CN208812037U - A kind of aircraft engine maintenance support bar component - Google Patents
A kind of aircraft engine maintenance support bar component Download PDFInfo
- Publication number
- CN208812037U CN208812037U CN201821389192.XU CN201821389192U CN208812037U CN 208812037 U CN208812037 U CN 208812037U CN 201821389192 U CN201821389192 U CN 201821389192U CN 208812037 U CN208812037 U CN 208812037U
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- Prior art keywords
- aircraft engine
- bar component
- width
- magnet
- fixedly installed
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Abstract
The utility model relates to support frame technical fields, and disclose a kind of aircraft engine maintenance support bar component, including bottom plate, the inside of bottom plate is fixedly installed with main turbine rod, the two sides of main turbine rod are fixedly installed with symmetrical secondary turbine rod, connecting plate is fixedly connected on the top of main turbine rod and secondary turbine rod, the two sides of connecting plate upper surface are connected with sliding panel, the upper surface of sliding panel is fixedly connected with slideway, runner is connected in slideway, the upper surface of set casing is fixedly installed with fixed block, and the top of fixed block is fixedly installed with fixed link.The aircraft engine maintenance supports bar component, the identical movable disk of two sizes is driven by conveyer belt, sliding panel can be allowed to draw close to centre, width can be changed by slideway, by the magnet of two identical magnetic poles, mutually exclusive principle, along with spring buffers, avoidable engine is placed on maintenance rig, and rigid collision occurs.
Description
Technical field
The utility model relates to support frame technical field, specially a kind of aircraft engine maintenance supports bar component.
Background technique
Aeronautical maintenance refers to the maintenance and repair that technical equipment to aircraft and thereon carries out, it is ensured that the peace of aircraft
Entirely, aeronautical maintenance is the important component of premise and necessary condition and aircraft industry that aircraft uses.And aero-engine
It is the heart of aircraft, aircraft engine maintenance is both a part of aircraft maintenance and the important component of aviation work,
But in existing technology, aircraft engine maintenance, cannot front and back or left in the maintenance support bar that uses and not convenient enough
It moves right, brings great inconvenience, waste of manpower and cost in maintenance engine to aviation staff.
Utility model content
(1) the technical issues of solving
In view of the deficiencies of the prior art, the utility model provides a kind of aircraft engine maintenance support bar component, has
The advantages that can all around moving, solves aircraft engine maintenance in the maintenance support bar and not convenient enough, Bu Nengqian used
It afterwards or moves left and right, brings great inconvenience in maintenance engine to aviation staff, waste of manpower and cost are asked
Topic.
(2) technical solution
Used to realize above-mentioned aircraft engine maintenance the maintenance support bar used is convenient, can front and back or left and right move
The purpose of moving, saving manpower and cost, the utility model provides the following technical solutions: a kind of aircraft engine maintenance support rod structure
Part, including bottom plate, the inside of the bottom plate are fixedly installed with main turbine rod, and the two sides of main turbine rod are fixedly installed with symmetrical pair
Turbine rod is fixedly connected with connecting plate on the top of main turbine rod and secondary turbine rod, and the activity of the two sides of connecting rod upper surface is even
It is connected to sliding panel, the upper surface of sliding panel is fixedly connected with slideway, runner is connected in slideway, runner is by extending transversely through
Motion bar be fixedly connected with the set casing being installed on outside slideway, the upper surface of set casing is fixedly installed with fixed block, fixed
The top of block is fixedly installed with fixed link, and the side of fixed link offers inside groove, and two opposite inside grooves pass through activity disk activity
Be connected with support frame, be fixedly installed with support plate in the fixed link on the downside of support frame, the lower surface of support plate by support column with
The side of fixed link is fixedly mounted, and the lower end of support frame as described above and the upper end of support plate are fixedly installed with magnet, and two
It is connected between magnet by spring, the inner cavity of the connecting plate is movably installed with conveyer belt, and the teeth of conveyer belt are engaged with
Positioned at the fixation turntable of connection board ends, the conveyer belt internal messing between fixed turntable has movable disk, the axle center of movable disk
Place is connected with connecting rod, and the top of connecting rod is fixedly connected through connecting plate and with sliding panel.
Preferably, the size of described two movable disks is equal, and driving gear disc is provided in the middle part of conveyer belt,
And the turntable outside connecting plate is fixedly connected at the axle center of driving gear disc, there are two conveyer belt settings, and conveyer belt is equal
It is flexibly connected with driving gear disc.
Preferably, the upper surface of the connecting plate offers notch, and the notch diameter of inside groove is greater than the diameter of connecting rod, and
No more than the diameter of sliding panel.
Preferably, described two magnet, magnetic pole is identical, and magnet is equal in magnitude, and magnet width is 30cm, a length of 40cm of magnet.
Preferably, the width of the inside groove is greater than the width of movable disk, and the width of notch is greater than the connection of movable disk connection
The width of block and the width for being not more than support frame.
Preferably, outer course slot is provided on the outside of the slideway, set casing is sticked in outer course slot, set casing and outer course slot
Scope of activities distance at engaging is no more than 5 millimeters.
Preferably, the lower surface size of support frame as described above lower surface, the upper surface of support plate and magnet is equal, support frame
It is 30cm with support plate width.
(3) beneficial effect
Compared with prior art, the utility model provides a kind of aircraft engine maintenance support bar component, has following
The utility model has the advantages that
1, the aircraft engine maintenance supports bar component, drives the identical movable disk of two sizes by conveyer belt, can
To allow sliding panel to draw close to centre, width can be changed by slideway, by the magnet of two identical magnetic poles, mutually exclusive original
Reason, along with spring buffers, avoidable engine is placed on maintenance rig, and rigid collision occurs, rigid contact is changed into soft
Property contact, avoid engine damage.
2, the aircraft engine maintenance supports bar component, and the height of maintenance rig can be changed by main turbine rod and secondary turbine rod
Degree, avoids when repairing engine, and since height cannot change, maintenance personal can not tie up specified position
It repairs, changes height and facilitate maintenance of the maintenance personal to machine.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is enlarged diagram at A in the utility model Fig. 1；
Fig. 3 is the utility model conveyer belt schematic top plan view.
In figure: 1 bottom plate, 2 main turbine rods, 3 secondary turbine rods, 4 connecting plates, 5 sliding panels, 6 slideways, 7 runners, 8 motion bars, 9
Set casing, 10 fixed blocks, 11 fixed links, 12 inside grooves, 13 movable disks, 14 support frames, 15 support plates, 16 magnet, 17 springs, 18
Dagger, 19 conveyer belts, 20 fixed turntables, 21 movable disks, 22 connecting rods.
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.
Please refer to Fig. 1-3, a kind of aircraft engine maintenance support bar component, including bottom plate 1, the fixed peace in the inside of bottom plate 1
Equipped with main turbine rod 2, the two sides of main turbine rod 2 are fixedly installed with symmetrical secondary turbine rod 3, in main turbine rod 2 and secondary turbine rod 3
Top be fixedly connected with connecting plate 4, the height of maintenance rig can be changed by main turbine rod 2 and secondary turbine rod 3, avoid and tieing up
When the motivation that trims the hair, since height cannot change, maintenance personal can not repair specified position, and it is convenient to change height
Maintenance of the maintenance personal to machine, the upper surface of connecting plate 4 offer notch, and the diameter of notch is greater than the straight of connecting rod 22
Diameter, and it is not more than the diameter of sliding panel 5, the two sides of 4 upper surface of connecting plate are connected with sliding panel 5, the upper table of sliding panel 5
Face is fixedly connected with slideway 6, and the outside of slideway 6 is provided with outer course slot, and set casing 9 is sticked in outer course slot, set casing 9 and outer course
Scope of activities distance at slot engaging is no more than 5 millimeters, and runner 7 is connected in slideway 6, and runner 7 is mainly convenient in cunning
It is moved on road 6, runner 7 passes through the motion bar 8 extended transversely through and is fixedly connected with the set casing 9 being installed on outside slideway 6, set casing
9 upper surface is fixedly installed with fixed block 10, and fixed block 10 are played transition connection, and the top of fixed block 10 is fixedly mounted
There is fixed link 11, the side of fixed link 11 offers inside groove 12, and inside groove 12 is primarily to engine when vibration, supports
Frame 14 can generate elastic potential energy therewith down, protect machine, and the width of inside groove 12 is greater than the width of movable disk 13, inside groove 12
Width of rebate be greater than movable disk 13 connect link block width and be not more than support frame 14 width, two opposite inside grooves
Support frame 14 is connected with by movable disk 13 in 12, support frame 14 mainly supports engine, engine is allowed to be placed on above,
The lower surface size of 14 lower surface of support frame, the upper surface of support plate 15 and magnet 16 is equal, and support frame 14, support plate 15 are wide
It is 30cm, a length of 40cm of magnet 16 is fixedly installed with support plate 15 in the fixed link 11 of 14 downside of support frame, support plate 15
Lower surface is fixedly mounted by the side of support column 18 and fixed link 11, and support column 18 is mainly fixed support plate 15, support frame
14 lower end and the upper end of support plate 15 are fixedly installed with magnet 16, and the magnetic pole of two magnet 16 is identical, identical by two
Magnetic pole magnet 16, mutually exclusive principle, along with spring 17 buffers, avoidable engine is placed on maintenance rig, hair
Raw rigid collision, is changed into flexible contact for rigid contact, avoids engine damage, magnet 16 is equal in magnitude, and 16 width of magnet is
30cm, and by 17 elastic connection of spring between two magnet 16, the inner cavity of connecting plate 4 is movably installed with conveyer belt 19, passes
It send the teeth of band 19 to be engaged with the fixation turntable 20 positioned at 4 both ends of connecting plate, drives two sizes identical by conveyer belt 19
Movable disk 21 can allow sliding panel 5 to be drawn close to centre, change width, can be changed width by slideway 6, fixed turntable 20 it
Between 19 internal messing of conveyer belt have and be connected with connecting rod 22 at the axle center of 21 movable disk 21 of movable disk, two activities turn
The size of disk 21 is equal, and the middle part of conveyer belt 19 is provided with driving gear disc, and fixed company at the axle center of driving gear disc
It is connected to the turntable being located at outside connecting plate 4, there are two the settings of conveyer belt 19, and conveyer belt 19 is flexibly connected with driving gear disc,
The top of connecting rod 22 is fixedly connected through connecting plate 4 and with sliding panel 5.
In conclusion the aircraft engine maintenance supports bar component, the identical work of two sizes is driven by conveyer belt 19
Turn disk 21 can allow sliding panel 5 to be drawn close to centre, and width can be changed by slideway 6, pass through the magnet of two identical magnetic poles
16, mutually exclusive principle, along with spring 17 buffers, avoidable engine is placed on maintenance rig, and rigid collision occurs, will
Rigid contact is changed into flexible contact, avoids engine damage.Maintenance rig can be changed by main turbine rod 2 and secondary turbine rod 3
Highly, it avoids when repairing engine, since height cannot change, maintenance personal can not tie up specified position
It repairs, changes height and facilitate maintenance of the maintenance personal to machine.
It should be noted that, in this document, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also including other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.In the absence of more restrictions, the element limited by sentence "including a ...", it is not excluded that
There is also other identical elements in process, method, article or equipment including the element.
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 aircraft engine maintenance supports bar component, including bottom plate (1), it is characterised in that: the inside of the bottom plate (1) is solid
Dingan County is equipped with main turbine rod (2), and the two sides of main turbine rod (2) are fixedly installed with symmetrical secondary turbine rod (3), in main turbine rod
(2) it is fixedly connected with connecting plate (4) with the top of secondary turbine rod (3), the two sides of connecting plate (4) upper surface are connected with cunning
Movable plate (5), the upper surface of sliding panel (5) are fixedly connected with slideway (6), are connected with runner (7) in slideway (6), runner (7)
It is fixedly connected by the motion bar (8) extended transversely through the set casing (9) external with slideway (6) is installed on, the upper table of set casing (9)
Face is fixedly installed with fixed block (10), and the top of fixed block (10) is fixedly installed with fixed link (11), the side of fixed link (11)
It offers inside groove (12), is connected with support frame (14), support frame by movable disk (13) in two opposite inside grooves (12)
(14) be fixedly installed with support plate (15) in the fixed link (11) on the downside of, the lower surface of support plate (15) by support column (18) with
The side of fixed link (11) is fixedly mounted, and the lower end of support frame as described above (14) and the upper end of support plate (15) are fixedly installed with magnetic
Iron (16), and by spring (17) elastic connection between two magnet (16), the inner cavity of the connecting plate (4) is movably installed with
Conveyer belt (19), the teeth of conveyer belt (19) are engaged with the fixation turntable (20) positioned at connecting plate (4) both ends, fixed turntable (20)
Between conveyer belt (19) internal messing have and be connected with connecting rod (22) at the axle center of movable disk (21) movable disk (21),
The top of connecting rod (22) is fixedly connected through connecting plate (4) and with sliding panel (5).
2. a kind of aircraft engine maintenance according to claim 1 supports bar component, it is characterised in that: described two activities
The size of turntable (21) is equal, and is provided with driving gear disc in the middle part of conveyer belt (19), and at the axle center of driving gear disc
It is fixedly connected with and is located at connecting plate (4) external turntable, there are two conveyer belt (19) settings, and conveyer belt (19) is and driving tooth
Disk activity connection.
3. a kind of aircraft engine maintenance according to claim 1 supports bar component, it is characterised in that: the connecting plate
(4) upper surface offers notch, and the diameter of notch is greater than the diameter of connecting rod (22), and is not more than the diameter of sliding panel (5).
4. a kind of aircraft engine maintenance according to claim 1 supports bar component, it is characterised in that: described two magnet
(16) magnetic pole is identical, and magnet (16) is equal in magnitude, and magnet (16) width is 30cm, magnet (16) a length of 40cm.
5. a kind of aircraft engine maintenance according to claim 1 supports bar component, it is characterised in that: the inside groove (12)
Width be greater than the width of movable disk (13), the width of rebate of inside groove (12) is greater than the width of the link block of movable disk (13) connection
And it is not more than the width of support frame (14).
6. a kind of aircraft engine maintenance according to claim 1 supports bar component, it is characterised in that: the slideway (6)
Outside be provided with outer course slot, set casing (9) is sticked in outer course slot, and set casing (9) engages the scope of activities at place with outer course slot
Distance is no more than 5 millimeters.
7. a kind of aircraft engine maintenance according to claim 1 supports bar component, it is characterised in that: support frame as described above
(14) the lower surface size of lower surface, the upper surface of support plate (15) and magnet (16) is equal, support frame (14) and support plate
(15) width is 30cm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821389192.XU CN208812037U (en) | 2018-08-28 | 2018-08-28 | A kind of aircraft engine maintenance support bar component |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821389192.XU CN208812037U (en) | 2018-08-28 | 2018-08-28 | A kind of aircraft engine maintenance support bar component |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208812037U true CN208812037U (en) | 2019-05-03 |
Family
ID=66274753
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821389192.XU Expired - Fee Related CN208812037U (en) | 2018-08-28 | 2018-08-28 | A kind of aircraft engine maintenance support bar component |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208812037U (en) |
-
2018
- 2018-08-28 CN CN201821389192.XU patent/CN208812037U/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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190503 Termination date: 20210828 |