CN209625508U - A kind of aviation cable tension implementation platform - Google Patents
A kind of aviation cable tension implementation platform Download PDFInfo
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- CN209625508U CN209625508U CN201822036349.7U CN201822036349U CN209625508U CN 209625508 U CN209625508 U CN 209625508U CN 201822036349 U CN201822036349 U CN 201822036349U CN 209625508 U CN209625508 U CN 209625508U
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- cable wire
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- wheel carrier
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- turnbuckle
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- 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 description 7
- 244000309464 bull Species 0.000 claims 1
- 230000005540 biological transmission Effects 0.000 description 10
- 229910000831 Steel Inorganic materials 0.000 description 6
- 238000012423 maintenance Methods 0.000 description 6
- 239000010959 steel Substances 0.000 description 6
- 230000000694 effects Effects 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 235000008331 Pinus X rigitaeda Nutrition 0.000 description 1
- 235000011613 Pinus brutia Nutrition 0.000 description 1
- 241000018646 Pinus brutia Species 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
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Abstract
The utility model discloses a kind of aviation cable tension implementation platforms, including desk, cable wire disk component, turnbuckle component, truck assembly, first cable wire, second cable wire, it is spaced pre-determined distance on desk top, cable wire disk component is respectively set, truck assembly turnbuckle component includes the first cable connector, turnbuckle, second cable connector, the left end of turnbuckle is connect with one end forward screw thread of the first cable connector, the right end of turnbuckle is connect with second cable connector one end reverse thread, the other end of first cable connector is connect with first cable wire one end, the first cable wire other end is connect with cable wire disk component, second cable wire one end is connect with cable wire disk component, the second cable wire other end bypasses truck assembly, and it is connect with the second cable connector other end.The purpose of this utility model is to provide a kind of tension adjustments to be more convenient, the aviation cable tension implementation platform of more secure and reliable.
Description
Technical field
The utility model relates to aviation training equipment technical field, in particular to a kind of aviation cable tension implementation platform.
Background technique
In commercial aircraft, cable wire plays transmission, provides power-actuated effect, and excessively if pine, strength is transmitted not
In place, associated components actuation below is influenced；If tension, it is easily damaged driving member, is also easy to scrap cable wire in advance, therefore,
There is stringent regulation in management board, civil aviation the Northwest, state to aviation cable tension in aircraft maintenance.It is currently undertaken by aircraft
The mechanism of training on maintenance also rests on the theory teaching stage to the training of student, and existing training equipment structure is simple, can not be right
The tension of cable wire is adjusted, and causes student in training that can not grasp prototype maintenance work.
Utility model content
The purpose of this utility model is to provide a kind of aviation cable tension implementation platforms, solve to mention in above-mentioned background technique
Out the problem of the tension of cable wire can not be adjusted.
To achieve the above object, the utility model provides the following technical solutions: a kind of aviation cable tension implementation platform, packet
Desk, cable wire disk component, turnbuckle component, truck assembly, the first cable wire, the second cable wire are included, is spaced on the desk top
Pre-determined distance is respectively set the cable wire disk component, the truck assembly, the turnbuckle component include the first cable connector,
Turnbuckle, the second cable connector, the left end of the turnbuckle are connect with one end forward screw thread of first cable connector,
The right end of the turnbuckle is connect with second cable connector one end reverse thread, the other end of first cable connector
It is connect with first cable wire one end, the first cable wire other end is connect with the cable wire disk component, second cable wire one
End is connect with the cable wire disk component, and the second cable wire other end bypasses the truck assembly, and connects with second cable wire
Head other end connection.
Preferably, the centre of the turnbuckle, which goes out, is provided through mounting hole.
Preferably, the truck assembly includes the first small wheel carrier, the second small wheel carrier, the first big wheel carrier, the second largest wheel carrier, institute
The first big wheel carrier and the second largest wheel carrier are stated at a distance of pre-determined distance, the pulley of the first big wheel carrier, the second largest wheel carrier
Equal vertical direction setting, the first big wheel carrier are provided with the described first small wheel carrier at left side, and the second largest wheel carrier leans on
It is provided with the second small wheel carrier at nearly left side, the first small wheel carrier, the pulley of the second small wheel carrier are horizontally arranged, institute
Second cable wire one end is stated to connect with the cable wire disk component, the second cable wire other end sequentially pass through the second largest wheel carrier,
The second small wheel carrier, the first small wheel carrier, the first big wheel carrier, connect with second cable connector one end.
Preferably, the described first small wheel carrier, the second small wheel carrier, the first big wheel carrier, the second largest wheel carrier are equal
It is connected by screw to the top end face of the desk.
Preferably, the cable wire disk component includes pedestal, shaft, cable wire disk, adjustment arm, adjusting screw rod, the side wall of pedestal
On be provided with the support plate of horizontal direction, bearing is installed in the support plate, the shaft of vertical direction passes through the bearing, and
It is fixed on the inner ring of the bearing, the top of the shaft is provided with the cable wire disk of horizontal direction, along diameter on the cable wire disk
To adjustment arm is provided with, described adjustment arm one end is connect with the cable wire disk hinge, through setting on the adjustment arm other end
There is vertical reversed connecting hole, the adjustment arm middle is provided through the threaded hole of horizontal direction, and adjusting screw rod passes through institute
Threaded hole is stated, and is connected on the cable wire disk, the adjustment arm, the connecting hole, the adjusting screw rod are about the cable wire
Another group of the center line symmetrical setting of disk.
Preferably, it is provided through and described first on the first pin hole of setting, the cable wire disk in the support plate
Corresponding second pin hole of pin hole.
Preferably, protection board is provided on the outside of the cable wire disk, described protection board one end and the cable wire disk hinge connect
It connects.
Compared with prior art, the utility model has the beneficial effects that a kind of aviation cable tension of the utility model is real
Make platform, including desk, cable wire disk component, turnbuckle component, truck assembly, the first cable wire, the second cable wire, on desk top
Cable wire disk component, truck assembly is respectively set in interval pre-determined distance, turnbuckle component includes the first cable connector, elastic spiral shell
Set, the second cable connector, the left end of turnbuckle are connect with one end forward screw thread of the first cable connector, the right end of turnbuckle
It is connect with second cable connector one end reverse thread, the other end of the first cable connector is connect with first cable wire one end, the first steel
The rope other end is connect with cable wire disk component, and second cable wire one end is connect with cable wire disk component, and the second cable wire other end bypasses wheel carrier
Component, and connect with the second cable connector other end.Desk, cable wire disk component, turnbuckle component, truck assembly, the first steel
Rope, the second cable wire form a transmission system and are used to transmit power, after long time running, due to fatigue, abrasion etc., and steel
The tension of rope is just changed, thus do not reach requirement, when not reached requirement by tonometry of the tensometer to cable wire,
Turnbuckle is rotated, is connected by positive/negative thread, so that the length of turnbuckle component elongates or shortens, so that steel
Rope is tightened or loosens to have the function that adjust tension, to reach the tensile requirements of aviation cable wire.Due to the utility model
Aviation cable tension implementation platform therefore, can be higher when institute trains using the transmission system equal proportion production on civil aircraft
The study of effect is detected to the tension to aviation cable wire, and carries out the adjusting maintenance work of cable tension.In addition, setting is elastic
Swivel nut component, the adjusting of cable tension can efficiently be realized very much by rotating turnbuckle by tool, to reach aviation cable wire
Tensile requirements.
Detailed description of the invention
Fig. 1 is the main view of the utility model.
Fig. 2 is the top view of the utility model.
Fig. 3 is the structural schematic diagram of turnbuckle component in the utility model.
Fig. 4 is the structural schematic diagram of cable wire disk component in the utility model.
In figure: 1- desk；2- cable wire disk component；201- pedestal；202- bearing；203- shaft；204- cable wire disk；205- tune
Whole arm；206- connecting hole；207- adjusting screw rod；208- support plate；The first pin hole of 209-；The second pin hole of 210-；211- protection board；
3- turnbuckle component；The first cable connector of 301-；302- turnbuckle；The second cable connector of 303-；304- mounting hole；4- wheel
Frame component；The small wheel carrier of 401- first；The small wheel carrier of 402- second；The big wheel carrier of 403- first；The second largest wheel carrier of 404-；The first steel of 5-
Rope；The second cable wire of 6-.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-3 is please referred to, the utility model provides a kind of aviation cable tension implementation platform, including desk 1, cable wire disk
Component 2, turnbuckle component 3, truck assembly 4, the first cable wire 5, the second cable wire 6 are spaced pre-determined distance on 1 top of desk
The cable wire disk component 2, the truck assembly 4 is respectively set, spacing distance can be designed according to transmission distance, described elastic
Swivel nut component 3 includes the first cable connector 301, turnbuckle 302, the second cable connector 303, a left side for the turnbuckle 302
End is connect with one end forward screw thread of first cable connector 301, the right end of the turnbuckle 302 and second cable wire
The connection of 303 one end reverse thread of connector, the other end of first cable connector 301 are connect with described first cable wire, 5 one end, institute
It states 5 other end of the first cable wire to connect with the cable wire disk component 2, described second cable wire, 6 one end and the cable wire disk component 2 connect
It connects, 6 other end of the second cable wire bypasses the truck assembly 4, and connect with 303 other end of the second cable connector, steel
The mode that riveting or welding can be used between rope and cable connector connects.
The working principle and technical effect of above scheme: desk 1, cable wire disk component 2, turnbuckle component 3, truck assembly
4, the first cable wire 5, the second cable wire 6 form a transmission system for transmitting power, after long time running, due to fatigue, mill
The reasons such as damage, the tension of cable wire is just changed, to not reach requirement, is reached when by tonometry of the tensometer to cable wire
When less than requiring, rotate turnbuckle 302, connected by positive/negative thread so that turnbuckle component 3 length occur elongation or
Shorten, so that cable wire is tightened or loosens to have the function that adjust tension, to reach the tensile requirements of aviation cable wire.By
It is therefore learned in the aviation cable tension implementation platform of the utility model using the transmission system equal proportion production on civil aircraft
When institute trains, the more efficient study of energy is detected to the tension to aviation cable wire, and carries out the adjusting maintenance mans of cable tension
Make.In addition, setting turnbuckle component 3, the tune of cable tension can efficiently be realized very much by rotating turnbuckle 302 by tool
Section, to reach the tensile requirements of aviation cable wire.
Preferably, the centre of the turnbuckle 302, which goes out, is provided through mounting hole 304, mounting hole and turnbuckle phase
Perforation plays fuse after the tension adjustment of cable wire is complete in mounting hole 304, and two fuses are distinguished across mounting hole 304
It is welded with the first cable connector 301, the second cable connector 303, the other end of two fuses extends to outside 304 and knots, to rise
It is rotated to screw thread is prevented because of vibration, causes tension to change, when needing to adjust again, fuse is dismantled.
Preferably, the truck assembly 4 includes the first small wheel carrier 401, the second small wheel carrier 402, the first big wheel carrier 403, the
Two big wheel carriers 404, for the first big wheel carrier 403 with the second largest wheel carrier 404 at a distance of pre-determined distance, distance can be according to cable wire disk
The size design of component 2, to guarantee the stationarity of transmission, the pulley of the first big wheel carrier 403, the second largest wheel carrier 404
Equal vertical direction setting, the first big wheel carrier 403 is provided with the described first small wheel carrier 401 at left side, described second largest
Wheel carrier 404 is provided with the second small wheel carrier 402, the cunning of the first small wheel carrier 401, the second small wheel carrier 402 at left side
Take turns it is horizontally arranged, described second cable wire, 6 one end is connect with the cable wire disk component 2,6 other end of the second cable wire according to
It is secondary to pass through the second largest wheel carrier 404, the second small wheel carrier 402, the first small wheel carrier 401, the first big wheel carrier
403, it is connect with described second cable connector, 303 one end.It is big by the small wheel carrier 401 of setting first, the second small wheel carrier 402, first
Wheel carrier 403, the second largest wheel carrier 404 change the transmission side of cable wire 5, and cable wire 5 is in the first small wheel carrier 401 and the second small wheel carrier 402
Between transmission direction from transmission direction before on the contrary, to meet power output demand different on aircraft.
Preferably, the described first small wheel carrier 401, the second small wheel carrier 402, the first big wheel carrier 403, described second
Big top end face of the wheel carrier 404 with the desk 1 is connected by screw to, and facilitates the installation and removal of truck assembly.
Preferably, referring to Fig. 4, the cable wire disk component 2 includes pedestal 201, shaft 203, cable wire disk 204, adjustment arm
205, adjusting screw rod 207 are provided with the support plate 208 of horizontal direction, installation in the support plate 208 on the side wall of pedestal 201
There is bearing 202, the shaft 203 of vertical direction passes through the bearing 202, and is fixed on the inner ring of the bearing 202, described turn
The top of axis 203 is provided with the cable wire disk 204 of horizontal direction, and adjustment arm 205, institute have been disposed radially on the cable wire disk 204
It states adjustment 205 one end of arm to connect with 204 hinge of cable wire disk, be provided through on 205 other end of adjustment arm vertical anti-
To connecting hole 206, adjustment 205 middle of arm is provided through the threaded hole of horizontal direction, and adjusting screw rod 207 passes through institute
Threaded hole is stated, and is connected on the cable wire disk 204, the adjustment arm 205, the connecting hole 206, the adjusting screw rod 207
Another group of center line symmetrical setting about the cable wire disk 204.In order to prevent the thread damage of turnbuckle component it is stuck and
It can not work, cause cable tension that can not adjust, the application devises cable wire disk component, first cable connector 301 and institute
The connection of 5 one end of the first cable wire is stated, 5 other end of the first cable wire bypasses cable wire disk 204, is fixed across connecting hole 206, institute
The connecting hole 206 that 6 one end of the second cable wire is stated across another group is fixed, and 6 other end of the second cable wire bypasses cable wire disk
204, it is connect further around the excessively described truck assembly 4 with the second cable connector 303.When needing to adjust the tension of cable wire, pass through rotation
Adjust two screw rods 207 so that adjustment arm 205 is provided with an end position of connecting hole 206 and rotates, by cable wire tightening or
Loosen, equally play the role of adjusting the first cable wire 5 and two cable wires, 6 tension, and the tension on both sides is made to reach the shape of balance
State improves the reliability of aviation cable tension adjusting, and the probability for leading to failure can not be adjusted by reducing cable tension, improves boat
The safety that empty cable wire uses.
Preferably, through the first pin hole 209 of setting in the support plate 208, be provided through on the cable wire disk 204 with
Corresponding second pin hole 210 of first pin hole 209, when adjusting cable tension, the rotation of cable wire disk 204 in order to prevent,
Cable wire disk is fixed by being inserted into positioning pin in the first pin hole 209 and the second pin hole 210, to carry out the tune of cable tension
Section.
Preferably, the outside of the cable wire disk 204 is provided with protection board 211, described 211 one end of protection board and the cable wire
The connection of 204 hinge of disk, protection board 211 are able to rotate opening, are convenient for maintenance cleaning, and protection board 211 is closed for protecting cable wire
Personnel are hurt in the running.
In the description of the present invention, it should be understood that term " coaxial ", " bottom ", " one end ", " top ", " in
The orientation of the instructions such as portion ", " other end ", "upper", " side ", " top ", "inner", " front ", " center ", " both ends " or position are closed
System is to be based on the orientation or positional relationship shown in the drawings, and is merely for convenience of describing the present invention and simplifying the description, rather than
The device or element of indication or suggestion meaning must have a particular orientation, be constructed and operated in a specific orientation, therefore cannot
It is construed as a limitation of the present invention.
In addition, term " first ", " second ", " third ", " the 4th " are used for description purposes only, and should not be understood as instruction or
It implies relative importance or implicitly indicates the quantity of indicated technical characteristic, define " first ", " second ", " the as a result,
Three ", the feature of " the 4th " can explicitly or implicitly include at least one of the features.
In the present invention unless specifically defined or limited otherwise, term " installation ", " setting ", " connection ", " Gu
Calmly ", the terms such as " being screwed on " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integral；
It can be mechanical connection, be also possible to be electrically connected；It can be directly connected, can also indirectly connected through an intermediary, it can be with
It is the interaction relationship of the connection or two elements inside two elements, unless otherwise restricted clearly, for this field
For those of ordinary skill, the concrete meaning of above-mentioned term in the present invention can be understood as the case may be.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (7)
1. a kind of aviation cable tension implementation platform, it is characterised in that: including desk (1), cable wire disk component (2), turnbuckle
Component (3), truck assembly (4), the first cable wire (5), the second cable wire (6), pre-determined distance difference in interval on desk (1) top
The cable wire disk component (2), the truck assembly (4) are set, and the turnbuckle component (3) includes the first cable connector
(301), turnbuckle (302), the second cable connector (303), left end and first cable wire of the turnbuckle (302) connect
One end forward screw thread connection of head (301), the right end of the turnbuckle (302) and described second cable connector (303) one end
Reverse thread connection, the other end of first cable connector (301) are connect with described first cable wire (5) one end, and described first
Cable wire (5) other end is connect with the cable wire disk component (2), and described second cable wire (6) one end and the cable wire disk component (2) are even
It connects, the second cable wire (6) other end bypasses the truck assembly (4), and connects with the second cable connector (303) other end
It connects.
2. a kind of aviation cable tension implementation platform according to claim 1, it is characterised in that: the turnbuckle
(302) centre goes out to be provided through mounting hole (304).
3. a kind of aviation cable tension implementation platform according to claim 1, it is characterised in that: the truck assembly (4)
Including the first small wheel carrier (401), the second small wheel carrier (402), the first big wheel carrier (403), the second largest wheel carrier (404), described first
Big wheel carrier (403) and the second largest wheel carrier (404) are at a distance of pre-determined distance, the first big wheel carrier (403), second bull wheel
The equal vertical direction setting of the pulley of frame (404), the first big wheel carrier (403) are provided with the described first small wheel carrier at left side
(401), the second largest wheel carrier (404) is provided with the second small wheel carrier (402) at the left side, the first small wheel carrier (401),
The pulley of the second small wheel carrier (402) is horizontally arranged, described second cable wire (6) one end and the cable wire disk component
(2) connect, the second cable wire (6) other end sequentially pass through the second largest wheel carrier (404), the second small wheel carrier (402),
The first small wheel carrier (401), the first big wheel carrier (403), connect with described second cable connector (303) one end.
4. a kind of aviation cable tension implementation platform according to claim 3, it is characterised in that: the first small wheel carrier
(401), the described second small wheel carrier (402), the first big wheel carrier (403), the second largest wheel carrier (404) with the desk
(1) top end face is connected by screw to.
5. a kind of aviation cable tension implementation platform according to claim 1, it is characterised in that: the cable wire disk component
(2) include pedestal (201), shaft (203), cable wire disk (204), adjust arm (205), adjusting screw rod (207), pedestal (201)
It is provided with the support plate (208) of horizontal direction on side wall, bearing (202) are installed in the support plate (208), vertical direction
Shaft (203) passes through the bearing (202), and is fixed on the inner ring of the bearing (202), the top of the shaft (203)
It is provided with the cable wire disk (204) of horizontal direction, has been disposed radially adjustment arm (205), the adjustment on the cable wire disk (204)
Arm (205) one end is connect with cable wire disk (204) hinge, is provided through on adjustment arm (205) other end vertical anti-
To connecting hole (206), described adjustment arm (205) middle is provided through the threaded hole of horizontal direction, adjusting screw rod (207)
Across the threaded hole, and it is connected on the cable wire disk (204), it is the adjustment arm (205), the connecting hole (206), described
Another group of center line symmetrical setting about the cable wire disk (204) of adjusting screw rod (207).
6. a kind of aviation cable tension implementation platform according to claim 5, it is characterised in that: the support plate (208)
It is upper to run through setting the first pin hole (209), it is provided through on the cable wire disk (204) corresponding with the first pin hole (209)
The second pin hole (210).
7. a kind of aviation cable tension implementation platform according to claim 5, it is characterised in that: the cable wire disk (204)
Outside be provided with protection board (211), described protection board (211) one end is connect with cable wire disk (204) hinge.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822036349.7U CN209625508U (en) | 2018-12-06 | 2018-12-06 | A kind of aviation cable tension implementation platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822036349.7U CN209625508U (en) | 2018-12-06 | 2018-12-06 | A kind of aviation cable tension implementation platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209625508U true CN209625508U (en) | 2019-11-12 |
Family
ID=68445133
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822036349.7U Active CN209625508U (en) | 2018-12-06 | 2018-12-06 | A kind of aviation cable tension implementation platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209625508U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110920868A (en) * | 2019-11-19 | 2020-03-27 | 哈尔滨飞机工业集团有限责任公司 | Steering engine mounting device of automatic pilot |
| CN112102683A (en) * | 2020-10-22 | 2020-12-18 | 江苏无国界航空技术有限公司 | Simulation training platform for airplane transmission system |
-
2018
- 2018-12-06 CN CN201822036349.7U patent/CN209625508U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110920868A (en) * | 2019-11-19 | 2020-03-27 | 哈尔滨飞机工业集团有限责任公司 | Steering engine mounting device of automatic pilot |
| CN110920868B (en) * | 2019-11-19 | 2024-01-12 | 哈尔滨飞机工业集团有限责任公司 | Steering engine mounting device of automatic pilot |
| CN112102683A (en) * | 2020-10-22 | 2020-12-18 | 江苏无国界航空技术有限公司 | Simulation training platform for airplane transmission system |
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Effective date of registration: 20231219 Address after: No. 339 Zhannan Avenue, Urban Rural Integration Demonstration Zone, Anyang City, Henan Province, 455100 Patentee after: Henan Jinyu Aviation Technology Co.,Ltd. Address before: 710071 room 101-102, No. 16, zhangba'er Road, high tech Zone, Xi'an, Shaanxi Province Patentee before: XI'AN GOLDENPOOL TECHNOLOGY ENGINEERING Co.,Ltd. |