CN209246924U - A kind of measurement auxiliary mould for survey aircraft covering bumps degree - Google Patents
A kind of measurement auxiliary mould for survey aircraft covering bumps degree Download PDFInfo
- Publication number
- CN209246924U CN209246924U CN201920029000.2U CN201920029000U CN209246924U CN 209246924 U CN209246924 U CN 209246924U CN 201920029000 U CN201920029000 U CN 201920029000U CN 209246924 U CN209246924 U CN 209246924U
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- China
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- sliding rail
- slider
- screw
- probe
- groove
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- Length-Measuring Instruments Using Mechanical Means (AREA)
- A Measuring Device Byusing Mechanical Method (AREA)
Abstract
A kind of measurement auxiliary mould for survey aircraft covering bumps degree, it pushes sliding rail to slide along guide rod and realizes that driving depth gauge slides along the longitudinal direction, by pushing slider I to slide by groove II along sliding rail left and right directions, it is slided in left-right direction to realize driving depth gauge, pass through the sliding of depth gauge front-rear direction and left and right directions, probe is set to be moved to the minimum point of aircraft skin recess or the highest point position of aircraft skin protrusion, probe actuation probe rod moves along the vertical direction, so that numerical value can be read by depth gauge.By rotating change, by sliding slider II make indicator slide into positioned at nearest notch perhaps fastener row top by read the scale on measuring scale it can be learnt that recess or protrusion edge and the distance between nearest notch or at a distance from arranging with nearest fastener.The precision of measurement and the convenience of operation are improved, measurement efficiency is improved.
Description
Technical field
The utility model relates to aircraft maintenance measuring tool fields, and in particular to one kind is used for survey aircraft covering bumps journey
The measurement auxiliary mould of degree.
Background technique
Air Passenger A320 series aircraft is larger due to bearing load during operation, separately there is the originals such as burn into foreign object strike
Cause, fuselage skin are often subject to damage, therefore can often have fuselage skin repair work in regular inspection.The pit or protrusion of covering
It is the common phenomenon of covering damage, determines whether pit or protrusion damage need to be further processed, it is also necessary to measures a fixed number
According to carrying out calculating analysis.Needed when handling Notch damage survey aircraft covering dent depth capacity be dent edge and recently
The distance between notch or or nearest fastener row distance, but existing tool only can confirm that aircraft skin dent
Depth capacity, then using distance between other rulers measurement dent edges and nearest notch or or nearest instead
The distance of fastener row, will affect the accuracy of measurement in this way, cause measurement result inaccurate.If in measurement damage data
When, it can be devoted a tremendous amount of time to reach measurement accuracy, cause the decline of efficiency.When measuring covering protrusion, data analysis
Principle and covering recess, but the practical tool due to not can be used for measuring height of projection at this stage, this protrusion
The measurement of damage needs on the inside of covering to measure, this will need to remove a large amount of aircraft interior parts, such as floor, side wall
Plate and some associated components, therefore a large amount of extra workloads are caused, some protrusions are damaged locating department and are tied if it is beam, rib etc.
It will be more difficult to measurement at structure, error in judgement is in turn resulted in.
Summary of the invention
The utility model in order to overcome the shortcomings of the above technology, provide a kind of raising survey aircraft covering height of projection and
The measurement auxiliary mould for survey aircraft covering bumps degree of cup depth accuracy and efficiency.
The utility model overcomes the technical solution used by its technical problem to be:
A kind of measurement auxiliary mould for survey aircraft covering bumps degree, comprising:
Two support bases are located at left and right ends, and groove I is provided in two support bases, and the groove I is interior along front and back
Direction is horizontally disposed guide rod；
Sliding rail is horizontally disposed in left-right direction, and the left side of sliding rail is located in the groove I of the support base of left-hand end and it is slided
It is installed on the guide rod in the groove I, the right side of sliding rail is located in the groove I of the support base of right-hand end and it is slidably mounted on this
On guide rod in groove I；
Block is placed in the top of sliding rail, and slider I is located at the lower section of sliding rail, is provided in the slider I and sliding rail matching
Groove II, slider I are plugged in sliding rail by groove II sliding, and slider I is connected and fixed with block by screw II；
Bracket, the upper end are equipped with depth gauge by screw I, and the pedestal lower end is provided with shaft, and the lower end of shaft is
Thread segment II is provided with the screw hole I to match with thread segment II in the block, and thread segment II is combined in screw hole I；
Change is rotatablely installed in shaft, and horizontally disposed measuring scale is connected with change, square along its length on measuring scale
To being provided with scale；
Sliding block II, for sliding sleeve loaded on measuring scale, the lower end of sliding block II is equipped with indicator along the vertical direction；And
Probe, is set to the lower end of slider I, the probe rod of depth gauge sequentially pass through after bracket, block and slider I with probe
It is coaxially connected.
It further include being set to support base upper end and the long hole parallel with guide rod and holding screw I to realize locking,
The holding screw I passes through long hole back spin together on sliding rail, and the head of screw of holding screw I is in contact with the upper surface of support base.
It further include the screw hole II being set in slider I, the axis of the screw hole II and the length of sliding rail to realize locking
Direction is perpendicular, and holding screw II is combined in screw hole II, and the tail end of holding screw II is in contact with sliding rail.
It further include the holding screw III being combined on sliding block II along the vertical direction, the holding screw to realize locking
III tail end is in contact with measuring scale.
It further include the nut for being set to the thread segment I of shaft upper end and being combined on thread segment I to realize locking,
The lower end surface of the nut is in contact with the upper surface of change.
It further include several section extension rods for the ease of measuring the recess of different depth, each extension rod is coaxially connected, connection
Several extension rod upper ends afterwards are coaxially connected with probe rod, and lower end is coaxially connected with probe.
It further include the stabilizer blade for being respectively arranged at support base lower end front and rear sides in order to facilitate support.
For ease of operation, handle is provided on above-mentioned nut.
The beneficial effects of the utility model are: pushing sliding rail to slide along guide rod realizes that driving depth gauge is slided along the longitudinal direction
It is dynamic, by pushing slider I to slide by groove II along sliding rail left and right directions, slided in left-right direction to realize driving depth gauge
It is dynamic, by the sliding of depth gauge front-rear direction and left and right directions, probe is made to be moved to the minimum point or aircraft of aircraft skin recess
The highest point position of covering protrusion, probe actuation probe rod move along the vertical direction, so that numerical value can be read by depth gauge.
By rotating change, make notch or the fastener row's that measuring scale drives indicator to be rocked to and be recessed or raised brim is nearest
Direction makes indicator slide into the top positioned at nearest notch or fastener row, passes through reading by sliding slider II later
Take the scale on measuring scale it can be learnt that the edge and the distance between nearest notch of recess or protrusion or with it is nearest tight
The distance of firmware row.The precision of measurement and the convenience of operation are improved, measurement efficiency is improved.
Detailed description of the invention
Fig. 1 is the schematic perspective view of the utility model；
Fig. 2 is the exploded perspective structural schematic diagram of the utility model.
In figure, 1. support base, 2. groove I, 3. guide rod, 4. long hole, 5. sliding rail, 6. holding screw, I 7. block, 8. screw hole I
9. 15. thread segment of bracket 10. depth gauge, 11. screw, I 12. probe rod, 13. thread segment, I 14. shaft, II 16. nut
17. II 22. holding screw of handle 18. change, 19. slider I, 20. groove II, 21. screw hole, II 23. screw II 24. extends
III 29. indicator of bar 25. probe, 26. measuring scale, 27. sliding block, II 28. holding screw, 30. stabilizer blade.
Specific embodiment
With reference to the accompanying drawing 1, attached drawing 2 is described further the utility model.
A kind of measurement auxiliary mould for survey aircraft covering bumps degree, comprising: two support bases 1 are located at
Left and right ends are provided with groove I 2 in two support bases 1, and being horizontally disposed with along the longitudinal direction in groove I 2 has guide rod 3；Sliding rail 5,
It is horizontally disposed in left-right direction, the left side of sliding rail 5 is located in the groove I 2 of the support base 1 of left-hand end and it is slidably mounted on this
On guide rod 3 in groove I 2, the right side of sliding rail 5 is located in the groove I 2 of the support base 1 of right-hand end and it is slidably mounted on this
On guide rod 3 in groove I 2；Block 7, is placed in the top of sliding rail 5, and slider I 19 is located at the lower section of sliding rail 5, sets in slider I 19
Be equipped with sliding rail 5 match groove II 20, slider I 19 by groove II 20 sliding be plugged in sliding rail 5, slider I 19 with
Block 7 is connected and fixed by screw II 23；Bracket 9, the upper end are equipped with depth gauge 10 by screw I 11, and 9 lower end of bracket is set
It is equipped with shaft 14, the lower end of shaft 14 is thread segment II 15, is provided with the screw hole I to match with thread segment II 15 in block 7
8, thread segment II 15 is combined in screw hole I 8；Change 18, rotational installation in shaft 14, horizontally disposed measuring scale 26 with turn
Ring 18 is connected, and is provided with scale along its length on measuring scale 26；Sliding block II 27, sliding sleeve are slided loaded on measuring scale 26
The lower end of block II 27 is equipped with indicator 29 along the vertical direction；And probe 25, it is set to the lower end of slider I 19, depth gauge
10 probe rod 12 sequentially passes through coaxially connected with probe 25 after bracket 9, block 7 and slider I 19.Two support bases 1 are placed in
On aircraft skin, realizes that driving depth gauge 10 slides along the longitudinal direction by pushing sliding rail 5 to slide along guide rod 3, slided by pushing
Block I 19 is slided by groove II 20 along 5 left and right directions of sliding rail, is slided in left-right direction to realize driving depth gauge 10,
By the sliding of depth gauge front-rear direction and left and right directions, probe 25 is made to be moved to the minimum point or aircraft illiteracy of aircraft skin recess
The highest point position of skin protrusion, probe 25 drives probe rod 12 to move along the vertical direction, so that numerical value can pass through depth gauge 10
It reads.By rotating change 18, make measuring scale 26 drive indicator 29 to be rocked to and be recessed or notch that raised brim is nearest or
The direction of person's fastener row, slides into indicator 29 positioned at nearest notch or fastening by sliding slider II 27 later
The top of part row, by reading the scale on measuring scale 26 it can be learnt that between the edge and nearest notch of recess or protrusion
Distance or at a distance from nearest fastener row.The precision of measurement and the convenience of operation are improved, measurement efficiency is improved.
It preferably, further include being set to 1 upper end of support base and the long hole 4 and holding screw I 6 parallel with guide rod 3,
Holding screw I 6 passes through 4 back spin of long hole together on sliding rail 5, and the head of screw of holding screw I 6 connects with the upper surface of support base 1
Touching.When sliding rail 5 is slided along guide rod 3, holding screw I 6 is slided along long hole 4, will when sliding the tight holding screw I 6 of back spin in place
The position locked and fixed of sliding rail 5.To which sliding rail 5 cannot be move freely again.
It preferably, further include the screw hole II 21 being set in slider I 19, the axis of screw hole II 21 and the length of sliding rail 5
Direction is perpendicular, and holding screw II 22 is combined in screw hole II 21, and the tail end of holding screw II 22 is in contact with sliding rail 5.When
Slider I 19 horizontally slips the tight holding screw II 22 of back spin in place along sliding rail 5, the tail end and 5 appearance of sliding rail of holding screw II 22
The locked and fixed of 19 position of slider I is realized after face contact.
It preferably, further include the holding screw III 28 being combined on sliding block II 27 along the vertical direction, holding screw III 28
Tail end be in contact with measuring scale 26.When by driving sliding block II 27 to slide the tight holding screw III of back spin in place along measuring scale 26
28 so that its tail end is in contact with the upper surface of measuring scale 26 after realize 29 position of indicator locked and fixed, prevent it from freely living
It is dynamic.
It further, further include the spiral shell for being set to the thread segment I 13 of 14 upper end of shaft and being combined on thread segment I 13
Mother 16, the lower end surface of nut 16 is in contact with the upper surface of change 18.When change 18 rotate in place, i.e., indicator 29 turns to finger
Positioning postpones, and by rotating nuts 16, is fixed it on block 7 change 18, to realize the position of change 18
Locked and fixed, prevent change 18 to be freely rotated.Handle 17 can be set on nut 16, operation can be convenient by handle 17
Nut 16 rotates, and further improves the convenience of operation.
It can also include several section extension rods 24, each extension rod 24 is coaxially connected, on several extension rods 24 after connection
End is coaxially connected with probe rod 12, and lower end and probe 25 are coaxially connected.By increasing extension rod 24, different depth can be adapted to
Sunk area measurement use, further improve the scope of application.
It further, further include the stabilizer blade 30 for being respectively arranged at 1 lower end front and rear sides of support base.It can be square by stabilizer blade 30
Support base 1 is just supported on to the surface of aircraft skin.
Claims (8)
1. a kind of measurement auxiliary mould for survey aircraft covering bumps degree characterized by comprising
Two support bases (1) are located at left and right ends, are provided with groove I (2) in two support bases (1), the groove I (2)
Inside being horizontally disposed with along the longitudinal direction has guide rod (3)；
Sliding rail (5), is horizontally disposed in left-right direction, and the left side of sliding rail (5) is located in the groove I (2) of the support base (1) of left-hand end
And it is slidably mounted on the guide rod (3) in the groove I (2), the right side of sliding rail (5) is located at the recessed of the support base (1) of right-hand end
In slot I (2) and it is slidably mounted on the guide rod (3) in the groove I (2)；
Block (7), is placed in the top of sliding rail (5), and slider I (19) is located at the lower section of sliding rail (5), setting in the slider I (19)
There is the groove II (20) to match with sliding rail (5), slider I (19) is plugged in sliding rail (5) by groove II (20) sliding, slider I
(19) it is connected and fixed with block (7) by screw II (23)；
Bracket (9), the upper end are equipped with depth gauge (10) by screw I (11), and bracket (9) lower end is provided with shaft
(14), the lower end of shaft (14) is thread segment II (15), is provided with the spiral shell to match with thread segment II (15) in the block (7)
Hole I (8), thread segment II (15) are combined in screw hole I (8)；
Change (18) is rotatablely installed on shaft (14), and horizontally disposed measuring scale (26) is connected with change (18), measuring scale
(26) scale is provided on along its length；
Sliding block II (27), for sliding sleeve loaded on measuring scale (26), the lower end of sliding block II (27) is equipped with indicator along the vertical direction
(29)；And
Probe (25), is set to the lower end of slider I (19), and the probe rod (12) of depth gauge (10) sequentially passes through bracket (9), block
(7) and slider I (19) is coaxially connected with probe (25) afterwards.
2. the measurement auxiliary mould according to claim 1 for survey aircraft covering bumps degree, it is characterised in that: also
Including being set to support base (1) upper end and the long hole (4) and holding screw I (6) parallel with guide rod (3), the clamp screw
It follows closely I (6) and passes through long hole (4) back spin together on sliding rail (5), the upper surface phase of the head of screw and support base (1) of holding screw I (6)
Contact.
3. the measurement auxiliary mould according to claim 1 for survey aircraft covering bumps degree, it is characterised in that: also
Including the screw hole II (21) being set on slider I (19), the length direction of the axis and sliding rail (5) of the screw hole II (21) mutually hangs down
Directly, holding screw II (22) is combined in screw hole II (21), and the tail end of holding screw II (22) is in contact with sliding rail (5).
4. the measurement auxiliary mould according to claim 1 for survey aircraft covering bumps degree, it is characterised in that: also
Including the holding screw III (28) being combined on sliding block II (27) along the vertical direction, the tail end of the holding screw III (28) and survey
Gage (26) is in contact.
5. the measurement auxiliary mould according to claim 1 for survey aircraft covering bumps degree, it is characterised in that: also
Including the nut (16) for being set to the thread segment I (13) of shaft (14) upper end and being combined on thread segment I (13), the nut
(16) lower end surface is in contact with the upper surface of change (18).
6. the measurement auxiliary mould according to claim 1 for survey aircraft covering bumps degree, it is characterised in that: also
Including several section extension rods (24), each extension rod (24) is coaxially connected, several extension rods (24) upper end and probe after connection
Bar (12) is coaxially connected, and lower end and probe (25) are coaxially connected.
7. the measurement auxiliary mould as claimed in any of claims 1 to 6 for survey aircraft covering bumps degree,
It is characterized by also including the stabilizer blades (30) for being respectively arranged at support base (1) lower end front and rear sides.
8. the measurement auxiliary mould according to claim 5 for survey aircraft covering bumps degree, it is characterised in that: institute
It states and is provided with handle (17) on nut (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920029000.2U CN209246924U (en) | 2019-01-09 | 2019-01-09 | A kind of measurement auxiliary mould for survey aircraft covering bumps degree |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920029000.2U CN209246924U (en) | 2019-01-09 | 2019-01-09 | A kind of measurement auxiliary mould for survey aircraft covering bumps degree |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209246924U true CN209246924U (en) | 2019-08-13 |
Family
ID=67536018
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920029000.2U Withdrawn - After Issue CN209246924U (en) | 2019-01-09 | 2019-01-09 | A kind of measurement auxiliary mould for survey aircraft covering bumps degree |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209246924U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109579675A (en) * | 2019-01-09 | 2019-04-05 | 山东太古飞机工程有限公司 | A kind of measurement auxiliary mould for survey aircraft covering bumps degree |
-
2019
- 2019-01-09 CN CN201920029000.2U patent/CN209246924U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109579675A (en) * | 2019-01-09 | 2019-04-05 | 山东太古飞机工程有限公司 | A kind of measurement auxiliary mould for survey aircraft covering bumps degree |
| CN109579675B (en) * | 2019-01-09 | 2023-09-08 | 山东太古飞机工程有限公司 | Auxiliary measurement tool for measuring concave-convex degree of aircraft skin |
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20190813 Effective date of abandoning: 20230908 |
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| AV01 | Patent right actively abandoned |
Granted publication date: 20190813 Effective date of abandoning: 20230908 |