CN109676554A - A kind of general fast-positioning device of monoblock type for Airplane frame plate parts and its application method - Google Patents
A kind of general fast-positioning device of monoblock type for Airplane frame plate parts and its application method Download PDFInfo
- Publication number
- CN109676554A CN109676554A CN201910039334.2A CN201910039334A CN109676554A CN 109676554 A CN109676554 A CN 109676554A CN 201910039334 A CN201910039334 A CN 201910039334A CN 109676554 A CN109676554 A CN 109676554A
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- positioning
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- slotted hole
- gauge
- snap
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- 238000000034 method Methods 0.000 title claims abstract description 9
- 125000006850 spacer group Chemical group 0.000 claims abstract description 15
- 239000000047 product Substances 0.000 claims description 16
- 238000009434 installation Methods 0.000 claims description 4
- 239000006227 byproduct Substances 0.000 claims description 3
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B11/00—Work holders not covered by any preceding group in the subclass, e.g. magnetic work holders, vacuum work holders
- B25B11/02—Assembly jigs
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Connection Of Plates (AREA)
Abstract
The invention belongs to aviations to assemble field, be related to a kind of general fast-positioning device of the monoblock type for Airplane frame plate parts and its application method.The device includes round orifices orientation plate, slotted hole positioning plate, positioning support, spacer pin, housing screw, protection screw, screw thread positioning pin, handle nut and snap-gauge.The erect-position face of snap-gauge is consistent with product deckle board positioning surface, and positioning support is fixed on snap-gauge；Round orifices orientation plate and slotted hole positioning plate are each passed through the through slot of two positioning supports, both ends setting protection screw；The spacer pin being inserted on positioning support, screws housing screw；One end that round orifices orientation plate and slotted hole positioning plate stretch out snap-gauge is connect with screw thread positioning pin and handle nut thread, the positioning for product deckle board.Positioning device and snap-gauge are designed to the adjustable form of entirety by the present invention, in conjunction with quick positioning and clamping element, are improved location efficiency, are positioned Board position or size adjustable, adapt to the positioning of different product frame plate parts, meet production requirement.
Description
Technical field
The invention belongs to aviations to assemble field, be related to a kind of general quick positioning of the monoblock type for Airplane frame plate parts
Device and its application method.
Background technique
The assembly of general Airplane frame plate parts is all to complete positioning function by positioning deckle board plane and hole.Due to product
Design feature, erection sequence and undercarriage mode limited, the deckle board positioning device of tooling is typically designed to seperated with snap-gauge
Form.At the scene in use, especially large-scale assembly tooling, right since the movable locating device quantity for needing to dismantle is more
Clamping difficulty, clamping time-bands centainly influence.Especially for the similar locator of structure, the neglected loading of Yi Fasheng locator, mistake
Phenomena such as dress.The management of quality and tooling to product brings certain influence.
Summary of the invention
, structure many kinds of for tooling deckle board positioning device be similar to lead to that the clamping time is long, is easy to happen leakage when using
The case where dress, misloading, the present invention propose a kind of general fast-positioning device of the monoblock type for Airplane frame plate parts and its make
Use method.
The technical solution of the present invention is as follows:
A kind of general fast-positioning device of monoblock type for Airplane frame plate parts, including round orifices orientation plate 1, slotted hole
Positioning plate 2, positioning support 3, spacer pin 4, housing screw 5, straight pin 6, attachment screw 7 protect screw 8, screw thread positioning pin 9, hand
Handle nut 10 and snap-gauge 11；
The erect-position face of the snap-gauge 11 is used for positioning product deckle board positioning surface, pre-threaded hole on snap-gauge 11；The positioning
It support 3 totally two, is respectively arranged on snap-gauge 11, is threadedly coupled by attachment screw 7 with the threaded hole of snap-gauge 11, and pass through circle
Pin 6 is fixed on snap-gauge 11；Positioning support 3, which is equipped between spacer pin 4 and housing screw 5, with snap-gauge contact surface, is equipped with groove；
Longitudinal chute is equipped on the round orifices orientation plate 1 and slotted hole positioning plate 2, round orifices orientation plate 1 and slotted hole are fixed
Position plate 2 respectively passes through the groove of two positioning supports 3, and one end setting protection screw 8, prevents round orifices orientation plate 1 and slotted hole
Positioning plate 2 slides from positioning support 3；Spacer pin 4 on positioning support 3 passes through longitudinal chute, is used to 1 He of round orifices orientation plate
Slotted hole positioning plate 2 is fixed to operating position, and housing screw 5 is screwed for eliminating round orifices orientation plate 1 and slotted hole positioning plate 2
With the gap between 11 erect-position face of snap-gauge；One end that round orifices orientation plate 1 stretches out snap-gauge 11 is equipped with circular hole, screw thread is inside set, with screw thread
Positioning pin 9 is threadedly coupled, and handle nut 10 is arranged on screw thread positioning pin 9, by screw thread positioning pin 9 and handle nut 10 by product
Deckle board positioning；One end that slotted hole positioning plate 2 stretches out snap-gauge 11 is equipped with lateral slotted hole and tool ball mounting hole；Lateral slotted hole
Screw thread is inside set, is threadedly coupled with screw thread positioning pin 9, handle nut 10 is set on screw thread positioning pin 9, passes through 9 He of screw thread positioning pin
Handle nut 10 positions product deckle board；Installation tool ball in tool ball mounting hole, for determining round orifices orientation plate 1 and slotted hole
Position plate 2 is adjusted to theoretical position.
Steps are as follows for application method:
Step 1, in use, round orifices orientation plate 1 and slotted hole positioning plate 2 are stretched out snap-gauge 11, insertion spacer pin 4 is distinguished
Round orifices orientation plate 1 and slotted hole positioning plate 2 are fixed to operating position, screw housing screw 5 to eliminate round orifices orientation plate 1 and length
Product deckle board is fixed to by the gap between round orifices orientation plate 2 and snap-gauge erect-position face by screw thread positioning pin 9 and handle nut 10
On round orifices orientation plate 1 and slotted hole positioning plate 2；
After use, screw thread positioning pin 9 and handle nut 10 are dismantled from product deckle board for step 2, extract limit
Pin 4 unclamps housing screw 5, round orifices orientation plate 1 and slotted hole positioning plate 2 is slid rearwardly out home, screw housing screw
5 prevent the movement of round orifices orientation plate 1 and slotted hole positioning plate 2 in an inactive state.
Beneficial effects of the present invention:
Positioning device and snap-gauge are designed to the adjustable form of entirety, in conjunction with the quick positioning and compression in positioning device
Element solves the problems, such as that positioning device location efficiency is low.By the adjustment to positioning Board position or size, different product frame is adapted to
The positioning of plate parts.Product deckle board after the installation of this device, assembly efficiency and quality are improved significantly, and meet life
Production demand.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of the general fast-positioning device of monoblock type for Airplane frame plate parts；
Fig. 2 is that a kind of positioning plate structure of the general fast-positioning device of monoblock type for Airplane frame plate parts is illustrated
Figure；
In figure: 1 round orifices orientation plate；2 slotted hole positioning plates；3 positioning supports；4 spacer pins；5 housing screws；6 straight pins；7
Attachment screw；8 protection screws；9 screw thread positioning pins；10 handle nuts；11 snap-gauges.
Specific embodiment
Below in conjunction with attached drawing and technical solution, specific embodiments of the present invention are further illustrated.
As shown in Figure 1, a kind of general fast-positioning device of monoblock type for Airplane frame plate parts, including round orifices orientation
Plate 1, slotted hole positioning plate 2, positioning support 3, spacer pin 4, housing screw 5, straight pin 6, attachment screw 7 protect screw 8, screw thread
Positioning pin 9, handle nut 10 and snap-gauge 11；
The erect-position face of the snap-gauge 11 is used for positioning product deckle board positioning surface, pre-threaded hole on snap-gauge 11；The positioning
It support 3 totally two, is respectively arranged on snap-gauge 11, is threadedly coupled by attachment screw 7 with the threaded hole of snap-gauge 11, and pass through circle
Pin 6 is fixed on snap-gauge 11；Positioning support 3, which is equipped between spacer pin 4 and housing screw 5, with snap-gauge contact surface, is equipped with groove；
Longitudinal chute is equipped on the round orifices orientation plate 1 and slotted hole positioning plate 2, round orifices orientation plate 1 and slotted hole are fixed
Position plate 2 respectively passes through the groove of two positioning supports 3, and one end setting protection screw 8, prevents round orifices orientation plate 1 and slotted hole
Positioning plate 2 slides from positioning support 3；Spacer pin 4 on positioning support 3 passes through longitudinal chute, is used to 1 He of round orifices orientation plate
Slotted hole positioning plate 2 is fixed to operating position, and housing screw 5 is screwed for eliminating round orifices orientation plate 1 and slotted hole positioning plate 2
With the gap between 11 erect-position face of snap-gauge；One end that round orifices orientation plate 1 stretches out snap-gauge 11 is equipped with circular hole, screw thread is inside set, with screw thread
Positioning pin 9 is threadedly coupled, and handle nut 10 is arranged on screw thread positioning pin 9, by screw thread positioning pin 9 and handle nut 10 by product
Deckle board positioning；One end that slotted hole positioning plate 2 stretches out snap-gauge 11 is equipped with lateral slotted hole and tool ball mounting hole；Lateral slotted hole
Screw thread is inside set, is threadedly coupled with screw thread positioning pin 9, handle nut 10 is set on screw thread positioning pin 9, passes through 9 He of screw thread positioning pin
Handle nut 10 positions product deckle board；Installation tool ball in tool ball mounting hole, for determining round orifices orientation plate 1 and slotted hole
Position plate 2 is adjusted to theoretical position.
Steps are as follows for application method:
Step 1, in use, round orifices orientation plate 1 and slotted hole positioning plate 2 are stretched out snap-gauge 11, insertion spacer pin 4 is distinguished
Round orifices orientation plate 1 and slotted hole positioning plate 2 are fixed to operating position, screw housing screw 5 to eliminate round orifices orientation plate 1 and length
Product deckle board is fixed to by the gap between round orifices orientation plate 2 and snap-gauge erect-position face by screw thread positioning pin 9 and handle nut 10
On round orifices orientation plate 1 and slotted hole positioning plate 2；
After use, screw thread positioning pin 9 and handle nut 10 are dismantled from product deckle board for step 2, extract limit
Pin 4 unclamps housing screw 5, round orifices orientation plate 1 and slotted hole positioning plate 2 is slid rearwardly out home, screw housing screw
5 prevent the movement of round orifices orientation plate 1 and slotted hole positioning plate 2 in an inactive state.
In addition to the implementation, the present invention can also have other embodiments.It is all to use equivalent substitution or equivalent transformation shape
At technical solution, fall within the scope of protection required by the present invention.
Claims (2)
1. a kind of general fast-positioning device of monoblock type for Airplane frame plate parts, which is characterized in that described is used to fly
The general fast-positioning device of the monoblock type of machine frame plate parts includes round orifices orientation plate (1), slotted hole positioning plate (2), positioning branch
Seat (3), spacer pin (4), housing screw (5), straight pin (6), attachment screw (7), protection screw (8), screw thread positioning pin (9),
Handle nut (10) and snap-gauge (11)；
The erect-position face of the snap-gauge (11) is used for positioning product deckle board positioning surface, pre-threaded hole on snap-gauge (11)；The positioning
It support (3) totally two, is respectively arranged on snap-gauge (11), is threadedly coupled by attachment screw (7) with the threaded hole of snap-gauge (11),
And it is fixed on snap-gauge (11) by straight pin (6)；Positioning support (3) is equipped with spacer pin (4) and housing screw (5), with card
Groove is equipped between plate contact surface；
Longitudinal chute, round orifices orientation plate (1) and slotted hole are equipped on the round orifices orientation plate (1) and slotted hole positioning plate (2)
Positioning plate (2) respectively passes through the groove of two positioning supports (3), and one end setting protection screw (8), prevents round orifices orientation plate
(1) it is slid from positioning support (3) with slotted hole positioning plate (2)；Spacer pin (4) on positioning support (3) passes through longitudinal chute,
For round orifices orientation plate (1) and slotted hole positioning plate (2) are fixed to operating position, housing screw (5) are screwed for eliminating
Gap between round orifices orientation plate (1) and slotted hole positioning plate (2) and snap-gauge (11) erect-position face；Round orifices orientation plate (1) stretches out card
One end of plate (11) is equipped with circular hole, inside sets screw thread, is threadedly coupled with screw thread positioning pin (9), handle is arranged on (9) in screw thread positioning pin
Nut (10) is positioned product deckle board by screw thread positioning pin (9) and handle nut (10)；Slotted hole positioning plate (2) stretches out card
One end of plate (11) is equipped with lateral slotted hole and tool ball mounting hole；Screw thread is set in lateral slotted hole, with screw thread positioning pin (9) spiral shell
Line connection, is arranged handle nut (10) on screw thread positioning pin (9), by screw thread positioning pin (9) and handle nut (10) by product
Deckle board positioning；Installation tool ball in tool ball mounting hole, for round orifices orientation plate (1) and slotted hole positioning plate (2) to be adjusted to
Theoretical position.
2. the user of the monoblock type general fast-positioning device according to claim 1 for Airplane frame plate parts
Method, which is characterized in that steps are as follows:
Step 1 is inserted into spacer pin (4) in use, round orifices orientation plate (1) and slotted hole positioning plate (2) are stretched out snap-gauge (11)
Round orifices orientation plate (1) and slotted hole positioning plate (2) are fixed to operating position respectively, screw housing screw (5) to eliminate circular hole
Gap between positioning plate (1) and slotted hole positioning plate (2) and snap-gauge erect-position face passes through screw thread positioning pin (9) and handle nut
(10) product deckle board is fixed on round orifices orientation plate (1) and slotted hole positioning plate (2)；
After use, screw thread positioning pin (9) and handle nut (10) are dismantled from product deckle board for step 2, extract limit
It sells (4), unclamps housing screw (5), round orifices orientation plate (1) and slotted hole positioning plate (2) are slid rearwardly out into home, screwed
Housing screw (5) prevents the movement of round orifices orientation plate (1) and slotted hole positioning plate (2) in an inactive state.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910039334.2A CN109676554A (en) | 2019-01-16 | 2019-01-16 | A kind of general fast-positioning device of monoblock type for Airplane frame plate parts and its application method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910039334.2A CN109676554A (en) | 2019-01-16 | 2019-01-16 | A kind of general fast-positioning device of monoblock type for Airplane frame plate parts and its application method |
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| Publication Number | Publication Date |
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| CN109676554A true CN109676554A (en) | 2019-04-26 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910039334.2A Pending CN109676554A (en) | 2019-01-16 | 2019-01-16 | A kind of general fast-positioning device of monoblock type for Airplane frame plate parts and its application method |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110026926A (en) * | 2019-05-16 | 2019-07-19 | 沈阳飞机工业（集团）有限公司 | A kind of Movable telescopic positioning device for the assembly of tooling upper product |
| CN110052986A (en) * | 2019-05-21 | 2019-07-26 | 沈阳飞机工业（集团）有限公司 | A kind of device and application method of profile class part positioning and Bidirectional compacting |
| CN112975794A (en) * | 2021-02-22 | 2021-06-18 | 浙江大学 | Positioning and clamping device for outer wing of airplane |
| CN113263312A (en) * | 2021-07-16 | 2021-08-17 | 成都飞机工业（集团）有限责任公司 | Airplane frame positioning structure based on tolerance distribution and process method |
| CN113500551A (en) * | 2021-08-19 | 2021-10-15 | 沈阳飞机工业（集团）有限公司 | Multi-support-arm sheet metal frame assembling and positioning device and using method thereof |
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110026926A (en) * | 2019-05-16 | 2019-07-19 | 沈阳飞机工业（集团）有限公司 | A kind of Movable telescopic positioning device for the assembly of tooling upper product |
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| CN110052986A (en) * | 2019-05-21 | 2019-07-26 | 沈阳飞机工业（集团）有限公司 | A kind of device and application method of profile class part positioning and Bidirectional compacting |
| CN110052986B (en) * | 2019-05-21 | 2024-01-23 | 沈阳飞机工业（集团）有限公司 | Section bar part positioning and two-way compacting device and use method |
| CN112975794A (en) * | 2021-02-22 | 2021-06-18 | 浙江大学 | Positioning and clamping device for outer wing of airplane |
| CN112975794B (en) * | 2021-02-22 | 2022-01-04 | 浙江大学 | Positioning and clamping device for outer wing of airplane |
| CN113263312A (en) * | 2021-07-16 | 2021-08-17 | 成都飞机工业（集团）有限责任公司 | Airplane frame positioning structure based on tolerance distribution and process method |
| CN113500551A (en) * | 2021-08-19 | 2021-10-15 | 沈阳飞机工业（集团）有限公司 | Multi-support-arm sheet metal frame assembling and positioning device and using method thereof |
| CN113500551B (en) * | 2021-08-19 | 2024-03-08 | 沈阳飞机工业（集团）有限公司 | Multi-support arm sheet metal frame assembly positioning device and use method thereof |
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Application publication date: 20190426 |
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