CN208730153U - A kind of pressurizing device for aerospace composite material - Google Patents
A kind of pressurizing device for aerospace composite material Download PDFInfo
- Publication number
- CN208730153U CN208730153U CN201821101320.6U CN201821101320U CN208730153U CN 208730153 U CN208730153 U CN 208730153U CN 201821101320 U CN201821101320 U CN 201821101320U CN 208730153 U CN208730153 U CN 208730153U
- Authority
- CN
- China
- Prior art keywords
- pressurized tank
- composite material
- screw rod
- pressurizing device
- push plate
- 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
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 19
- 238000003825 pressing Methods 0.000 claims abstract description 25
- 238000003780 insertion Methods 0.000 claims abstract description 21
- 230000037431 insertion Effects 0.000 claims abstract description 21
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 13
- 238000007789 sealing Methods 0.000 claims abstract description 11
- 230000033228 biological regulation Effects 0.000 claims abstract description 7
- 238000007689 inspection Methods 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 7
- 239000007788 liquid Substances 0.000 abstract description 4
- 239000000463 material Substances 0.000 abstract description 4
- 239000012530 fluid Substances 0.000 abstract description 3
- 150000001875 compounds Chemical class 0.000 abstract 1
- 238000005516 engineering process Methods 0.000 description 10
- 238000000034 method Methods 0.000 description 5
- 229910001018 Cast iron Inorganic materials 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 238000009833 condensation Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 230000005674 electromagnetic induction Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000012466 permeate Substances 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
Landscapes
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
The utility model discloses a kind of pressurizing devices for aerospace composite material, its structure includes electric pressing, bottom panel, pedestal, rectangular item, bracket, left side column, platform, sprue, mobile cap tube, right side column, through-hole, regulation handle, pressurized tank, check cover board, the insertion of electric pressing outer surface is installed in pressurized tank, base upper surface is mutually welded with rectangular lower surface, electric pressing is provided in structure, open motor, motor drives screw rod rotation, the meshing relation of screw rod and movable block moves up movable block, oil liquid in auxiliary cylinder is promoted transfer tube by sealing plate, it enters back into master cylinder, piston rod is pushed to the left, similarly, screw rod band moving gear rotates, saw teeth bars move down, connecting rod pushes push plate, push plate is through piston rod, connecting rod collective effect is compound into intermediate extruding pressurized tank Material is assisted while being pressurizeed using fluid pressure type and motor connection lever, and pressure effect is obvious, convenient and efficient.
Description
Technical field
The utility model is a kind of pressurizing device for aerospace composite material, belongs to aerospace field.
Background technique
Aeronautical technology and space technology are all the modern science and technology of high integrity, they are with basic science and technological sciences
Based on, pooled applications 20th century many engineering technology New TownMovements, mechanics, thermodynamics, materialogy, medicine, electronic technology, from
Dynamic control, jet-propulsion, computer, vacuum technique, cryogenic technique, semiconductor technology, manufacturing technology etc. are all to aerospace
Progress played important function, these science and technology crossing one another and permeate in the application of aerospace, produce
New disciplines make aerospace science and technology form rounded system, the new demand that aerospace constantly proposes, and promote
The progress of these science and technology.
Prior art discloses application No. is: CN201720010686.1 it is a kind of for aerospace composite material plus
Pressure device includes workbench, the first strut, lifter plate, cylinder, upper mold block, lower mold block etc.；Workbench bottom is equipped with cold
But mechanism, bench-top middle part is connected with lower mold block, groove is provided in lower mold block, inner cavity is provided with inside workbench, interior
Chamber is located at the outside of lower mold block, and workbench or so two are provided with through-hole, but the prior art is often pressurizeed using mechanical,
It is lost larger between inner components, and Caton is more obvious in pressure process when internal damage.
Utility model content
In view of the deficienciess of the prior art, the utility model aim be to provide it is a kind of for aerospace composite material
Pressurizing device, it is existing often using mechanical pressurization to solve, it is lost larger between inner components, and pressurizeed when internal damage
The more obvious problem of Caton in journey.
To achieve the goals above, the utility model is achieved through the following technical solutions: a kind of navigate for aviation
The pressurizing device of its composite material, structure include electric pressing, bottom panel, pedestal, rectangular item, bracket, left side column, put down
Platform, mobile cap tube, right side column, through-hole, regulation handle, pressurized tank, checks cover board, the electric pressing appearance at sprue
Face insertion is installed in pressurized tank, and the base upper surface is mutually welded with rectangular lower surface, and the bracket is set under the column of left side
Square, insertion is equipped with sprue on the platform, is connected on the right side of the right side column left side and mobile cap tube, the through-hole runs through
In checking on cover board, the electric pressing includes shell, pressurized tank, pressing plate, push plate, piston rod, master cylinder, transfer tube, auxiliary
Cylinder, sealing plate, movable block, screw rod, motor, gear, saw teeth bars, connecting rod, guide rail, the shell inner surface insertion, which is equipped with, to be led
Rail, the pressing plate are located at pressurized tank two sides, and the right surface of pressing plate is mutually welded with push plate left surface, and the piston rod and push plate are cut with scissors
Chain link, the piston rod outer surface insertion are installed in master cylinder, and the transfer tube bottom end is connected with auxiliary cylinder top, described close
The insertion of sealing plate outer surface is installed in auxiliary cylinder, and the movable block is meshed with screw rod, and the screw rod bottom end insertion is installed on motor
On, the gear is meshed with saw teeth bars, and the connecting rod is connect with saw teeth bars hinge, and the mobile cap tube is located in pressurized tank
Side.
Further, the bottom panel bottom surface fits with base top surface.
Further, it is connected on the right side of the left side column on the left of mobile cap tube.
Further, the regulation handle bottom surface insertion is installed in pressurized tank.
Further, the bottom panel is rectangular parallelepiped structure.
Further, the pedestal is made of cast iron, has the advantages that hardness is big.
Further, the rectangular item shares 2.
Beneficial effect
A kind of pressurizing device for aerospace composite material of the utility model is provided with electric pressuring in structure and fills
It sets, opens motor, motor drives screw rod to rotate, and the meshing relation of screw rod and movable block moves up movable block, and sealing plate will
Oil liquid in auxiliary cylinder promotes transfer tube, enters back into master cylinder, pushes piston rod to the left, and similarly, screw rod band moving gear rotates, saw
Ratch moves down, and connecting rod pushes push plate, composite wood of the push plate through piston rod, connecting rod collective effect into intermediate extruding pressurized tank
Material is assisted while being pressurizeed using fluid pressure type and motor connection lever, and pressure effect is obvious, convenient and efficient.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon:
Fig. 1 is a kind of structural schematic diagram of the pressurizing device for aerospace composite material of the utility model；
Fig. 2 is the structural schematic diagram of the utility model electric pressing.
In figure: electric pressing -1, bottom panel -2, pedestal -3, rectangular item -4, bracket -5, left side column -6, platform -7,
Sprue -8, right side column -10, through-hole -11, regulation handle -12, pressurized tank -13, checks cover board -14, shell-at mobile cap tube -9
101, pressurized tank -102, pressing plate -103, push plate -104, piston rod -105, master cylinder -106, transfer tube -107, auxiliary cylinder -108, sealing
Plate -109, movable block -110, screw rod -111, motor -112, gear -113, saw teeth bars -114, connecting rod -115, guide rail -116.
Specific embodiment
To be easy to understand the technical means, creative features, achievement of purpose, and effectiveness of the utility model, below
In conjunction with specific embodiment, the utility model is further described.
Fig. 1, Fig. 2 are please referred to, the utility model provides a kind of pressurizing device technical side for aerospace composite material
Case: its structure include electric pressing 1, bottom panel 2, pedestal 3, rectangular item 4, bracket 5, left side column 6, platform 7, sprue 8,
Mobile cap tube 9, through-hole 11, regulation handle 12, pressurized tank 13, checks cover board 14 at right side column 10, outside the electric pressing 1
Surface insertion is installed in pressurized tank 13, and 3 upper surface of pedestal is mutually welded with rectangular 4 lower surface of item, and the bracket 5 is set to a left side
Below lateral column 6, insertion is equipped with sprue 8 on the platform 7, is connected on the right side of 10 left side of right side column and mobile cap tube 9,
The through-hole 11 through check cover board 14 on, the electric pressing 1 include shell 101, pressurized tank 102, pressing plate 103,
Push plate 104, piston rod 105, master cylinder 106, transfer tube 107, auxiliary cylinder 108, sealing plate 109, movable block 110, screw rod 111, motor
112, gear 113, saw teeth bars 114, connecting rod 115, guide rail 116,101 inner surface of the shell insertion is equipped with guide rail 116, described
Pressing plate 103 is located at 102 two sides of pressurized tank, and the right surface of the pressing plate 103 is mutually welded with 104 left surface of push plate, the piston rod 105
Connect with 104 hinge of push plate, 105 outer surface of piston rod insertion is installed in master cylinder 106,107 bottom end of transfer tube with
Auxiliary 108 top of cylinder is connected, and 109 outer surface of the sealing plate insertion is installed in auxiliary cylinder 108, the movable block 110 and screw rod
111 are meshed, and 111 bottom end of the screw rod insertion is installed on motor 112, and the gear 113 is meshed with saw teeth bars 114, institute
Connecting rod 115 is stated to connect with 114 hinge of saw teeth bars, the mobile cap tube 9 is located at the top of pressurized tank 102,2 bottom surface of bottom panel with
3 top surface of pedestal fits, and is connected on the left of 6 right side of left side column and mobile cap tube 9,12 bottom surface of the regulation handle insertion peace
Loaded in pressurized tank 13, the bottom panel 2 is rectangular parallelepiped structure, and the pedestal 3 is made of cast iron, has the advantages that hardness is big,
The rectangular item 4 shares 2.
Motor 112 described in this patent refers to a kind of electromagnetism that electric energy conversion or transmitting are realized according to the law of electromagnetic induction
Device, motor are indicated with letter M in circuit, its main function is to generate driving torque, as electrical appliance or various machines
The power source of tool, model Y80M2-2 have the advantages that light-weight, revolving speed is high；The guide rail 116 is metal or other materials
Manufactured slot or ridge can bear, fix, guiding mobile device or equipment and reducing a kind of device of its friction, in guide rail surface
Longitudinal slot or ridge, for guiding, stationary machines component, special equipment, instrument etc., guide rail is also known as sliding rail, linear guides, linear
Sliding rail is used for straight reciprocating motion occasion, possesses nominal load more higher than linear bearing, while can undertake certain torsion
Square can realize high-precision linear motion in high-load situations, this.
For example, it is multiple to inject aerospace from sprue 8 when old engineer carries out compression forming to aerospace composite material
Mobile cap tube 9 is moved to 7 position of center line of platform by condensation material, is moved cap tube 9 at this time and is blocked 102 top of pressurized tank, opens
Motor 112, motor 112 drive screw rod 111 to rotate, and the meshing relation of screw rod 111 and movable block 110 makes movable block 110 to moving up
Dynamic, the oil liquid in auxiliary cylinder 108 is promoted transfer tube 107 by sealing plate 109, is entered back into master cylinder 106, is pushed piston rod to the left
105, similarly, screw rod 111 is rotated with moving gear 113, and saw teeth bars 114 move down, and connecting rod 115 pushes push plate 104, push plate 104
Composite material through piston rod 105, from 115 collective effect of connecting rod to intermediate extruding pressurized tank 102.
The utility model solves often using mechanical pressurization, be lost between inner components it is larger, and when internal damage
The more obvious problem of Caton in pressure process, the utility model are combined with each other by above-mentioned component, are provided in structure
Electric pressing, opens motor, and motor drives screw rod rotation, and the meshing relation of screw rod and movable block makes movable block to moving up
Dynamic, the oil liquid in auxiliary cylinder is promoted transfer tube by sealing plate, is entered back into master cylinder, is pushed piston rod to the left, and similarly, screw rod drives
Gear rotation, saw teeth bars move down, and connecting rod pushes push plate, and push plate squeezes pressurization to centre through piston rod, connecting rod collective effect
Composite material in slot is assisted while being pressurizeed using fluid pressure type and motor connection lever, and pressure effect is obvious, convenient and efficient.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above, for
For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this
In the case where the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent elements of the claims
All changes are embraced therein.It should not treat any reference in the claims as limiting related right
It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (5)
1. a kind of pressurizing device for aerospace composite material, it is characterised in that: its structure includes electric pressing
(1), bottom panel (2), pedestal (3), rectangular item (4), bracket (5), left side column (6), platform (7), sprue (8), mobile cap tube
(9), right side column (10), through-hole (11), regulation handle (12), pressurized tank (13), inspection cover board (14), the electric pressing
(1) outer surface insertion is installed in pressurized tank (13), and pedestal (3) upper surface is mutually welded with rectangular item (4) lower surface, described
Bracket (5) is set to below left side column (6), is embedded in and is equipped with sprue (8) on the platform (7), on the left of the right side column (10)
It is connected on the right side of mobile cap tube (9), the through-hole (11) is through checking on cover board (14), the electric pressing (1)
Including shell (101), pressurized tank (102), pressing plate (103), push plate (104), piston rod (105), master cylinder (106), transfer tube
(107), auxiliary cylinder (108), sealing plate (109), movable block (110), screw rod (111), motor (112), gear (113), saw teeth bars
(114), connecting rod (115), guide rail (116), shell (101) the inner surface insertion are equipped with guide rail (116), the pressing plate
(103) it is located at pressurized tank (102) two sides, the right surface of the pressing plate (103) is mutually welded with push plate (104) left surface, the piston
Bar (105) is connect with push plate (104) hinge, and piston rod (105) the outer surface insertion is installed in master cylinder (106), the biography
Defeated pipe (107) bottom end is connected with auxiliary cylinder (108) top, and sealing plate (109) the outer surface insertion is installed on auxiliary cylinder (108)
Interior, the movable block (110) is meshed with screw rod (111), and screw rod (111) the bottom end insertion is installed on motor (112), institute
It states gear (113) to be meshed with saw teeth bars (114), the connecting rod (115) connect with saw teeth bars (114) hinge, the mobile lid
Cylinder (9) is located above pressurized tank (102).
2. a kind of pressurizing device for aerospace composite material according to claim 1, it is characterised in that: the bottom
Panel (2) bottom surface fits with pedestal (3) top surface.
3. a kind of pressurizing device for aerospace composite material according to claim 1, it is characterised in that: the left side
It is connected on the right side of lateral column (6) on the left of mobile cap tube (9).
4. a kind of pressurizing device for aerospace composite material according to claim 1, it is characterised in that: the tune
The insertion of section handle (12) bottom surface is installed on pressurized tank (13).
5. a kind of pressurizing device for aerospace composite material according to claim 1, it is characterised in that: the side
Shape item (4) is rectangular parallelepiped structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821101320.6U CN208730153U (en) | 2018-07-11 | 2018-07-11 | A kind of pressurizing device for aerospace composite material |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821101320.6U CN208730153U (en) | 2018-07-11 | 2018-07-11 | A kind of pressurizing device for aerospace composite material |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208730153U true CN208730153U (en) | 2019-04-12 |
Family
ID=66025424
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821101320.6U Expired - Fee Related CN208730153U (en) | 2018-07-11 | 2018-07-11 | A kind of pressurizing device for aerospace composite material |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208730153U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112474185A (en) * | 2020-12-09 | 2021-03-12 | 杭州皓淡机电设备有限公司 | Quantitative oil coating auxiliary device of wiper switch assembly |
| CN112729763A (en) * | 2021-04-06 | 2021-04-30 | 中国空气动力研究与发展中心高速空气动力研究所 | Symmetric pasting quantitative pressurizing device for wind tunnel balance |
-
2018
- 2018-07-11 CN CN201821101320.6U patent/CN208730153U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112474185A (en) * | 2020-12-09 | 2021-03-12 | 杭州皓淡机电设备有限公司 | Quantitative oil coating auxiliary device of wiper switch assembly |
| CN112474185B (en) * | 2020-12-09 | 2022-07-15 | 杭州皓淡机电设备有限公司 | Quantitative oil coating auxiliary device of wiper switch assembly |
| CN112729763A (en) * | 2021-04-06 | 2021-04-30 | 中国空气动力研究与发展中心高速空气动力研究所 | Symmetric pasting quantitative pressurizing device for wind tunnel balance |
| CN112729763B (en) * | 2021-04-06 | 2021-06-22 | 中国空气动力研究与发展中心高速空气动力研究所 | Symmetric pasting quantitative pressurizing device for wind tunnel balance |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN208730153U (en) | A kind of pressurizing device for aerospace composite material | |
| WO2015085648A1 (en) | Inner-circulation high-speed hydraulic system, hydraulic platform, and hydraulic platform assembly | |
| CN107009380A (en) | A kind of caliper brake manipulator | |
| CN203889707U (en) | Cotton tape elastic tensioning device for corrugated paper production line | |
| CN110280631A (en) | Mechanical full electric servo numerical control bender based on multiple degrees of freedom coupling driving | |
| CN209035989U (en) | A kind of mechanical-hydraulic combination slide unit | |
| CN104439012B (en) | The die filling height adjustment device of MP hotdie forging press | |
| CN105163516B (en) | A kind of process equipment of structure improved lift circuit plate | |
| CN203481991U (en) | Planetary roller screw electric cylinder | |
| CN100551662C (en) | Combined tyre vulcanizing machine | |
| CN205080830U (en) | Mechanical press operating mechanism physical simulation experimental apparatus | |
| CN202240568U (en) | Hydraulic control mechanical type compressing device | |
| CN104952349B (en) | A kind of mechanical press operating mechanism physical simulation experiment device | |
| CN205887763U (en) | Quick fashioned stamping device | |
| CN204430070U (en) | A kind of bar cutting bends dual-purpose machine | |
| CN104154204B (en) | A kind of oil pressure promotes device | |
| CN209424839U (en) | A kind of vertical structure increasing journey side ejection device | |
| CN103203609A (en) | Miniature press | |
| CN203265355U (en) | Worm gear pressurizing type punch press | |
| CN207172805U (en) | A kind of compact mechanical driver of press with guide pillar | |
| CN208301843U (en) | Operating table bed board mobile mechanism | |
| CN201625696U (en) | Novel oil press for right-angle pipe clamps | |
| CN203979321U (en) | A kind of oil pressure pushing device | |
| CN212367045U (en) | Long-stroke high-thrust servo electric mechanism | |
| CN218401023U (en) | Sliding opening device for large-scale component tool frame |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190412 Termination date: 20190711 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |