CN109692987A - A kind of positioning support auxiliary mould precisely to drill on aircraft - Google Patents
A kind of positioning support auxiliary mould precisely to drill on aircraft Download PDFInfo
- Publication number
- CN109692987A CN109692987A CN201910158929.XA CN201910158929A CN109692987A CN 109692987 A CN109692987 A CN 109692987A CN 201910158929 A CN201910158929 A CN 201910158929A CN 109692987 A CN109692987 A CN 109692987A
- Authority
- CN
- China
- Prior art keywords
- sliding
- slide rail
- track groove
- longitudinal slide
- drill gun
- Prior art date
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B45/00—Hand-held or like portable drilling machines, e.g. drill guns; Equipment therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25H—WORKSHOP EQUIPMENT, e.g. FOR MARKING-OUT WORK; STORAGE MEANS FOR WORKSHOPS
- B25H1/00—Work benches; Portable stands or supports for positioning portable tools or work to be operated on thereby
- B25H1/0021—Stands, supports or guiding devices for positioning portable tools or for securing them to the work
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/10—Greenhouse gas [GHG] capture, material saving, heat recovery or other energy efficient measures, e.g. motor control, characterised by manufacturing processes, e.g. for rolling metal or metal working
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Drilling And Boring (AREA)
Abstract
A kind of positioning support auxiliary mould precisely to drill on aircraft, comprising: sliding rail, sliding block, two electric telescopic rods, connecting shaft, longitudinal slide rail I, longitudinal slide rail II, horizontally disposed along the longitudinal direction, sliding support and drill gun clamp system.It is fixedly clamped with the position realization to match in bore position short transverse to drill gun by drill gun clamping device.Moving left and right sliding support slides longitudinal slide rail I along connecting shaft by linear bearing, slide longitudinal slide rail II along the guide-track groove I of sliding rail by sliding block, to make drill gun conveniently be adjusted to required bore position in left-right direction, it pushes drill gun to make sliding support sliding rail I and the inside Slideslip of longitudinal slide rail II along longitudinal direction, drill gun can be realized to carry out drilling or ream operation perpendicular to the direction of drilling plane.Improve the efficiency of drilling and the precision of drilling, operator, which need to only hold drill gun and move inwardly, can be completed drilling, improve the convenience of the operation in preceding locker small space.
Description
Technical field
The present invention relates to aircraft conversion technical field of tools, and in particular to a kind of positioning branch precisely to drill on aircraft
Support auxiliary mould.
Background technique
When carrying out the work such as Boeing-737 series aircraft WiFi repacking, need to bore in the associated components such as such as locker
The work such as built-in nut are placed in hole, the purpose is to provide brace foundation for increased component, because aircraft space is limited, such as
Say the placement space for needing to install additional WiFi device in WiFi repacking in preceding locker, it is therefore desirable to drill and place in the cabinet
Built-in nut, but the locational space narrow space reequiped required for it, staff are difficult specified position again and are precisely drilled
And reaming, due to narrow space, staff's operation is extremely difficult to be cannot guarantee that during carrying out drilling propulsion,
Drilling is carried out in this small space and built-in nut will lead to drilling and bored plane not because of the Work Limitations of staff
It is able to maintain vertically, and the motion profile that staff is difficult holding boring action when boring work carries out remains and institute
Brill plane is vertical, will greatly increase the probability of drilling failure in this way, this will not only result in additional patch work, or even also
Certain economic loss will be caused, and cannot guarantee that the precision of drilling, in turn resulted in more errors.
Summary of the invention
To overcome the above deficiencies, the invention provides a kind of convenience to drill and improve in locker before aircraft
The positioning support auxiliary mould for precisely drilling on aircraft of borehole accuracy.
The present invention overcomes the technical solution used by its technical problem to be:
A kind of positioning support auxiliary mould precisely to drill on aircraft, comprising:
Sliding rail is horizontally disposed in left-right direction, and being horizontally disposed in sliding rail has guide-track groove I；
Sliding block is slidably mounted in left-right direction in guide-track groove I；
Two electric telescopic rods are fixed on the left and right ends of sliding rail vertically by screw II respectively；
Connecting shaft is horizontally disposed with, and both ends are connected with the top of ipsilateral electric telescopic rod respectively, the connecting shaft and sliding rail phase
In parallel, it is slidably fitted with linear bearing in left-right direction in the connecting shaft；
Longitudinal slide rail I, is horizontally disposed with along the longitudinal direction, and the front end of longitudinal slide rail I is fixed on linear bearing by screw I；
Longitudinal slide rail II, is horizontally disposed with along the longitudinal direction, and the front end of longitudinal slide rail II is fixed on sliding block by screw III；
Sliding support, the upper end of sliding support are provided with the track groove II to match with I cross section of longitudinal slide rail, lower end setting
There is the track groove I to match with II cross section of longitudinal slide rail, the sliding of longitudinal slide rail I is plugged in track groove II, longitudinal slide rail II
Sliding is plugged in track groove I；And
Drill gun clamp system, is set in sliding support, and drill gun is fixedly clamped in sliding support and making the axis of drill gun
It is parallel with longitudinal slide rail I and longitudinal slide rail II.
Above-mentioned drill gun clamp system includes the fixation fixture block being slidably mounted in sliding support along the vertical direction and is located at
The active fastening block of fixed fixture block upper end, the fixed fixture block top are provided with semicircular arc groove I, the active fastening block lower section
It is provided with semicircular arc groove II, after active fastening block is fixed by the relatively fixed fixture block locking of locking system, drill gun clamps solid
Due between arc groove I and arc groove II, the outboard end of the fixed fixture block is combined with hand rotation bolt, the head of the hand rotation bolt
End is in contact with sliding support.
It further include the axis transverse direction for being horizontally installed to the axis upper end of sliding support upper and lower ends respectively for the ease of Rapid reset
Across track groove II, the axis of lower end is horizontally through track groove I；Prolong its length direction in longitudinal slide rail I and is provided with guide-track groove III, bullet
Spring II is plugged in guide-track groove III, is rotatably equipped with ball on the axis in track groove II, and ball rolling is set to guide rail
In slot III, the tail end of spring II is connected with longitudinal slide rail I, and head end is in contact with the ball in track groove II；Longitudinal slide rail II
Inside prolong its length direction and be provided with guide-track groove II, spring I is plugged in guide-track groove II, and peace is rotated on the axis in track groove I
Equipped with ball, ball rolling is set in guide-track groove II, and I tail end of spring is connected with longitudinal slide rail II, head end and guide-track groove
Ball in II is in contact.
Locker is worn in order to prevent, and the lower end of above-mentioned sliding rail is provided with cushion rubber bumper.
Locker is worn in order to prevent, and the piston rod head end of above-mentioned electric telescopic rod is provided with non-slip rubber block.
Sliding support is fallen in order to prevent, and the tail end of above-mentioned longitudinal slide rail I is equipped with block I, the longitudinal direction by bolt I
The tail end of sliding rail II is equipped with block II by bolt II.
Above-mentioned locking system includes the sliding slot being set in fixed fixture block along the vertical direction, short transverse interval is set along the chute
Several card slots for being placed in sliding slot side and the slide bar for being set to active fastening block side, the slide bar outboard end is provided with and card slot
The ratchet to match, spring one end are connected with slide bar, and the other end is connected with active fastening block, and sliding bar is plugged in sliding slot,
When spring in a free state, ratchet is plugged in corresponding card slot.
In order to improve supportive, the lower end of above-mentioned sliding support is equipped with buphthalmos wheel.
Drill gun is damaged in order to prevent, is provided with rubber pad I, active card between the arc groove I and drill gun of above-mentioned fixed fixture block
Rubber pad II is provided between the arc groove II and drill gun of block.
The beneficial effects of the present invention are: before entire tooling is placed into locker, sliding rail and preceding locker lower end surface phase
Contact, after the piston rod of two electric telescopic rods stretches out, head end is in contact with the upper surface of preceding locker, realizes entire work
Support in preceding locker is fixed, later by drill gun clamping device with the position that matches in bore position short transverse
Realization is set to be fixedly clamped to drill gun.Moving left and right sliding support slides longitudinal slide rail I along connecting shaft by linear bearing,
Slide longitudinal slide rail II along the guide-track groove I of sliding rail by sliding block, so that drill gun be made conveniently to be adjusted to required brill in left-right direction
Hole site pushes drill gun to make sliding support sliding rail I and the inside Slideslip of longitudinal slide rail II along longitudinal direction, drill gun can be realized with vertical
Drilling or ream operation are carried out in the direction of drilling plane.The efficiency of drilling is not only increased, while improving the precision of drilling,
Operator, which need to only hold drill gun and move inwardly, can be completed drilling, improve in preceding locker small space operation just
Benefit.
Detailed description of the invention
Fig. 1 is schematic perspective view of the invention；
Fig. 2 is stereochemical structure perspective view of the explosion of the invention；
Fig. 3 is the structural schematic diagram of fixation fastening block part position of the invention；
Fig. 4 is the structural schematic diagram at active fastening block position of the invention；
In figure, 1. sliding rail, 2. cushion rubber bumper, 3. electric telescopic rod, 4. connecting shaft, 5. linear bearing, 6. longitudinal slide rail, I 7. spiral shell
Follow closely I 8. longitudinal slide rail, II 9. sliding support, 10. block, I 11. bolt, I 12. block, II 13. bolt, II 14. buphthalmos wheel
15. fixed 16. hand of fixture block revolves 17. active fastening block of bolt, 18. drill gun, 19. guide-track groove, I 20. screw, II 21. anti-slip rubber
I 27. spring of block 22. sliding block, 23. screw, III 24. guide-track groove, II 25. guide-track groove, III 26. spring, II 28. rubber pad I
29. 35. card slot of rubber pad II 30. track groove, I 31. track groove, II 32. axis, 33. ball, 34. sliding slot, 36. slide bar 37.
38. spring III of ratchet.
Specific embodiment
1 to attached drawing 4, the present invention will be further described with reference to the accompanying drawing.
A kind of positioning support auxiliary mould precisely to drill on aircraft, comprising: sliding rail 1, it is horizontal in left-right direction
It is arranged, being horizontally disposed in sliding rail 1 has guide-track groove I 19；Sliding block 22 is slidably mounted in left-right direction in guide-track groove I 19；Two
Electric telescopic rod 3 is fixed on the left and right ends of sliding rail 1 vertically by screw II 20 respectively；Connecting shaft 4 is horizontally disposed with, two
End is connected with the top of ipsilateral electric telescopic rod 3 respectively, and connecting shaft 4 is parallel with sliding rail 1, in connecting shaft 4 in left-right direction
It is slidably fitted with linear bearing 5；Longitudinal slide rail I 6, is horizontally disposed with along the longitudinal direction, and the front end of longitudinal slide rail I 6 passes through spiral shell
I 7 are followed closely to be fixed on linear bearing 5；Longitudinal slide rail II 8, is horizontally disposed with along the longitudinal direction, and the front end of longitudinal slide rail II 8 is logical
Screw III 23 is crossed to be fixed on sliding block 22；Sliding support 9, the upper end of sliding support 9 are provided with and I 6 cross section of longitudinal slide rail
The track groove II 31 to match, lower end is provided with the track groove I 30 to match with II 8 cross section of longitudinal slide rail, longitudinal sliding
The sliding of rail I 6 is plugged in track groove II 31, and the sliding of longitudinal slide rail II 8 is plugged in track groove I 30；And drill gun clamps
Mechanism is set in sliding support 9, and drill gun 18 is fixedly clamped in sliding support 9 and making axis and the longitudinal direction of drill gun 18
Sliding rail I 6 and longitudinal slide rail II 8 are parallel.In use, before entire tooling is placed into locker, sliding rail 1 and preceding locker
Lower end surface is in contact, and after the piston rod of two electric telescopic rods 3 stretches out, head end is in contact with the upper surface of preceding locker, real
Showed support of the entire tooling in preceding locker to fix, later by drill gun clamping device in bore position short transverse
Realize being fixedly clamped to drill gun 18 in the position to match.Moving left and right sliding support 9 makes longitudinal slide rail I 6 pass through linear bearing
5 slide along connecting shaft 4, slide longitudinal slide rail II 8 along the guide-track groove I 19 of sliding rail 1 by sliding block 22, to make drill gun 18
It is conveniently adjusted to required bore position in left-right direction, drill gun 18 is pushed to make sliding support 9 sliding rail I 6 and longitudinal slide rail along longitudinal direction
Drill gun 18 can be realized to carry out drilling or ream operation perpendicular to the direction of drilling plane in II 8 inside Slideslips.Not only mention
The high efficiency of drilling, while improving the precision of drilling, operator, which need to only hold drill gun and move inwardly, can be completed brill
Hole improves the convenience of the operation in preceding locker small space.
Further, drill gun clamp system includes the fixation fixture block 15 being slidably mounted in sliding support 9 along the vertical direction
And the active fastening block 17 positioned at fixed 15 upper end of fixture block, it fixes above fixture block 15 and is provided with semicircular arc groove I, active card
Semicircular arc groove II is provided with below block 17, active fastening block 17 is fixed by relatively fixed 15 locking of fixture block of locking system
Afterwards, drill gun 18 is fixedly clamped between arc groove I and arc groove II, and the outboard end of fixed fixture block 15 is combined with hand rotation bolt 16,
The head end of hand rotation bolt 16 is in contact with sliding support 9.Unclamping hand rotation bolt 16 can make fixed fixture block 15 along sliding support 9
Lower slider then realizes the height of condition drill gun 18 to facilitate the height for adjusting fixed fixture block 15.It is screwed after being adjusted in place
Hand revolves bolt 16.Drill gun 18 can be realized after fixing by relatively fixed 15 locking of fixture block of locking system in active fastening block 17
It is fixedly clamped.
It can also include the axis 32 for being horizontally installed to 9 upper and lower ends of sliding support respectively, the axis 32 of upper end is horizontally through rail
The axis 32 of road slot II 31, lower end is horizontally through track groove I 30；Prolong its length direction in longitudinal slide rail I 6 and is provided with guide-track groove III
25, spring II 27 is plugged in guide-track groove III 25, is rotatably equipped with ball 33 on the axis 32 in track groove II 31, should
The rolling of ball 33 is set in guide-track groove III 25, and the tail end of spring II 27 is connected with longitudinal slide rail I 6, head end and track groove
Ball 33 in II 31 is in contact；Prolong its length direction in longitudinal slide rail II 8 and be provided with guide-track groove II 24, spring I 26 inserts
In in guide-track groove II 24, it is rotatably equipped with ball 33 on the axis 32 in track groove I 30, the ball 33 rolling, which is set to, to be led
In track slot II 24, I 26 tail end of spring is connected with longitudinal slide rail II 8, and head end connects with the ball 33 in guide-track groove II 24
Touching.When needing to drill, pushing drill gun 18 to make sliding support 9, sliding rail I 6 and longitudinal slide rail II 8 are slided along longitudinal direction, track groove II
Compressed spring II 27 when ball 33 rolls in guide-track groove III 25 in 31, the ball 33 in track groove I are rolled in guide-track groove II 24
Compressed spring I 26 when dynamic.After drilling, spring I 26 and spring II 27 release energy and 9 edge of sliding support can be driven
Rearward opposite direction slides for longitudinal slide rail I 6 and longitudinal slide rail II 8, realizes Rapid reset.
Preferably, the lower end of sliding rail 1 is provided with cushion rubber bumper 2.1 bottom of sliding rail passes through cushion rubber bumper 2 and preceding locker
Bottom connection touching can damage locker before aircraft to avoid sliding rail 1.The piston rod head end of electric telescopic rod 3 is provided with anti-slip rubber
Block 21.It is anti-skidding when the piston rod of electric telescopic rod 3 is protruding to be made to be in contact at the top of non-slip rubber block 21 and preceding locker
Rubber block 21 can prevent damage of the electric telescopic rod 3 to preceding locker.
The tail end of longitudinal slide rail I 6 is equipped with block I 10 by bolt I 11, and the tail end of longitudinal slide rail II 8 passes through spiral shell
Bolt II 13 is equipped with block II 12.Setting block I 10 and block II 12 can prevent sliding support 9 from longitudinal slide rail I 6
Or the tail end of longitudinal slide rail II 8 slides, and improves the reliability used.
Further, above-mentioned locking system includes the sliding slot 34 being set in fixed fixture block 15 along the vertical direction, along the chute
34 short transverses are arranged at intervals at several card slots 35 of 34 side of sliding slot and are set to the slide bar 36 of 17 side of active fastening block, sliding
36 outboard end of bar is provided with the ratchet 37 to match with card slot 35, and 38 one end of spring is connected with slide bar 36, the other end and activity
Fixture block 17 be connected, slide bar 36 sliding be plugged in sliding slot 34, when spring 38 in a free state, ratchet 37 is plugged in corresponding
In card slot 35.Ratchet 37, which is located in card slot 35, realizes the locked of relatively fixed 15 position of fixture block of active fastening block 17, when outside
When layback moving slide-bar 36, spring 38 is stretched, and ratchet 37 is detached from from card slot 35 at this time, and slide bar 36 can slide in sliding slot 34,
Realize unlock.Since multiple groups card slot 35 is arranged, to be suitable for the fixation of the drill gun 18 of different size.
Preferably, the lower end of sliding support 9 is equipped with buphthalmos wheel 14.When sliding rail I 6 and longitudinal direction are sliding along longitudinal direction for sliding support 9
When the inside Slideslip of rail II 8 realizes that drill gun 18 drills, sliding support 9 is by the buphthalmos wheel 14 of lower end along under preceding locker
Plane rolling not only realizes the support to sliding support 9, while also improving the smoothness when movement of sliding support 9.
Further, it is provided with rubber pad I 28 between the arc groove I and drill gun 18 of fixed fixture block 15, active fastening block 17
Rubber pad II 29 is provided between arc groove II and drill gun 18.Arc groove I is to drill gun 18 when rubber pad I 28 can prevent from clamping
Damage, damage of the arc groove II to drill gun 18 when rubber pad II 29 can prevent from clamping, further improve use it is reliable
Property.
Claims (9)
1. a kind of positioning support auxiliary mould precisely to drill on aircraft characterized by comprising
Sliding rail (1), is horizontally disposed in left-right direction, and being horizontally disposed in sliding rail (1) has guide-track groove I (19)；
Sliding block (22) is slidably mounted in left-right direction in guide-track groove I (19)；
Two electric telescopic rods (3) are fixed on the left and right ends of sliding rail (1) vertically by screw II (20) respectively；
Connecting shaft (4) is horizontally disposed with, and both ends are connected with the top of ipsilateral electric telescopic rod (3) respectively, the connecting shaft
(4) parallel with sliding rail (1), it is slidably fitted with linear bearing (5) in left-right direction on the connecting shaft (4)；
Longitudinal slide rail I (6), is horizontally disposed with along the longitudinal direction, and the front end of longitudinal slide rail I (6) is fixed on directly by screw I (7)
Spool is held on (5)；
Longitudinal slide rail II (8), is horizontally disposed with along the longitudinal direction, and the front end of longitudinal slide rail II (8) is fixed by screw III (23)
In on sliding block (22)；
Sliding support (9), the upper end of sliding support (9) are provided with the track groove II to match with longitudinal slide rail I (6) cross section
(31), lower end is provided with the track groove I (30) to match with longitudinal slide rail II (8) cross section, and longitudinal slide rail I (6) sliding is inserted
Loaded in track groove II (31), longitudinal slide rail II (8) sliding is plugged in track groove I (30)；And
Drill gun clamp system is set in sliding support (9), and drill gun (18) is fixedly clamped in sliding support (9) and is made
The axis of drill gun (18) is parallel with longitudinal slide rail I (6) and longitudinal slide rail II (8).
2. the positioning support auxiliary mould according to claim 1 for precisely drilling on aircraft, it is characterised in that: described
Drill gun clamp system includes the fixation fixture block (15) that is slidably mounted in sliding support (9) along the vertical direction and is located at fixing card
The active fastening block (17) of block (15) upper end, fixed fixture block (15) top are provided with semicircular arc groove I, the active card
Semicircular arc groove II is provided with below block (17), active fastening block (17) passes through relatively fixed fixture block (15) locking of locking system
After fixation, drill gun (18) is fixedly clamped between arc groove I and arc groove II, and the outboard end of the fixed fixture block (15) is combined with
Hand revolves bolt (16), and the head end of hand rotation bolt (16) is in contact with sliding support (9).
3. the positioning support auxiliary mould according to claim 1 for precisely drilling on aircraft, it is characterised in that: also wrap
The axis (32) for being horizontally installed to sliding support (9) upper and lower ends respectively is included, the axis (32) of upper end is horizontally through track groove II (31),
The axis (32) of lower end is horizontally through track groove I (30)；Prolong its length direction in longitudinal slide rail I (6) and be provided with guide-track groove III (25),
Spring II (27) is plugged in guide-track groove III (25), is rotatably equipped with ball on the axis (32) being located in track groove II (31)
(33), the ball (33) rolling is set in guide-track groove III (25), and the tail end of spring II (27) is connected with longitudinal slide rail I (6),
Head end is in contact with the ball (33) in track groove II (31)；Prolong its length direction in longitudinal slide rail II (8) and is provided with guide-track groove
II (24), spring I (26) are plugged in guide-track groove II (24), are rotatably equipped with rolling on the axis (32) being located in track groove I (30)
Pearl (33), the ball (33) rolling are set in guide-track groove II (24), and spring I (26) tail end is connected with longitudinal slide rail II (8),
Head end is in contact with the ball (33) in guide-track groove II (24).
4. the positioning support auxiliary mould according to claim 1 for precisely drilling on aircraft, it is characterised in that: described
The lower end of sliding rail (1) is provided with cushion rubber bumper (2).
5. the positioning support auxiliary mould according to claim 1 for precisely drilling on aircraft, it is characterised in that: described
The piston rod head end of electric telescopic rod (3) is provided with non-slip rubber block (21).
6. the positioning support auxiliary mould as claimed in any of claims 1 to 5 for precisely drilling on aircraft,
Be characterized in that: the tail end of the longitudinal slide rail I (6) is equipped with block I (10), the longitudinal slide rail II (8) by bolt I (11)
Tail end block II (12) is equipped with by bolt II (13).
7. the positioning support auxiliary mould according to claim 1 for precisely drilling on aircraft, it is characterised in that: described
Locking system includes the sliding slot (34) being set in fixed fixture block (15) along the vertical direction, (34) short transverse interval is set along the chute
It is placed in several card slots (35) of sliding slot (34) side and is set to the slide bar (36) of active fastening block (17) side, the slide bar
(36) outboard end is provided with the ratchet (37) to match with card slot (35), and spring (38) one end is connected with slide bar (36), another
End be connected with active fastening block (17), slide bar (36) slide be plugged in sliding slot (34), when spring (38) in a free state, spine
Tooth (37) is plugged in corresponding card slot (35).
8. the positioning support auxiliary mould according to claim 7 for precisely drilling on aircraft, it is characterised in that: described
The lower end of sliding support (9) is equipped with buphthalmos wheel (14).
9. the positioning support auxiliary mould according to claim 7 for precisely drilling on aircraft, it is characterised in that: described
Be provided with rubber pad I (28) between the arc groove I and drill gun (18) of fixed fixture block (15), the arc groove II of active fastening block (17) and
Drill gun is provided with rubber pad II (29) between (18).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910158929.XA CN109692987B (en) | 2019-03-04 | 2019-03-04 | Positioning support auxiliary tool for accurate drilling on airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910158929.XA CN109692987B (en) | 2019-03-04 | 2019-03-04 | Positioning support auxiliary tool for accurate drilling on airplane |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109692987A true CN109692987A (en) | 2019-04-30 |
| CN109692987B CN109692987B (en) | 2023-09-08 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910158929.XA Active CN109692987B (en) | 2019-03-04 | 2019-03-04 | Positioning support auxiliary tool for accurate drilling on airplane |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111730300A (en) * | 2020-05-29 | 2020-10-02 | 铜陵长江金刚石工具有限责任公司 | Assembling tool for electric drill with sliding rail |
| CN111842972A (en) * | 2020-07-28 | 2020-10-30 | 沈阳航空航天大学 | A location support auxiliary fixtures that is used for accurate drilling on aircraft |
| CN113510258A (en) * | 2021-08-12 | 2021-10-19 | 天津华建天恒传动有限责任公司 | Continuous positioning drilling method for inner wall radial hole |
| CN114261531A (en) * | 2021-12-21 | 2022-04-01 | 电子科技大学 | Intelligent flexible clamping equipment for wing |
| CN114274274A (en) * | 2022-01-03 | 2022-04-05 | 罗贤生 | Furniture processing drilling equipment |
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| CN111730300A (en) * | 2020-05-29 | 2020-10-02 | 铜陵长江金刚石工具有限责任公司 | Assembling tool for electric drill with sliding rail |
| CN111730300B (en) * | 2020-05-29 | 2021-03-16 | 铜陵长江金刚石工具有限责任公司 | Assembling tool for electric drill with sliding rail |
| CN111842972A (en) * | 2020-07-28 | 2020-10-30 | 沈阳航空航天大学 | A location support auxiliary fixtures that is used for accurate drilling on aircraft |
| CN113510258A (en) * | 2021-08-12 | 2021-10-19 | 天津华建天恒传动有限责任公司 | Continuous positioning drilling method for inner wall radial hole |
| CN113510258B (en) * | 2021-08-12 | 2022-03-15 | 天津华建天恒传动有限责任公司 | Continuous positioning drilling method for inner wall radial hole |
| CN114261531A (en) * | 2021-12-21 | 2022-04-01 | 电子科技大学 | Intelligent flexible clamping equipment for wing |
| CN114261531B (en) * | 2021-12-21 | 2023-04-11 | 电子科技大学 | Intelligent flexible clamping equipment for wing |
| CN114274274A (en) * | 2022-01-03 | 2022-04-05 | 罗贤生 | Furniture processing drilling equipment |
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