CN212832510U - Equipment fixing hanger for aircraft maintenance - Google Patents
Equipment fixing hanger for aircraft maintenance Download PDFInfo
- Publication number
- CN212832510U CN212832510U CN202021786425.7U CN202021786425U CN212832510U CN 212832510 U CN212832510 U CN 212832510U CN 202021786425 U CN202021786425 U CN 202021786425U CN 212832510 U CN212832510 U CN 212832510U
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- China
- Prior art keywords
- gear
- rod
- motor
- movably connected
- fixedly connected
- Prior art date
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- Expired - Fee Related
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- 238000012423 maintenance Methods 0.000 title claims abstract description 26
- 238000004804 winding Methods 0.000 claims description 22
- 230000005540 biological transmission Effects 0.000 claims description 10
- 230000000903 blocking effect Effects 0.000 claims description 5
- 230000000694 effects Effects 0.000 abstract description 7
- 238000005096 rolling process Methods 0.000 abstract 1
- 238000000926 separation method Methods 0.000 abstract 1
- 230000001174 ascending effect Effects 0.000 description 3
- 238000009434 installation Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004883 computer application Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
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Abstract
The utility model discloses an equipment fixing gallows for aircraft maintenance, including roof, bracing piece and cross mount, the upper surface of roof is provided with the motor, the output swing joint of motor has the transfer line, the one end swing joint of transfer line has first gear, one side meshing of first gear has the second gear, the middle part swing joint of second gear has the connecting rod, the one end swing joint of connecting rod has the third gear, and one side meshing of third gear has the fourth gear. This equipment fixing gallows for aircraft maintenance through the setting of supporting leg frame, has improved the contact surface of bracing piece with ground, has improved the device's stability, through the setting of motor bracket, has played the effect of fixed motor, through the setting of slipmat, has increased the equipment part for aircraft maintenance and the frictional force of layer board, has prevented the part landing, through the setting of spacing separation blade, when having prevented that the coiling stick is the rolling function to the stay cord, the stay cord breaks away from the coiling stick.
Description
Technical Field
The utility model relates to an aircraft electromechanical maintenance technical field specifically is an equipment fixing gallows for aircraft maintenance.
Background
The maintenance of the aircraft electromechanical equipment is a work with high requirement on professional knowledge and strong technical performance, and the theoretical knowledge learned by students in the major is arranged according to the principle of 'must and sufficient', so that the English ability and the computer application ability are emphasized, and the practical ability is emphasized to meet the requirement of the aircraft work of the air transportation enterprise.
The aircraft need use the installation gallows when the maintenance, but current installation gallows adjusting device part height effect is relatively poor, and stability is relatively poor, consequently the utility model provides an equipment fixing gallows for aircraft maintenance.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
Not enough to prior art, the utility model provides an equipment fixing gallows for aircraft maintenance has solved the problem of proposing among the above-mentioned background art.
(II) technical scheme
In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: an equipment mounting hanger for aircraft maintenance comprises a top plate, a support rod and a cross fixing frame, wherein a motor is arranged on the upper surface of the top plate, an output end of the motor is movably connected with a transmission rod, one end of the transmission rod is movably connected with a first gear, one side of the first gear is meshed with a second gear, the middle of the second gear is movably connected with a connecting rod, one end of the connecting rod is movably connected with a third gear, one side of the third gear is meshed with a fourth gear, the middle of the fourth gear is movably connected with a rotating rod, the surface of the rotating rod is movably connected with a winding rod, a pull rope is arranged on the surface of the winding rod, one end of the pull rope is fixedly connected with a hanging ring, a hanging buckle is lapped on the inner side wall of the hanging ring, the bottom of the hanging buckle is fixedly connected with the cross fixing frame, and the bottom of the, the bottom of the top plate is fixedly connected with a supporting rod.
Optionally, the bottom of the supporting rod is fixedly connected with a fixing block, and the bottom of the fixing block is fixedly connected with a supporting foot frame.
Optionally, a motor bracket is lapped at the bottom of the motor, and anti-skid patterns are arranged on the inner side wall of the motor bracket.
Optionally, both ends of the rotating rod are movably connected with bearing seats.
Optionally, the middle part of the supporting plate is provided with a non-slip mat, and the thickness of the non-slip mat is three millimeters.
Optionally, both ends of the winding bar are movably connected with limiting blocking pieces.
(III) advantageous effects
The utility model provides an equipment fixing gallows for aircraft maintenance possesses following beneficial effect:
the equipment mounting hanger for airplane maintenance is characterized in that through the arrangement of a motor, a stay cord and a cross fixing frame, an operator places equipment parts for airplane maintenance on a supporting plate, when the hanger is used, the motor is externally connected with a power supply, a transmission rod drives a first gear to rotate, the rotation of the first gear drives a second gear to rotate, a third gear drives a fourth gear to rotate, a winding rod on the surface of a rotating rod drives the stay cord to wind through the rotation of the fourth gear, the cross fixing frame drives the supporting plate to ascend or descend through the winding of the stay cord, so that the effect of adjusting the ascending or descending of the equipment parts for airplane maintenance on the supporting plate is achieved, the operation of the operator is facilitated, through the arrangement of a supporting foot rest, the contact surface of the supporting rod and the ground is improved, the stability of the device is improved, through the arrangement of a motor bracket, the function of fixing the motor is achieved, through the arrangement of an anti-, the friction force between the equipment parts for aircraft maintenance and the supporting plate is increased, the parts are prevented from sliding off, and the stay cord is prevented from being separated from the winding bar when the winding bar is used for winding the stay cord through the arrangement of the limiting blocking piece.
Drawings
FIG. 1 is a perspective view of the present invention;
FIG. 2 is a sectional view of the structure of the present invention;
fig. 3 is an enlarged schematic view of a position a in the first drawing of the present invention.
In the figure: 1. a top plate; 2. a support bar; 3. a cross-shaped fixing frame; 4. a motor; 5. a transmission rod; 6. a first gear; 7. a connecting rod; 8. a third gear; 9. a fourth gear; 10. a rotating rod; 11. winding a wire rod; 12. Pulling a rope; 13. hanging a ring; 14. hanging and buckling; 15. fixing the rod; 16. a support plate; 17. a second gear; 18. A supporting foot rest; 19. a motor bracket; 20. a bearing seat; 21. a non-slip mat; 22. a limiting baffle plate.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
Referring to fig. 1 to 3, the present invention provides a technical solution: an equipment mounting hanger for aircraft maintenance comprises a top plate 1, the device comprises a supporting rod 2 and a cross fixing frame 3, wherein a motor 4 is arranged on the upper surface of a top plate 1, an output end of the motor 4 is movably connected with a transmission rod 5, one end of the transmission rod 5 is movably connected with a first gear 6, one side of the first gear 6 is meshed with a second gear 17, the middle part of the second gear 17 is movably connected with a connecting rod 7, one end of the connecting rod 7 is movably connected with a third gear 8, one side of the third gear 8 is meshed with a fourth gear 9, the middle part of the fourth gear 9 is movably connected with a rotating rod 10, the surface of the rotating rod 10 is movably connected with a winding rod 11, a pull rope 12 is arranged on the surface of the winding rod 11, one end of the pull rope 12 is fixedly connected with a hanging ring 13, a hanging buckle 14 is lapped on the inner side wall of the hanging ring 13, the bottom of the hanging buckle 14;
through the arrangement of the motor 4, the pull rope 12 and the cross fixing frame 3, a worker places equipment parts for aircraft maintenance on the supporting plate 16, when the aircraft maintenance device is used, the motor 4 is externally connected with a power supply, the transmission rod 5 drives the first gear 6 to rotate, the rotation of the first gear 6 enables the second gear 17 to drive the third gear 8 to rotate, the third gear 8 drives the fourth gear 9 to rotate, the rotation of the fourth gear 9 enables the winding rod 11 on the surface of the rotating rod 10 to drive the pull rope 12 to wind, and the winding of the pull rope 12 enables the cross fixing frame 3 to drive the supporting plate 16 to ascend, so that the effect of adjusting ascending or descending of the equipment parts for aircraft maintenance on the supporting plate 16 is achieved, and the operation of the worker is facilitated;
the bottom of the top plate 1 is fixedly connected with a supporting rod 2, the bottom of the supporting rod 2 is fixedly connected with a fixed block, the bottom of the fixed block is fixedly connected with a supporting foot frame 18, the contact surface of the supporting rod 2 and the ground is improved through the arrangement of the supporting foot frame 18, the stability of the device is improved, the bottom of the motor 4 is lapped with a motor bracket 19, the effect of fixing the motor 4 is achieved through the arrangement of the motor bracket 19, the inner side wall of the motor bracket 19 is provided with anti-skid patterns, both ends of the rotating rod 10 are movably connected with bearing seats 20, the middle part of the supporting plate 16 is provided with an anti-skid pad 21, the thickness of the anti-skid pad 21 is three millimeters, the friction force between equipment parts for aircraft maintenance and the supporting plate 16 is increased through the arrangement of the anti-skid pad 21, the parts are prevented from slipping off, both ends of the winding rod 11 are movably connected with limiting blocking pieces 22, and through, the pull cord 12 is disengaged from the winding bar 11.
The electrical components presented in the document are all electrically connected with an external master controller and 220V mains, and the master controller can be a conventional known device controlled by a computer or the like.
The utility model discloses in, the device's working procedure as follows:
1. the motor 4, the pull rope 12 and the cross fixing frame 3 are matched for work, a worker places equipment parts for airplane maintenance on the supporting plate 16, when the device is used, the motor 4 is externally connected with a power supply, the transmission rod 5 drives the first gear 6 to rotate, the second gear 17 drives the third gear 8 to rotate due to the rotation of the first gear 6, the third gear 8 drives the fourth gear 9 to rotate, the winding rod 11 on the surface of the rotating rod 10 drives the pull rope 12 to wind due to the rotation of the fourth gear 9, the cross fixing frame 3 drives the supporting plate 16 to ascend due to the winding of the pull rope 12, and therefore the effect of adjusting ascending or descending of the equipment parts for airplane maintenance on the supporting plate 16 is achieved, and the operation of the worker is facilitated;
2. the supporting foot rest 18 works, so that the contact surface of the supporting rod 2 and the ground is improved, and the stability of the device is improved;
3. the motor bracket 19 works to fix the motor 4;
4. the friction force between equipment parts for airplane maintenance and the supporting plate 16 is increased by the operation of the anti-slip pad 21, and the parts are prevented from slipping;
5. the limiting blocking piece 22 works to prevent the pull rope 12 from separating from the winding rod 11 when the winding rod 11 winds the pull rope 12.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (6)
1. The utility model provides an equipment fixing gallows is used in aircraft maintenance, includes roof (1), bracing piece (2) and cross mount (3), its characterized in that: the upper surface of the top plate (1) is provided with a motor (4), the output end of the motor (4) is movably connected with a transmission rod (5), one end of the transmission rod (5) is movably connected with a first gear (6), one side of the first gear (6) is meshed with a second gear (17), the middle part of the second gear (17) is movably connected with a connecting rod (7), one end of the connecting rod (7) is movably connected with a third gear (8), one side of the third gear (8) is meshed with a fourth gear (9), the middle part of the fourth gear (9) is movably connected with a rotating rod (10), the surface of the rotating rod (10) is movably connected with a winding rod (11), the surface of the winding rod (11) is provided with a pull rope (12), one end of the pull rope (12) is fixedly connected with a hanging ring (13), and a hanging buckle (14) is lapped on the inner side wall of the hanging ring (13), the bottom of the hanging buckle (14) is fixedly connected with a cross fixing frame (3), the bottom of the cross fixing frame (3) is fixedly connected with a supporting plate (16) through a fixing rod (15), and the bottom of the top plate (1) is fixedly connected with a supporting rod (2).
2. An aircraft servicing equipment mounting hanger as claimed in claim 1 in which: the bottom of the supporting rod (2) is fixedly connected with a fixing block, and the bottom of the fixing block is fixedly connected with a supporting foot frame (18).
3. An aircraft servicing equipment mounting hanger as claimed in claim 1 in which: the bottom of motor (4) overlap joint has motor bracket (19), the inside wall of motor bracket (19) is provided with anti-skidding decorative pattern.
4. An aircraft servicing equipment mounting hanger as claimed in claim 1 in which: and both ends of the rotating rod (10) are movably connected with bearing seats (20).
5. An aircraft servicing equipment mounting hanger as claimed in claim 1 in which: the middle part of the supporting plate (16) is provided with a non-slip pad (21), and the thickness of the non-slip pad (21) is three millimeters.
6. An aircraft servicing equipment mounting hanger as claimed in claim 1 in which: both ends of the winding bar (11) are movably connected with limiting blocking pieces (22).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021786425.7U CN212832510U (en) | 2020-08-25 | 2020-08-25 | Equipment fixing hanger for aircraft maintenance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021786425.7U CN212832510U (en) | 2020-08-25 | 2020-08-25 | Equipment fixing hanger for aircraft maintenance |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212832510U true CN212832510U (en) | 2021-03-30 |
Family
ID=75140767
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021786425.7U Expired - Fee Related CN212832510U (en) | 2020-08-25 | 2020-08-25 | Equipment fixing hanger for aircraft maintenance |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212832510U (en) |
-
2020
- 2020-08-25 CN CN202021786425.7U patent/CN212832510U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210330 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |