CN108716797A - A kind of mechanical device that can manufacture the residual ice of experimental aeroplane - Google Patents
A kind of mechanical device that can manufacture the residual ice of experimental aeroplane Download PDFInfo
- Publication number
- CN108716797A CN108716797A CN201810505093.1A CN201810505093A CN108716797A CN 108716797 A CN108716797 A CN 108716797A CN 201810505093 A CN201810505093 A CN 201810505093A CN 108716797 A CN108716797 A CN 108716797A
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- CN
- China
- Prior art keywords
- borneol
- sleeve
- lid
- aeroplane
- mechanical device
- 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.)
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25C—PRODUCING, WORKING OR HANDLING ICE
- F25C1/00—Producing ice
- F25C1/22—Construction of moulds; Filling devices for moulds
- F25C1/24—Construction of moulds; Filling devices for moulds for refrigerators, e.g. freezing trays
Abstract
A kind of mechanical device that can manufacture the residual ice of experimental aeroplane.It includes main body, thickness block, sleeve and cap；The present invention is placed thickness block on bottom plate, then cap is pressed on thickness block, the space between cap lower surface and plate upper surface is the thickness of borneol by the diameter of the internal diameter restrictions borneol of sleeve.Sleeve can be removed at left and right sides of borneol when taking out borneol, ensure that the integrality of the cylinder surface of borneol by the tube-in-tube structure for devising two halves formula.Method by applying hydrophobic coat in plate upper surface so that borneol lower surface can completely take off from bottom plate.By way of being embedded to heating wire in cap, borneol upper surface is slightly melted electric-heating-wire-heating, the heat of generation when sloughing borneol, to can guarantee that the upper surface of borneol is completely disengaged with cap.In addition, the present apparatus also has many advantages, such as reasonable in design, operating method, at low cost.
Description
Technical field
The invention belongs to technical field of civil aviation, are filled more particularly to a kind of machinery that can manufacture the residual ice of experimental aeroplane
It sets.
Background technology
Aircraft deicing problem is to influence one of the most important safety problems of winter safety of civil aviation operation.At present to the residual ice of aircraft
Detection mainly utilizes infrared multispectral detection technique.This technology can detect the residual ice thickness of aircraft surfaces.Its exploitation and
Optimizing phase needs that its equipment, algorithm etc. are tested and calibrated in laboratory conditions.Currently, making in the lab
Borneol is difficult to accurately control on thickness, and due to required borneol thinner thickness, is easily damaged, causes when taking out borneol
Waste in time and efforts.
Invention content
To solve the above-mentioned problems, the purpose of the present invention is to provide a kind of machineries that can manufacture the residual ice of experimental aeroplane
Device.
In order to achieve the above object, the mechanical device provided by the invention that can manufacture the residual ice of experimental aeroplane includes master
Body, thickness block, sleeve and cap；Wherein main body includes compression bar, column, nut and bottom plate, and the upper and lower side of column is equipped with outer spiral shell
Line；Floor level is arranged, and both sides are respectively formed there are one for fixing the screw hole of two root posts lower end, concave shape on middle part surface
At there are one locating slots；Compression bar is horizontally disposed, and both sides and middle part are respectively formed there are one the through-hole vertically extended, two
The upper end of column is extended through and is fixed using nut after two through-holes of both sides on compression bar；Thickness block is made of three bars
Star structure, set that there are one the anchor points for being downwardly projected and being inserted on bottom plate in locating slot at bottom center；Sleeve
Including two sub-sleeves, at least one cuff and two sealing strips；Wherein sub-sleeve is half-round tubular arc panel, two sub-sleeves
Circular tube shaped is formed after corresponding assembly, at least one circumferentially positioned slot, every positioning are formed on the outer circumference surface of every sub-sleeve
There are one cuffs for set on slot, and the stitching portion of two sub-sleeves is separately installed with a sealing strip；Sleeve is placed on positioned at thickness
The backplate surface on the outside of block is spent, upper end is compressed by compression bar；Cap includes bull stick, top of closure, lid lower part and heating wire；Wherein
The vertical rod that top of closure is fixed on by lid and lower end in the middle part of lid top surface is constituted, and outer spiral shell is formed on the outer circumference surface of lid
Line, forms that there are two the binding posts for trepanning and fixed heating wire outer end through heating wire both ends on top surface；Vertical rod
There are one radial holes for top formation；Bull stick is inserted in radial hole；Lid lower part it is opening up, formed in inner bottom surface useful
It is formed with internal thread, and the circumferential wall two sides of lid lower part in the helical form locating slot for placing heating wire, on inner peripheral surface
Edge position is respectively formed there are one water injection hole up and down, is screwed by internal and external threads between top of closure and lid lower part；
Sleeve inner is placed on after top of closure, heating wire and the combination of lid lower part, vertical rod passes through logical in the middle part of compression bar from bottom to top
Hole, bull stick are located at cartridge exterior.
It is additionally provided with sealing ring between the top of closure and lid lower part.
The cuff is fastened by screw bolt and nut.
The thickness block is multiple, is respectively provided with different thickness.
The mechanical device provided by the invention that the residual ice of experimental aeroplane can be manufactured passes through the internal diameter restrictions borneol of sleeve
Diameter is placed thickness block on bottom plate, then cap is pressed on thickness block, the sky between cap lower surface and plate upper surface
Between be borneol thickness.The tube-in-tube structure for devising two halves formula can move sleeve at left and right sides of borneol when taking out borneol
It removes, ensure that the integrality of the cylinder surface of borneol.Method by applying hydrophobic coat in plate upper surface so that borneol following table
Face can completely take off from bottom plate.By way of being embedded to heating wire in cap, when sloughing borneol to electric-heating-wire-heating,
The heat of generation makes borneol upper surface slightly melt, to can guarantee that the upper surface of borneol is completely disengaged with cap.In addition,
The present apparatus also has many advantages, such as reasonable in design, operating method, at low cost.
Description of the drawings
Fig. 1 is agent structure exploded pictorial in the mechanical device provided by the invention that can manufacture the residual ice of experimental aeroplane
Figure.
Fig. 2 is thickness block structure schematic diagram in the mechanical device provided by the invention that can manufacture the residual ice of experimental aeroplane.
Fig. 3 is the mechanical device middle sleeve STRUCTURE DECOMPOSITION signal provided by the invention that can manufacture the residual ice of experimental aeroplane
Figure.
Fig. 4 is that cap STRUCTURE DECOMPOSITION is illustrated in the mechanical device provided by the invention that can manufacture the residual ice of experimental aeroplane
Figure.
Fig. 5 is the mechanical device overall structure decomposition diagram provided by the invention that can manufacture the residual ice of experimental aeroplane.
Specific implementation mode
The machinery provided by the invention that the residual ice of experimental aeroplane can be manufactured is filled in the following with reference to the drawings and specific embodiments
It sets and is described in detail.
As Figure 1-Figure 5, the mechanical device provided by the invention that the residual ice of experimental aeroplane can be manufactured include main body,
Thickness block 5, sleeve and cap；Wherein main body includes compression bar 1, column 2, nut 3 and bottom plate 4, and the upper and lower side of column 2 is equipped with outside
Screw thread；Bottom plate 4 is horizontally disposed, and both sides are respectively formed that there are one the screw hole for fixing 2 lower end of two root posts, middle part surface fovea superiors
Fall into locating slot 6 there are one being formed；Compression bar 1 is horizontally disposed, and both sides and middle part are respectively formed logical there are one what is vertically extended
Hole, the upper end of two root posts 2 extends through to be fixed after two through-holes of both sides using nut 3 on compression bar 1；Thickness block 5 is
The star structure being made of three bars, sets that there are one be downwardly projected and be inserted on bottom plate 4 in locating slot 6 at bottom center
Anchor point；Sleeve includes two sub-sleeves 7, at least one cuff 8 and two sealing strips 9；Wherein sub-sleeve 7 is half-round tubular
Arc panel, two sub-sleeves 7 form circular tube shaped after corresponding to assembly, at least one are formed on the outer circumference surface of every sub-sleeve 7
Circumferentially positioned slot, on every locating slot set there are one cuff 8, and the stitching portion of two sub-sleeves 7 be separately installed with one it is close
Strip of paper used for sealing 9；Sleeve is placed on 4 surface of bottom plate positioned at 5 outside of thickness block, and upper end is compressed by compression bar 1；Cap includes bull stick 10, lid
Sub- top 11, lid lower part 12 and heating wire 13；Wherein top of closure 11 is fixed on by lid 15 and lower end in 15 top surface of lid
The vertical rod 16 in portion is constituted, and external screw thread is formed on the outer circumference surface of lid 15, forms that there are two for running through electric heating on top surface
The binding post 20 of 13 outer end of trepanning and fixed heating wire at 13 both ends of silk；There are one radial holes 17 for the top formation of vertical rod 16；
Bull stick 10 is inserted in radial hole 17；Lid lower part 12 it is opening up, be formed in inner bottom surface for placing heating wire 13
Helical form locating slot, internal thread, and the circumferential wall both sides of the edge position difference of lid lower part 12 are formed on inner peripheral surface
It is formed there are one water injection hole 21 up and down, is screwed by internal and external threads between top of closure 11 and lid lower part 12；Lid
Top 11, heating wire 13 and lid lower part 12 are placed on sleeve inner after combining, vertical rod 16 passes through 1 middle part of compression bar from bottom to top
Through-hole, bull stick 10 is located at cartridge exterior.
It is additionally provided with sealing ring 14 between the top of closure 11 and lid lower part 12, to ensure its internal leakproofness.
The cuff 8 is fastened by bolt 18 and nut 19, and two sub-sleeves 7 are tightly secured together.
The thickness block 5 is multiple, is respectively provided with different thickness, for example, 0.5mm, 1mm, 2mm, 5mm, 6mm, 7mm,
8mm, 9mm, 10mm etc..
Now the mechanical device application method provided by the invention that the residual ice of experimental aeroplane can be manufactured is described below：
1, one layer of hydrophobic coat is coated in the upper surface of bottom plate 4 first, then distinguishes the lower end of two root posts in Fig. 12
It is threadedly coupled with two screw holes of 4 both sides of bottom plate；
2, the sleeve in Fig. 3 is assembled, wherein two sealing strips 9 are mounted at the docking of two sub-sleeves 7, will be covered
Hoop 8 is sleeved in the locating slot on 7 outer circumference surface of sub-sleeve, and is fastened by bolt 18 and nut 19；
3, it needs to choose the thickness block 5 shown in Fig. 2 with suitable thickness according to experiment, then passes through 5 bottom surface of thickness block
Thickness block 5 is fixed on bottom plate 4 by the cooperation of anchor point and locating slot 6 on bottom plate 4 at center；
4, the good sleeve of said combination is placed on 4 upper surface of bottom plate in 5 outside of thickness block；
5, the heating wire 13 in Fig. 4 is put into the helical form locating slot of lid lower part 12, then by 13 both ends of heating wire
It draws and is fixed on binding post 20 upwards from two trepannings of top of closure 11 respectively, later by top of closure 11 and lid
It is screwed by internal and external threads between lower part 12, while sealing ring 14 being added therebetween to ensure to seal；
6, the vertical rod 15 of top of closure in Fig. 4 11 is inserted into Fig. 1 in the through-hole at the middle part of compression bar 1, while by 1 liang of compression bar
The upper end that the through-hole at end is respectively aligned to two root posts 2 is inserted into, and is fastened column 2 by nut 3, with ensure the lower end of sleeve with
4 upper surface of bottom plate fits closely；
7, the bull stick 10 in Fig. 4 is inserted into top of closure 11 in the radial hole 17 of vertical rod 16, is rotated using bull stick 10
Cap makes its lower surface be bonded with thickness block 5；
8, by the water filling into the present apparatus of any water injection hole 21 of 12 edge of lid lower part in Fig. 4, when water is from another note
Illustrate that water filling is complete when being overflowed in water hole 21；
9, the present apparatus is put into freezing equipment, completes water freezing and forms ice between 4 upper surface of lid lower part 12 and bottom plate
The process of piece；
10, after the completion of freezing, the present apparatus is taken out from freezing equipment；
11, nut 3 is first unclamped, bolt 18 and nut 19 is then unclamped, removes cuff 8；
12, sub-sleeve 7 is separated from both sides, completes the disengagement of borneol side；
13, due to the effect of the hydrophobic coat of 4 upper surface of bottom plate, the small surface thereon of cohesive force of borneol lower surface is glued
When tying power, therefore removing cap, borneol lower surface can rapidly be disengaged with 4 upper surface of bottom plate, and borneol is bonded in lid at this time
On lower part 12；
14, binding post 20 is powered, heats heating wire 13, will be disengaged with lid lower part 12 after borneol upper surface is heated, this
When can take out borneol.
Claims (4)
1. a kind of mechanical device that can manufacture the residual ice of experimental aeroplane, it is characterised in that：The mechanical device include main body,
Thickness block (5), sleeve and cap；Wherein main body includes compression bar (1), column (2), nut (3) and bottom plate (4), column (2) it is upper
Lower end is equipped with external screw thread；Bottom plate (4) is horizontally disposed, and both sides are respectively formed that there are one for fixing two root posts (2) lower end
Screw hole, recess is formed with a locating slot (6) on middle part surface；Compression bar (1) is horizontally disposed, and both sides and middle part are respectively formed with one
The upper end of a through-hole vertically extended, two root posts (2) extends through on compression bar (1) after two through-holes of both sides
It is fixed using nut (3)；Thickness block (5) is the star structure being made of three bars, is set at bottom center there are one being downwardly projected
And it is inserted into the anchor point on bottom plate (4) in locating slot (6)；Sleeve includes two sub-sleeves (7), at least one cuffs
(8) and two sealing strips (9)；Wherein sub-sleeve (7) is half-round tubular arc panel, is formed after the corresponding assembly of two sub-sleeves (7)
Circular tube shaped, is formed at least one circumferentially positioned slot on the outer circumference surface of every sub-sleeve (7), on every locating slot there are one sets
Cuff (8), and the stitching portion of two sub-sleeves (7) is separately installed with a sealing strip (9)；Sleeve is placed on positioned at thickness block
(5) bottom plate (4) surface on the outside of, upper end are compressed by compression bar (1)；Cap includes bull stick (10), top of closure (11), lid lower part
(12) and heating wire (13)；Wherein top of closure (11) is fixed on vertical in the middle part of lid (15) top surface by lid (15) and lower end
Bar (16) is constituted, and external screw thread is formed on the outer circumference surface of lid (15), forms that there are two for running through heating wire on top surface
(13) binding post (20) of the trepanning at both ends and fixed heating wire (13) outer end；There are one radial for the top formation of vertical rod (16)
Hole (17)；(10 are inserted in radial hole (17) bull stick；Lid lower part (12) it is opening up, be formed with and be used in inner bottom surface
The helical form locating slot of heating wire (13) is placed, internal thread, and the circumferential wall of lid lower part (12) are formed on inner peripheral surface
Both sides of the edge position is respectively formed the water injection hole (21) there are one up and down, between top of closure (11) and lid lower part (12)
It is screwed by internal and external threads；It is placed on sleeve inner after top of closure (11), heating wire (13) and lid lower part (12) combination, is hung down
Straight-bar (16) passes through the through-hole in the middle part of compression bar (1), bull stick (10) to be located at cartridge exterior from bottom to top.
2. the mechanical device according to claim 1 that the residual ice of experimental aeroplane can be manufactured, it is characterised in that：The lid
It is additionally provided with sealing ring (14) between sub- top (11) and lid lower part (12).
3. the mechanical device according to claim 1 that the residual ice of experimental aeroplane can be manufactured, it is characterised in that：The set
(8) are bound round to fasten by bolt (18) and nut (19).
4. the mechanical device according to claim 1 that the residual ice of experimental aeroplane can be manufactured, it is characterised in that：The thickness
It is multiple to spend block (5), is respectively provided with different thickness.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810505093.1A CN108716797B (en) | 2018-05-24 | 2018-05-24 | Mechanical device capable of manufacturing residual ice of airplane for experiment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810505093.1A CN108716797B (en) | 2018-05-24 | 2018-05-24 | Mechanical device capable of manufacturing residual ice of airplane for experiment |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108716797A true CN108716797A (en) | 2018-10-30 |
| CN108716797B CN108716797B (en) | 2020-04-17 |
Family
ID=63900505
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810505093.1A Active CN108716797B (en) | 2018-05-24 | 2018-05-24 | Mechanical device capable of manufacturing residual ice of airplane for experiment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108716797B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114812029A (en) * | 2022-04-14 | 2022-07-29 | 中国航发沈阳发动机研究所 | Borneol preparation device and method for aviation turbofan engine borneol swallowing test |
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| US5113664A (en) * | 1991-01-18 | 1992-05-19 | Polar Spring Corporation | Melt system for liquid purification by batch crystallization |
| CN2145960Y (en) * | 1993-02-23 | 1993-11-10 | 郭进登 | Flat thin ice maker |
| JPH10267478A (en) * | 1997-03-27 | 1998-10-09 | Sanyo Electric Co Ltd | Auger type ice making machine |
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2018
- 2018-05-24 CN CN201810505093.1A patent/CN108716797B/en active Active
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| US5113664A (en) * | 1991-01-18 | 1992-05-19 | Polar Spring Corporation | Melt system for liquid purification by batch crystallization |
| CN2145960Y (en) * | 1993-02-23 | 1993-11-10 | 郭进登 | Flat thin ice maker |
| JPH10267478A (en) * | 1997-03-27 | 1998-10-09 | Sanyo Electric Co Ltd | Auger type ice making machine |
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| CN1844809A (en) * | 2006-05-16 | 2006-10-11 | 宁波大学 | Thawing stripping type ice making apparatus |
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| EP2630423A1 (en) * | 2010-10-19 | 2013-08-28 | Université du Québec à Chicoutimi | Mechanical vibration de-icing system and method |
| CN202188709U (en) * | 2011-08-05 | 2012-04-11 | 赵义军 | Mould box for producing ice plate |
| CN106965939A (en) * | 2017-03-17 | 2017-07-21 | 中国民航大学 | A kind of polyphaser image collecting device based on the residual ice detection of near infrared multispectral |
Non-Patent Citations (1)
| Title |
|---|
| 高建树，郑大川，于之靖，诸葛晶昌: ""机翼铝蒙皮积冰及冰厚的近红外多光谱检测"", 《激光与红外》 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114812029A (en) * | 2022-04-14 | 2022-07-29 | 中国航发沈阳发动机研究所 | Borneol preparation device and method for aviation turbofan engine borneol swallowing test |
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| Publication number | Publication date |
|---|---|
| CN108716797B (en) | 2020-04-17 |
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