CN107175785A - A kind of composite propeller curing oven of built-in rotating mechanism - Google Patents
A kind of composite propeller curing oven of built-in rotating mechanism Download PDFInfo
- Publication number
- CN107175785A CN107175785A CN201710630657.XA CN201710630657A CN107175785A CN 107175785 A CN107175785 A CN 107175785A CN 201710630657 A CN201710630657 A CN 201710630657A CN 107175785 A CN107175785 A CN 107175785A
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- China
- Prior art keywords
- rotating
- support bar
- support
- pole
- built
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- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
- B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
- B29C35/04—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould using liquids, gas or steam
- B29C35/045—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould using liquids, gas or steam using gas or flames
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
- B29L2031/087—Propellers
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- Physics & Mathematics (AREA)
- Health & Medical Sciences (AREA)
- Oral & Maxillofacial Surgery (AREA)
- Thermal Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Heating, Cooling, Or Curing Plastics Or The Like In General (AREA)
Abstract
The present invention proposes a kind of composite propeller curing oven of built-in rotating mechanism, including body of heater, rotating mechanism, multiple mould placing racks and drive mechanism, rotating mechanism includes the first rotating ring, second rotating ring, multiple connecting shafts, rotating shaft, first rotating ring, second rotating ring is positioned opposite, rotating shaft first end is rotated with body of heater the first side wall and is connected, the end of rotating shaft second sequentially passes through the first rotating ring, the geometric center of second rotating ring is rotated with body of heater second sidewall and is connected, multiple connecting shaft first ends are connected with the first rotating ring and the end of multiple connecting shafts second is connected with the second rotating ring；Multiple mould placing racks are hinged with multiple connecting shafts respectively；Drive mechanism is connected with rotating shaft and drive shaft is rotated.Curing oven of the present invention reaches that the upper and lower mould temperature difference is at ± 1 DEG C or so in stove by using the mode of built-in rotating mechanism and hot air circulating system, meets requirement of the composite propeller to temperature in forming process.
Description
Technical field
The present invention relates to a kind of curing oven, more particularly to a kind of composite propeller curing oven of built-in rotating mechanism.
Background technology
At present, composite propeller curing oven is used and deposited inside fixed non-rotatable form, this curing oven mostly
The upper and lower, left and right temperature difference is larger in the larger temperature difference, stove, is especially put into after propeller mould, the upper and lower mould of mould have the temperature difference and
Temperature Difference Ratio is larger, has a strong impact on the quality of composite propeller.
The content of the invention
Based on technical problem present in background technology, the present invention proposes a kind of composite spiral shell of built-in rotating mechanism
Revolve oar curing oven.
A kind of composite propeller curing oven of built-in rotating mechanism proposed by the present invention, including body of heater, rotating mechanism,
Multiple mould placing racks and drive mechanism, wherein：Rotating mechanism is arranged in body of heater, and rotating mechanism includes the first rotating ring, the
Two rotating rings, multiple connecting shafts, rotating shaft, the first rotating ring, the second rotating ring are positioned opposite, rotating shaft first end and the side of body of heater first
Wall rotates connection, and the end of rotating shaft second sequentially passes through the first rotating ring, the geometric center of the second rotating ring and body of heater second sidewall and turned
It is fixedly connected on the inside of dynamic connection, the first rotating ring by multiple head rods with rotating shaft, by multiple on the inside of the second rotating ring
Second connecting rod is fixedly connected with rotating shaft, and multiple connecting shafts are arranged between the first rotating ring and the second rotating ring in parallel to each other
And be circumferentially distributed centered on rotating shaft, multiple connecting shaft first ends are connected and the end of multiple connecting shafts second with the first rotating ring
It is connected with the second rotating ring；The quantity of mould placing rack is consistent with the quantity of connecting shaft, multiple mould placing racks respectively with it is many
Individual connecting shaft is hinged；Drive mechanism is connected with rotating shaft and drive shaft is rotated.
It is preferred that, mould placing rack includes two the first triangle frames positioned opposite, and the first triangle frame is included successively
The first pole, the second pole, the 3rd pole of head and the tail connection, the first pole and the second pole junction are by articulated elements with being connected
Axle is hinged, and is connected between the 3rd pole of two triangle frames by multiple 4th poles.
It is preferred that, connected between two neighboring 4th pole by the 5th pole.
It is preferred that, the first pole and the second pole junction are connected by the 6th pole with the 3rd pole middle part.
It is preferred that, in addition to two the first support frames positioned opposite, the second support frames, the first support frame are arranged on body of heater
Outside is simultaneously located on the outside of body of heater the first side wall, and the second support frame is arranged on outside body of heater and positioned at body of heater second sidewall outside, drive
Motivation structure is arranged on the first support frame, and rotating shaft first end is rotated with the first support frame to be connected and its second end and the second support frame
Rotate connection.
It is preferred that, the first support frame includes the second triangle frame, and the second triangle frame includes the first of head and the tail connection successively
Support bar, second support bar, the 3rd support bar, rotating shaft first end is rotated with first support bar and second support bar junction to be connected
Connect, the 3rd support bar bottom is provided with multiple first support feets.
It is preferred that, first support bar and second support bar junction are connected by the 4th support bar with the 3rd support bar middle part
Connect.
It is preferred that, the second support frame includes the 3rd triangle frame, and the 3rd triangle frame includes the 5th of head and the tail connection successively
Support bar, the 6th support bar, the 7th support bar, the end of rotating shaft second is rotated with the 5th support bar and the 6th support bar junction to be connected
Connect, the 7th support bar bottom is provided with multiple second support feets.
It is preferred that, the 5th support bar and the 6th support bar junction are connected by the 8th support bar with the 7th support bar middle part
Connect.
It is preferred that, connected between the 3rd support bar and the 7th support bar by multiple 9th support bars.
The composite propeller curing oven of built-in rotating mechanism proposed by the present invention, by setting multiple mould placing racks
The composite propeller mould to be heated for placing, is rotated by drive mechanism drive shaft, and rotating shaft drives first to rotate
Ring, the second rotating ring are rotated, and the first rotating ring, the second rotating ring drive multiple mould placing racks to rotate, and mould placing rack drives
Mold rotation, is heating and curing in use, being passed through circulating air into body of heater to mould.Curing oven of the present invention is by making
Reach that the upper and lower mould temperature difference is at ± 1 DEG C or so in stove with the mode of built-in rotating mechanism and hot air circulating system, so as to meet multiple
Requirement of the condensation material propeller in forming process to temperature, cost is low, and in-furnace temperature is uniform, reasonable in design, takes empty
Between it is small, heat utilization efficiency is high.
Brief description of the drawings
Fig. 1 is a kind of structural representation of the composite propeller curing oven of built-in rotating mechanism proposed by the present invention；
Fig. 2 is Fig. 1 rearview；
Fig. 3 is Fig. 1 left view；
Fig. 4 is Fig. 1 top view.
Embodiment
As shown in Figure 1, Figure 2, Figure 3, Figure 4, Fig. 1 is a kind of composite spiral of built-in rotating mechanism proposed by the present invention
The structural representation of oar curing oven；Fig. 2 is Fig. 1 rearview；Fig. 3 is Fig. 1 left view；Fig. 4 is Fig. 1 top view.
Reference picture 1- Fig. 4, the present invention proposes a kind of composite propeller curing oven of built-in rotating mechanism, including body of heater
1st, the first support frame, the second support frame, rotating mechanism, multiple mould placing racks and drive mechanism 2, wherein：
First support frame is arranged on the outside of body of heater 1 and on the outside of the first side wall of body of heater 1, and the first support frame includes the two or three
Angular frame, the second triangle frame includes the first support bar 15 of head and the tail connection, second support bar 16, the 3rd support bar 17 successively,
First support bar 15 and the junction of second support bar 16 are connected by the 4th support bar 19 with the middle part of the 3rd support bar 17, the 3rd
The bottom of strut 17 is provided with multiple first support feets 18.
Second support frame and the first support frame are positioned opposite, and the second support frame is arranged on the outside of body of heater 1 and positioned at body of heater 1 the
Two side-wall outer sides, the second support frame includes the 3rd triangle frame, and the 3rd triangle frame includes the 5th support of head and the tail connection successively
Bar 20, the 6th support bar 21, the 7th support bar 22, the 5th support bar 20 and the junction of the 6th support bar 21 pass through the 8th support bar
24 are connected with the middle part of the 7th support bar 22, are connected between the 7th support bar 22 and the 3rd support bar 17 by multiple 9th support bars 25
Connect, the bottom of the 7th support bar 22 is provided with multiple second support feets 23.
Rotating mechanism is arranged in body of heater 1, and rotating mechanism includes the first rotating ring 3, the second rotating ring 4, multiple connecting shafts
5th, rotating shaft 6, the first rotating ring 3, the second rotating ring 4 are positioned opposite.The first end of rotating shaft 6 and body of heater 1 and first support bar 15 and the
The junction of two support bar 16 rotates connection, and the end of rotating shaft 6 second is sequentially passed through in the first side wall of body of heater 1, the geometry of the first rotating ring 3
Turn after the heart, the geometric center of the second rotating ring 4, the second sidewall of body of heater 1 with the 5th support bar 20 and the junction of the 6th support bar 21
Dynamic connection, the inner side of the first rotating ring 3 is fixedly connected by multiple head rods 7 with rotating shaft 6, and the inner side of the second rotating ring 4 passes through
Multiple second connecting rods 8 are fixedly connected with rotating shaft 6.Multiple connecting shafts 5 are arranged on the first rotating ring 3 and the second rotation in parallel to each other
Circumferentially it is distributed between change 4 and centered on rotating shaft 6, multiple first ends of connecting shaft 5 are connected and multiple with the first rotating ring 3
The end of connecting shaft 5 second is connected with the second rotating ring 4.
Mould placing rack includes two the first triangle frames positioned opposite, and the first triangle frame includes head and the tail successively and connected
The first pole 9, the second pole 10, the 3rd pole 11, the first pole 9 and the junction of the second pole 10 by the 6th pole 14 with
The middle part of 3rd pole 11 is connected, and is connected between the 3rd pole 11 of two triangle frames by multiple 4th poles 12, adjacent two
Connected between individual 4th pole 12 by the 5th pole 13.The quantity of mould placing rack is consistent with the quantity of connecting shaft 5, each mould
First pole 9 of two the first triangle frames of rack and the junction of the second pole 10 by articulated elements respectively with each connecting shaft
5 are hinged.
Drive mechanism 2 is arranged on the first support frame, and drive mechanism 2 is connected with rotating shaft 6 and drive shaft 6 is rotated.
The composite propeller curing oven of a kind of built-in rotating mechanism proposed by the present invention, by setting multiple moulds to put
Putting frame is used to place composite propeller mould to be heated, is rotated by the drive shaft 5 of drive mechanism 2, rotating shaft 5 drives the
One rotating ring 3, the second rotating ring 4 are rotated, and the first rotating ring 3, the second rotating ring 4 drive multiple mould placing racks to rotate, mould
Rack driven mold is rotated, and mould is heating and curing in use, being passed through circulating air into body of heater.The present invention is solid
Change stove and reach that the upper and lower mould temperature difference is at ± 1 DEG C or so in stove by using the mode of built-in rotating mechanism and hot air circulating system,
So as to meet requirement of the composite propeller to temperature in forming process, cost is low, and in-furnace temperature is uniform, and structure design is closed
Reason, occupies little space, and heat utilization efficiency is high.By setting the second triangle frame, the 3rd triangle frame to be propped up for countershaft 6
Support so that rotating shaft 6 installs stable, can avoid mould placing rack during the rotation of rotating shaft 6 from rocking.
The foregoing is only a preferred embodiment of the present invention, but protection scope of the present invention be not limited thereto,
Any one skilled in the art the invention discloses technical scope in, technique according to the invention scheme and its
Inventive concept is subject to equivalent substitution or change, should all be included within the scope of the present invention.
Claims (10)
1. a kind of composite propeller curing oven of built-in rotating mechanism, it is characterised in that including body of heater (1), rotating mechanism,
Multiple mould placing racks and drive mechanism (2), wherein：Rotating mechanism is arranged in body of heater (1), and rotating mechanism includes the first rotation
Ring (3), the second rotating ring (4), multiple connecting shafts (5), rotating shaft (6), the first rotating ring (3), the second rotating ring (4) are with respect to cloth
Put, rotating shaft (6) first end and body of heater (1) the first side wall are rotated and be connected, the end of rotating shaft (6) second sequentially pass through the first rotating ring (3),
The geometric center of second rotating ring (4) and body of heater (1) second sidewall are rotated and be connecteds, and the first rotating ring (3) inner side passes through multiple the
One connecting rod (7) is fixedly connected with rotating shaft (6), and multiple second connecting rods (8) and rotating shaft (6) are passed through on the inside of the second rotating ring (4)
It is fixedly connected, multiple connecting shafts (5) are arranged between the first rotating ring (3) and the second rotating ring (4) and to turn in parallel to each other
Axle is circumferentially distributed centered on (6), and multiple connecting shaft (5) first ends are connected and multiple connecting shafts (5) with the first rotating ring (3)
Second end is connected with the second rotating ring (4)；The quantity of mould placing rack is consistent with the quantity of connecting shaft (5), and multiple moulds are put
Frame is put to be hinged with multiple connecting shafts (5) respectively；Drive mechanism (2) is connected with rotating shaft (6) and drive shaft (6) is rotated.
2. the composite propeller curing oven of built-in rotating mechanism according to claim 1, it is characterised in that mould is put
Putting frame includes two the first triangle frames positioned opposite, the first triangle frame include successively the first pole (9) of head and the tail connection,
Second pole (10), the 3rd pole (11), the first pole (9) pass through articulated elements and connecting shaft with the second pole (10) junction
(5) it is hinged, is connected between the 3rd pole (11) of two triangle frames by multiple 4th poles (12).
3. the composite propeller curing oven of built-in rotating mechanism according to claim 2, it is characterised in that adjacent two
Connected between individual 4th pole (12) by the 5th pole (13).
4. the composite propeller curing oven of built-in rotating mechanism according to claim 2, it is characterised in that first
Bar (9) and the second pole (10) junction are by the 6th pole (14) with being connected in the middle part of the 3rd pole (11).
5. the composite propeller curing oven of the built-in rotating mechanism according to any one of claim 1-4, its feature
It is, in addition to two the first support frames positioned opposite, the second support frames, it is outside simultaneously that the first support frame is arranged on body of heater (1)
On the outside of body of heater (1) the first side wall, the second support frame is arranged on body of heater (1) outside and on the outside of body of heater (1) second sidewall,
Drive mechanism (2) is arranged on the first support frame, and rotating shaft (6) first end and the first support frame, which are rotated, to be connected and its second end and the
Two support frames rotate connection.
6. the composite propeller curing oven of built-in rotating mechanism according to claim 5, it is characterised in that first
Support includes the second triangle frame, and the second triangle frame includes first support bar (15), the second support bar of head and the tail connection successively
(16), the 3rd support bar (17), rotating shaft (6) first end is rotated with first support bar (15) and second support bar (16) junction to be connected
Connect, the 3rd support bar (17) bottom is provided with multiple first support feets (18).
7. the composite propeller curing oven of built-in rotating mechanism according to claim 6, it is characterised in that first
Strut (15) and second support bar (16) junction are by the 4th support bar (19) with being connected in the middle part of the 3rd support bar (17).
8. the composite propeller curing oven of the built-in rotating mechanism according to claim 6 or 7, it is characterised in that the
Two support frames include the 3rd triangle frame, the 3rd triangle frame include successively head and the tail connection the 5th support bar (20), the 6th
Strut (21), the 7th support bar (22), the end of rotating shaft (6) second turn with the 5th support bar (20) and the 6th support bar (21) junction
Dynamic connection, the 7th support bar (22) bottom is provided with multiple second support feets (23).
9. the composite propeller curing oven of built-in rotating mechanism according to claim 8, it is characterised in that the 5th
Strut (20) and the 6th support bar (21) junction are by the 8th support bar (24) with being connected in the middle part of the 7th support bar (22).
10. the composite propeller curing oven of built-in rotating mechanism according to claim 8, it is characterised in that the 3rd
It is connected between support bar (17) and the 7th support bar (22) by multiple 9th support bars (25).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710630657.XA CN107175785A (en) | 2017-07-28 | 2017-07-28 | A kind of composite propeller curing oven of built-in rotating mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710630657.XA CN107175785A (en) | 2017-07-28 | 2017-07-28 | A kind of composite propeller curing oven of built-in rotating mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107175785A true CN107175785A (en) | 2017-09-19 |
Family
ID=59837786
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710630657.XA Pending CN107175785A (en) | 2017-07-28 | 2017-07-28 | A kind of composite propeller curing oven of built-in rotating mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107175785A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108889633A (en) * | 2018-05-29 | 2018-11-27 | 安徽卓尔航空科技有限公司 | A kind of propeller detects automatically picks device |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS63154333A (en) * | 1986-12-18 | 1988-06-27 | Sumitomo Electric Ind Ltd | Continuous curing equipment for cylinder made of fiber-reinforced plastics |
| CN1672522A (en) * | 2004-03-28 | 2005-09-28 | 郑西安 | Design method of barbecue oven for baking, roasting and braising |
| CN202842544U (en) * | 2012-09-14 | 2013-04-03 | 程远平 | Oven applied to shoe material molding machine |
| JP2014115021A (en) * | 2012-12-10 | 2014-06-26 | Oppc Co Ltd | Capacitor chip vacuum sintering furnace |
| CN204286088U (en) * | 2014-11-25 | 2015-04-22 | 盐城市盛丰机械有限公司 | A kind of efficient heat parts preheating furnace |
| CN104943202A (en) * | 2015-07-03 | 2015-09-30 | 浙江大学 | Carbon fiber composite material axial flow fan impeller molding and curing device |
| CN204714859U (en) * | 2015-06-09 | 2015-10-21 | 含山县朝霞铸造有限公司 | A kind of rotation annealing furnace |
| CN205086347U (en) * | 2015-11-13 | 2016-03-16 | 成都鲁晨新材料科技有限公司 | Wound product is with rotatory solidification frock |
| CN205989458U (en) * | 2016-08-04 | 2017-03-01 | 青岛高测科技股份有限公司 | A kind of resin-diamond line of cut curing furnace special |
| CN207027996U (en) * | 2017-07-28 | 2018-02-23 | 安徽卓尔航空科技有限公司 | A kind of composite propeller curing oven of built-in rotating mechanism |
-
2017
- 2017-07-28 CN CN201710630657.XA patent/CN107175785A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS63154333A (en) * | 1986-12-18 | 1988-06-27 | Sumitomo Electric Ind Ltd | Continuous curing equipment for cylinder made of fiber-reinforced plastics |
| CN1672522A (en) * | 2004-03-28 | 2005-09-28 | 郑西安 | Design method of barbecue oven for baking, roasting and braising |
| CN202842544U (en) * | 2012-09-14 | 2013-04-03 | 程远平 | Oven applied to shoe material molding machine |
| JP2014115021A (en) * | 2012-12-10 | 2014-06-26 | Oppc Co Ltd | Capacitor chip vacuum sintering furnace |
| CN204286088U (en) * | 2014-11-25 | 2015-04-22 | 盐城市盛丰机械有限公司 | A kind of efficient heat parts preheating furnace |
| CN204714859U (en) * | 2015-06-09 | 2015-10-21 | 含山县朝霞铸造有限公司 | A kind of rotation annealing furnace |
| CN104943202A (en) * | 2015-07-03 | 2015-09-30 | 浙江大学 | Carbon fiber composite material axial flow fan impeller molding and curing device |
| CN205086347U (en) * | 2015-11-13 | 2016-03-16 | 成都鲁晨新材料科技有限公司 | Wound product is with rotatory solidification frock |
| CN205989458U (en) * | 2016-08-04 | 2017-03-01 | 青岛高测科技股份有限公司 | A kind of resin-diamond line of cut curing furnace special |
| CN207027996U (en) * | 2017-07-28 | 2018-02-23 | 安徽卓尔航空科技有限公司 | A kind of composite propeller curing oven of built-in rotating mechanism |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108889633A (en) * | 2018-05-29 | 2018-11-27 | 安徽卓尔航空科技有限公司 | A kind of propeller detects automatically picks device |
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