CN217494435U - Carbon fiber fixed wing screw is cut edge and is used fixed frock - Google Patents
Carbon fiber fixed wing screw is cut edge and is used fixed frock Download PDFInfo
- Publication number
- CN217494435U CN217494435U CN202221284218.0U CN202221284218U CN217494435U CN 217494435 U CN217494435 U CN 217494435U CN 202221284218 U CN202221284218 U CN 202221284218U CN 217494435 U CN217494435 U CN 217494435U
- Authority
- CN
- China
- Prior art keywords
- placing
- carbon fiber
- fixed
- vacuum suction
- screw
- 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.)
- Active
Links
Images
Landscapes
- Hooks, Suction Cups, And Attachment By Adhesive Means (AREA)
Abstract
The utility model relates to the technical field of unmanned aerial vehicle production, concretely relates to carbon fiber fixed wing screw is cut edge and is used fixed frock, vacuum suction platform including cavity structure, the last breather pipe that is connected with of vacuum suction platform, the last fixing base that can dismantle and be connected with and be used for fixed screw that is connected with of vacuum suction platform, be provided with the portion of placing that is used for placing the screw on the fixing base, the portion of placing includes paddle root portion of placing and two paddle portions of placing, a plurality of air vent one and air vent one run through the fixed seat setting are all seted up on the paddle portion of placing, a plurality of air vent two have been seted up on the side that is connected with the fixing base on the vacuum suction platform; realize when the deckle edge excision of screw, carry out fixed frock.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle produces technical field, concretely relates to carbon fiber fixed wing screw is cut edge and is used fixed frock.
Background
Unmanned aerial vehicle's screw includes paddle root and two paddles, has seted up the motor shaft on the paddle root and has passed the hole, and the screw is made out the back edge through the mould and is had deckle edge to need cut edge and handle, consequently need fix the screw, then cut edge again.
SUMMERY OF THE UTILITY MODEL
The utility model provides a carbon fiber stationary vane screw is cut edge and is used fixed frock when the deckle edge to the screw is amputated, carries out fixed frock.
The technical scheme of the utility model is realized like this: the utility model provides a carbon fiber fixed wing screw is cut edge and is used fixed frock, vacuum platform of breathing in including the cavity structure, the last breather pipe that is connected with of vacuum platform of breathing in, the last fixing base that is used for fixed screw that can dismantle of vacuum platform of breathing in is connected with, be provided with the portion of placing that is used for placing the screw on the fixing base, the portion of placing includes that the paddle root places portion and two paddle portions of placing, a plurality of air vent one and air vent one are all seted up in the paddle portion of placing and are run through the fixed seat setting, a plurality of air vent two has been seted up on the side that is connected with the fixing base on the vacuum platform of breathing in.
The back of the fixed seat is provided with a positioning pin, the side surface of the vacuum air suction platform, which is connected with the fixed seat, is provided with a positioning hole, and the positioning hole is matched with the positioning pin.
The paddle root placing part is provided with a positioning column.
Threaded holes are formed in the placing part and the vacuum suction platform.
The back of the fixing seat is provided with two grooves, and the positions of the two grooves are fixed with the positions of the two paddle placing parts.
The second vent holes are provided with two groups, and each group is located in the corresponding groove.
The technical scheme of the utility model has following positive effect: the utility model discloses a vacuum suction platform and fixing base carry out evacuation fixing to the screw that needs the side cut, are provided with the portion of placing that is used for placing the screw on the fixing base, and the portion of placing includes paddle root portion of placing and paddle portion of placing, is provided with the reference column on the paddle root portion of placing, and the reference column plays the effect of fixed location to the screw; the fixed seat and the vacuum air suction platform are respectively provided with a first vent hole and a second vent hole, and the first vent hole and the second vent hole are both positioned at the groove so as to enable air to pass through; the locating pin is used for locating the fixed seat.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a schematic structural view of the fixing base.
Fig. 3 is a schematic structural view of the fixing base.
Fig. 4 is a schematic structural view of a vacuum suction platform.
Detailed Description
As shown in fig. 1, 2, 3 and 4, the fixing tool for trimming the carbon fiber fixed-wing propeller comprises a vacuum air suction platform 1, wherein an air pipe 6 is connected to the vacuum air suction platform 1, a fixing seat 8 for fixing the propeller 2 is detachably connected to the vacuum air suction platform 1, a placing part 9 for placing the propeller is arranged on the fixing seat 8, the placing part 9 is arranged on one side far away from the vacuum air suction platform 1, the placing part 9 comprises a blade root placing part 3 and a blade placing part 4 which are integrally connected, a plurality of air holes 10 are formed in the blade placing part 4, the air holes 10 penetrate through the fixing seat 8, and a plurality of air holes two 11 are also formed in the side surface, connected with the fixing seat 8, of the vacuum air suction platform 1; specifically, the vent pipe 6 is connected on the vacuum pump, the propeller 20 needing trimming is placed on the placing portion 9, the shape of the propeller is matched with the shape of the placing portion 9, the first vent hole 10 corresponds to the second vent hole 11 in position, the vacuum pump vacuumizes, gas passes through the first vent hole 10 on the blade placing portion 4 and passes through the second vent hole 11, the propeller 20 is adsorbed on the placing portion 9 through vacuum suction, and therefore fixing of the propeller 20 is achieved, and trimming processing is conducted on the propeller 20.
The back of the fixed seat 8 is provided with a positioning pin 12, the side surface of the vacuum air suction platform 1 connected with the fixed seat 8 is provided with a positioning hole 13, and the positioning hole 13 is matched with the positioning pin 12; the fixing base 8 is positioned by the positioning pin 12.
A positioning column 14 is arranged on the blade root placing part 3; the root of the propeller blade of the propeller 20 is provided with a fixing hole, the hole of the propeller needing to be trimmed is just placed on the positioning column 14, and the positioning column 14 plays a role in fixing and positioning.
Threaded holes 15 are formed in the fixed seat 8 and the vacuum suction platform 1; the fixing seat 8 corresponds to the threaded holes 15 in the vacuum air suction platform 1 one to one, the bolt holes 15 are used for installing bolts, and the placing part 9 is fixedly connected with the vacuum air suction platform 1 through the bolts.
The back of the fixed seat 8 is provided with two grooves 16, and the positions of the two grooves 16 correspond to the positions of the two paddle placing parts 4; two groups of vent holes 11 are arranged, and each group is positioned in the corresponding groove 16; the first vent hole 10 and the second vent hole 11 are both positioned in the groove 16, and when vacuum is pumped, gas can enter the first vent hole 10 into the second vent hole 11.
Claims (6)
1. The utility model provides a carbon fiber fixed wing screw is cut edge with fixed frock, includes the vacuum of cavity structure platform (1) of breathing in, its characterized in that: be connected with breather pipe (6) on vacuum suction platform (1), the last fixing base (8) that are used for fixed screw (20) that can dismantle of vacuum suction platform (1), be provided with on fixing base (8) and be used for placing screw portion (9), portion (9) are placed including the paddle root portion of placing (3) and two paddle portion of placing (4), it sets up to all seted up a plurality of air vent (10) and air vent (10) run through fixing base (8) on paddle portion of placing (4), set up a plurality of air vent two (11) on vacuum suction platform (1) on the side that is connected with fixing base (8).
2. The carbon fiber fixed wing propeller fixing tool for trimming is characterized in that: the back of the fixed seat (8) is provided with a positioning pin (12), the side surface of the vacuum suction platform (1) connected with the fixed seat (8) is provided with a positioning hole (13), and the positioning hole (13) is matched with the positioning pin (12).
3. The carbon fiber fixed wing propeller fixing tool for trimming is characterized in that: the blade root placing part (3) is provided with a positioning column (14).
4. The carbon fiber fixed wing propeller fixing tool for trimming is characterized in that: threaded holes (15) are formed in the fixing seat (8) and the vacuum suction platform (1).
5. The carbon fiber fixed wing propeller fixing tool for trimming is characterized in that: the back of the fixed seat (8) is provided with two grooves (16), and the positions of the two grooves (16) are fixed with the positions of the two paddle placing parts (4).
6. The carbon fiber fixed wing propeller fixing tool for trimming is characterized in that: two groups of vent holes (10) are arranged, and each group is located in the corresponding groove (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221284218.0U CN217494435U (en) | 2022-05-26 | 2022-05-26 | Carbon fiber fixed wing screw is cut edge and is used fixed frock |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221284218.0U CN217494435U (en) | 2022-05-26 | 2022-05-26 | Carbon fiber fixed wing screw is cut edge and is used fixed frock |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217494435U true CN217494435U (en) | 2022-09-27 |
Family
ID=83357363
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221284218.0U Active CN217494435U (en) | 2022-05-26 | 2022-05-26 | Carbon fiber fixed wing screw is cut edge and is used fixed frock |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217494435U (en) |
-
2022
- 2022-05-26 CN CN202221284218.0U patent/CN217494435U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11046460B2 (en) | Machine holding fixture for machining composite laminates on a rotor blade | |
| ES8503080A1 (en) | Aerodynamic propeller blade and manufacturing process. | |
| EP2878433A1 (en) | Shrouded rotary assembly from segmented composite for aircraft and method for its manufacture | |
| CN217494435U (en) | Carbon fiber fixed wing screw is cut edge and is used fixed frock | |
| EP2050926A3 (en) | Method for restoring airfoil contour on integrally bladed rotors | |
| CN104093940A (en) | Optimisation of the bearing points of the stilts of vanes in a method for machining said vanes | |
| JP3291167B2 (en) | Method of manufacturing impeller for centrifugal blower having airfoil blade | |
| CN111231183A (en) | Manufacturing die for unmanned aerial vehicle blade | |
| CN102338127A (en) | Impeller assembly machine for multi-blade centrifugal fan | |
| CN211993633U (en) | Pneumatic stable semiconductor wafer cutting device based on magnetic pole pressurization principle | |
| CN211135135U (en) | Punching and edge cutting machine | |
| CN2767723Y (en) | Axial flow fan having hyperboloidal sweepforward blade with knifes on surface | |
| CN207479582U (en) | A kind of intake chamber shaving die | |
| CN112453963A (en) | Helicopter blade bore hole erection equipment | |
| CN211333502U (en) | Double-blade turbine for full-automatic soft material cutting device | |
| CN213195851U (en) | Aluminum alloy ex-trusions concatenation operation is with cutting platform | |
| CN219622934U (en) | Fan casing device based on integral type bearing frame | |
| RU2798639C1 (en) | Method for manufacturing an aircraft engine compressor or fan impeller from a composite material | |
| CN115539427B (en) | Adjustable fish suction pump impeller test device | |
| CN2382652Y (en) | Composite rotary wing of aeroplane | |
| CN211778201U (en) | Motor stator vane and motor | |
| CN213392841U (en) | Combined impeller of centrifugal fan | |
| CN219054616U (en) | Composite foam slitting mechanism | |
| CN214788228U (en) | Combined device for impeller of forward multi-wing centrifugal ventilator | |
| CN220883100U (en) | Light carbon fiber composite missile wing die |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |