis movement in the winding section of component to be wound.Winding angle is usually 85 to 90
Degree.Component to be wound circles certainly, the width of the approximate mobile fiber prepreg material 8 of conductive filament head.Fig. 8 is 8 spiral shell of fiber prepreg material
Rotation winds block diagram to be wound.Spiral winding：Optimal winding angle is determined according to experiment, makes fibrous composite 3 uniform
And more pressure can be born.Component to be wound is rotated around own axes, and conductive filament head is done in the winding section of component to be wound
The parallel and reciprocating motion of axis.Figure 13 is winding fabric composite material schematic diagram, and fiber prepreg material 8 is wrapped in from level to level
Member outer surface to be wound.
When it is implemented, closing plunger rod, make super-pressure inactivation nacelle closure, inactivated to super-pressure in nacelle and inject high pressure
Liquid.Or directly inactivated in cabin and pressurizeed to super-pressure using plunger rod, super-pressure inactivates nacelle by high pressure.The fibre of equal quality
Dimension composite material and steel construction, its tensile strength of fibrous composite such as carbon fiber and glass fibre are far above steel construction.Superelevation
When pressure inactivation nacelle is pressurized, fibrous composite 3 such as carbon fiber and glass fibre are by pulling force, its light weight and existing good power
Learn performance.When needing mobile super-pressure inactivation nacelle, because its lighter weight, also more convenient.
Claims (8)
1. a kind of fibrous composite super-pressure inactivates nacelle, including inactivation cabin body, inactivation cabin body interior sets cylinder
Referred to as inactivate the blind hole of chamber；It is characterized in that：The inactivation cabin body peripheral winding fibrous composite.
2. fibrous composite super-pressure inactivation nacelle according to claim 1, it is characterised in that：The inactivation cabin sheet is external
Week winding fibrous composite, is winding fabric composite material, winding fabric belt composite or winding fiber
Tow composite material.
3. fibrous composite super-pressure inactivation cabin according to claim 2, it is characterised in that：The inactivation cabin body appearance
Face is cylinder.
4. fibrous composite super-pressure inactivation nacelle according to claim 3, it is characterised in that：It is described inactivation cabin body be
Bottom plug is fixed in cold tube rolling, one end of cold tube rolling, forms inactivation cabin body of the outer surface for cylinder.
5. fibrous composite super-pressure inactivation nacelle according to claim 2, it is characterised in that：The inactivation cabin body is indulged
Section outer contour is in I-shaped.
6. fibrous composite super-pressure inactivation nacelle according to claim 5, it is characterised in that：The inactivation cabin body bag
Cold tube rolling is included, bottom plug is fixed in one end of cold tube rolling, and the both ends fixed flange of cold tube rolling, forms longitudinal section foreign steamer
Exterior feature is in I-shaped inactivation cabin body.
7. nacelle is inactivated according to the fibrous composite super-pressure of claim 4 or 6, it is characterised in that：The winding fiber
Fabric composites is to wrap up in volume in cold tube rolling outer surface with axial closely coated with wide fiber prepreg material of cold tube rolling；It is described
Winding fabric belt composite either wind fibre bundle composite material and refers to that fiber prepreg material is circumferential to be wound or spiral twine
It is wound on cold tube rolling outer surface.
8. nacelle is inactivated according to the fibrous composite super-pressure of claim 4 or 6, it is characterised in that：The bottom plug
The highly pressurised liquid manhole appendix that upper setting is connected with inactivation chamber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711390892.0A CN107899029A (en) | 2017-12-21 | 2017-12-21 | Fibrous composite super-pressure inactivates nacelle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711390892.0A CN107899029A (en) | 2017-12-21 | 2017-12-21 | Fibrous composite super-pressure inactivates nacelle |
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| Publication Number | Publication Date |
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| CN107899029A true CN107899029A (en) | 2018-04-13 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711390892.0A Pending CN107899029A (en) | 2017-12-21 | 2017-12-21 | Fibrous composite super-pressure inactivates nacelle |
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Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1614266A (en) * | 2003-11-03 | 2005-05-11 | 唯赛勃环保材料制造(上海)有限公司 | Fibreglass winded pressure container and machining method thereof |
| CN200968491Y (en) * | 2006-11-27 | 2007-10-31 | 赵士龙 | Annular pressure vessels |
| CN106151161A (en) * | 2016-06-20 | 2016-11-23 | 浙江大学 | A kind of detachable hydraulic cylinder using carbon fibre composite to couple and carry |
| CN205814714U (en) * | 2016-05-21 | 2016-12-21 | 郑州飞龙医疗设备有限公司 | The supertension inactivation equipment of pathogen in liquid bio goods |
-
2017
- 2017-12-21 CN CN201711390892.0A patent/CN107899029A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1614266A (en) * | 2003-11-03 | 2005-05-11 | 唯赛勃环保材料制造(上海)有限公司 | Fibreglass winded pressure container and machining method thereof |
| CN200968491Y (en) * | 2006-11-27 | 2007-10-31 | 赵士龙 | Annular pressure vessels |
| CN205814714U (en) * | 2016-05-21 | 2016-12-21 | 郑州飞龙医疗设备有限公司 | The supertension inactivation equipment of pathogen in liquid bio goods |
| CN106151161A (en) * | 2016-06-20 | 2016-11-23 | 浙江大学 | A kind of detachable hydraulic cylinder using carbon fibre composite to couple and carry |
Non-Patent Citations (1)
| Title |
|---|
| 纵伟主编: "《食品工业新技术》", 30 April 2006, 哈尔滨：东北林业大学出版社 * |
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Application publication date: 20180413 |
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| RJ01 | Rejection of invention patent application after publication |