CN204240995U - A kind of full machine docking collimation and level measurement device - Google Patents
A kind of full machine docking collimation and level measurement device Download PDFInfo
- Publication number
- CN204240995U CN204240995U CN201420637843.8U CN201420637843U CN204240995U CN 204240995 U CN204240995 U CN 204240995U CN 201420637843 U CN201420637843 U CN 201420637843U CN 204240995 U CN204240995 U CN 204240995U
- Authority
- CN
- China
- Prior art keywords
- collimation
- laser
- pedestal
- described pedestal
- measurement device
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000003032 molecular docking Methods 0.000 title claims abstract description 33
- 238000005259 measurement Methods 0.000 title claims abstract description 29
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 45
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
Landscapes
- Length Measuring Devices By Optical Means (AREA)
Abstract
The utility model provides a kind of full machine docking collimation and level measurement device, comprising: pedestal, and the two ends of described pedestal are located respectively and are clamped in two seat slides be arrangeding in parallel; Generating laser, it is arranged vertically on described pedestal, and described generating laser has the first laser beam emitting head for launching collimation laser plane and the second laser beam emitting head for emission level laser plane; Horizontal receiving target, it is arranged vertically on described pedestal, and is used for receiving described horizontal laser light plane; And collimation receiving target, it is parallel to described pedestal and arranges, and is used for receiving described collimation laser plane.The utility model Appropriate application product structure, designs light, and location clamping is convenient and reliable, disposablely carries out level and alignment measurement.
Description
Technical field
The utility model relates to a kind of full machine docking collimation and level measurement device, and being specially adapted to take seat slide as the full machine docking of aircraft of docking benchmark.
Background technology
Before aircraft docking, need to carry out level and alignment measurement adjustment, judge whether the requirement meeting product design document and technical conditions.
Current mean level and collimation are separately measured, and need the two cover frocks that outfit two is overlapped instrument and matched.Operating process is complicated, inefficiency, and the Fixture Design manufacturing cycle is longer, and production cost is higher.
Utility model content
In order to solve the problem, it take seat slide as the full machine docking collimation and the level measurement device that dock benchmark that the utility model provides a kind of, it can utilize aircraft product structure, fuselage seat slide is located and clamps, and in the full machine docking of aircraft, realize level and alignment measurement simultaneously, and ensure measuring accuracy.
To achieve these goals, comprise with level measurement device according to full machine docking collimation of the present utility model:
Pedestal, the two ends of described pedestal are located respectively and are clamped in two seat slides be arrangeding in parallel;
Generating laser, it is arranged vertically on described pedestal, and described generating laser has the first laser beam emitting head for launching collimation laser plane and the second laser beam emitting head for emission level laser plane;
Horizontal receiving target, it is arranged vertically on described pedestal, and is used for receiving described horizontal laser light plane; And
Collimation receiving target, it is parallel to described pedestal and arranges, and is used for receiving described collimation laser plane.
In one embodiment, the two ends of described pedestal are arranged in the hole of described seat slide respectively by straight pin.
In another embodiment, the two ends of described pedestal are arranged in the chute of described seat slide by straight pin.
In yet another embodiment, one end of described pedestal is arranged on by straight pin in the hole of described seat slide, and the other end of described pedestal is arranged in the chute of described seat slide by straight pin.
Preferably, the binding clasp for being clamped to by described pedestal in described seat slide is also comprised.
Preferably, described generating laser is adsorbed on described pedestal by magnetic bases.
The utility model selects the new pattern laser instrument simultaneously can launching pairwise orthogonal laser plane, and instrument, with magnetic bases, is directly adsorbed on the location-plate of frock.Frock is with aircraft docking benchmark for design basis, and Appropriate application aircraft product structure, on fuselage seat slide, (aircraft docking benchmark) locates and clamp.
Advantage of the present utility model: Appropriate application product structure, designs light, and location clamping is convenient and reliable; Surveying instrument and device precision high, utilize that set of device is disposable carries out level and alignment measurement, ensure that full machine merging precision, to the level of the large parts docking such as aircraft, boats and ships, spacecraft and alignment measurement, there is reference significance.
Accompanying drawing explanation
Fig. 1 shows according to the side view of full machine docking collimation of the present utility model with level measurement device;
Fig. 2 shows according to the vertical view of full machine docking collimation of the present utility model with level measurement device;
Fig. 3 shows the locator meams according to full machine docking collimation of the present utility model and the pedestal of level measurement device and the hole of seat slide;
Fig. 4 shows the locator meams according to full machine docking collimation of the present utility model and the pedestal of level measurement device and the chute of seat slide;
Fig. 5 shows according to full machine docking collimation of the present utility model and the pedestal of level measurement device and the clamping mode of seat slide; And
Fig. 6 shows the schematic diagram using full machine docking collimation of the present utility model and level measurement device.
Embodiment
In the specific descriptions of following preferred embodiment, with reference to the accompanying drawing formed appended by the utility model part.Appended accompanying drawing shows by way of example and can realize specific embodiment of the present utility model.The embodiment of example is not intended to limit according to all embodiments of the present utility model.Be appreciated that under the prerequisite not departing from scope of the present utility model, other embodiments can be utilized, also can carry out amendment that is structural or logicality.
In following specific descriptions, the term of directivity, such as "left", "right" " top ", " bottom ", "front", "rear", " forward ", " backward " etc., use with reference to the direction described in accompanying drawing.The parts of embodiment of the present utility model can be placed in multiple different direction, and the term of directivity is nonrestrictive for the object of example.
As shown in Figures 1 and 2, full machine docking collimation of the present utility model mainly comprises pedestal 10, generating laser 20, horizontal receiving target 30 with level measurement device and collimates receiving target 40.The two ends of pedestal 10 are located respectively and are clamped in two seat slides 50 be arrangeding in parallel.Generating laser 20 is arranged vertically on pedestal 10, is adsorbed on pedestal 10 preferably by magnetic bases.Generating laser 20 has the first laser beam emitting head 21 for launching collimation laser plane BL and the second laser beam emitting head 22 for emission level laser plane WL.Horizontal receiving target 30 is arranged vertically on pedestal 10, and is used for receiving horizontal laser light plane WL, and collimation receiving target 40 is parallel to pedestal 10 and arranges, and is used for receiving collimation laser plane BL.
As shown in Figures 3 and 4, one end of pedestal 10 is arranged in the hole 51 of seat slide 50 by straight pin 70, and the other end is arranged in the chute 52 of seat slide 50 by straight pin 70.This locator meams makes full use of aircraft seat rail structure, adopts a locating surface (end face of slide rail) and two short straight pins to position.For solving orientation problem, a straight pin adopted location, hole (see Fig. 3), and another straight pin adopts groove location (see Fig. 4), thus does not limit the location interference problem of slide rail axis direction.
As shown in Figure 5, full machine docking collimation of the present utility model and level measurement device also comprise the binding clasp 60 for being clamped to by pedestal 10 in seat slide 50.By adopting tightening structure, sliding-rail groove put into by binding clasp 60, rotates 90 °, tightens upper nut, complete clamping, and this structure is simple, easy to operate.
A whole set of frock arranges conjunction measuring system, symmetrical at center line two ends, makes full use of laser beam, receiving target is placed on farthest as far as possible, and docking is measured more accurate.
Illustrate in Fig. 6 according to the using method of full machine docking collimation of the present utility model with level measurement device.Dock with middle rear body for fuselage in aircraft, during docking adopts, fuselage seat slide is as benchmark.According to the feature of aircraft engineering digital-to-analogue and generating laser self, devise laser bench and target seat.Laser bench is similar with target holder structure, and laser bench is for installing generating laser and receiving target, and target seat only installs receiving target.
In Fig. 6, upside is from left to right followed successively by laser bench, laser bench, target seat, target seat, and downside is 4 target seats.Particularly, laser bench and target seat before and after installing in middle fuselage, installation targets seat in middle rear body, demarcates all receiving targets, comprises horizontal receiving target A, B, C, D, E, F, G, H and collimation receiving target 1#, 2#, 3#, 4#).
(1) horizontal survey
In middle fuselage and middle rear body, be separately installed with four horizontal receiving targets, fuselage attitude in adjustment, make the platform of four receiving targets in middle fuselage in same level.Adjustment generating laser, makes horizontal laser beam plane and base parallel.Rear body attitude in adjustment, makes four receiving target readings in middle rear body consistent with the reading of the receiving target in middle fuselage, then in, the floor level of rear body and middle fuselage is in same plane, completes horizontal adjustment.
(2) alignment measurement
Two collimation receiving targets are installed respectively in middle fuselage and middle rear body.Adjustment generating laser, makes collimated laser beam plane collimate (namely reading is consistent) with receiving target 1#, 2# in middle fuselage.Then, rear body in adjustment, makes receiving target 3#, 4# in middle rear body collimate (consistent with 1#, 2# reading) with longitudinal laser beam plane, completes collimation adjustment.
The utility model selects the new pattern laser instrument simultaneously can launching pairwise orthogonal laser plane, and instrument, with magnetic bases, is directly adsorbed on the location-plate of frock.Frock is with aircraft docking benchmark for design basis, and Appropriate application aircraft product structure, on fuselage seat slide, (aircraft docking benchmark) locates and clamp.
Advantage of the present utility model: Appropriate application product structure, designs light, and location clamping is convenient and reliable; Surveying instrument and device precision high, utilize that set of device is disposable carries out level and alignment measurement, ensure that full machine merging precision, to the level of the large parts docking such as aircraft, boats and ships, spacecraft and alignment measurement, there is reference significance.
Below technology contents and the technical characterstic of specific embodiment of the utility model has been disclosed; but be appreciated that; under creative ideas of the present utility model; those skilled in the art can not make various changes in the combination of this feature clearly illustrated and improve above-mentioned disclosed various characteristic sum, but all belongs to protection domain of the present utility model.The description of above-described embodiment is exemplary and not restrictive, and protection domain of the present utility model determined by claim.
Claims (6)
1. full machine docking collimation and a level measurement device, is characterized in that, comprising:
Pedestal (10), the two ends of described pedestal (10) are located respectively and are clamped in two seat slides (50) be arrangeding in parallel;
Generating laser (20), it is arranged vertically on described pedestal (10), and described generating laser (20) has the first laser beam emitting head (21) for launching collimation laser plane (BL) and the second laser beam emitting head (22) for emission level laser plane (WL);
Horizontal receiving target (30), it is arranged vertically on described pedestal (10), and is used for receiving described horizontal laser light plane (WL); And
Collimation receiving target (40), it is parallel to described pedestal (10) and arranges, and is used for receiving described collimation laser plane (BL).
2. full machine docking collimation according to claim 1 and level measurement device, it is characterized in that, the two ends of described pedestal (10) are arranged in the hole of described seat slide (50) respectively by straight pin (70).
3. full machine docking collimation according to claim 1 and level measurement device, it is characterized in that, the two ends of described pedestal (10) are arranged in the chute of described seat slide (50) respectively by straight pin (70).
4. full machine docking collimation according to claim 1 and level measurement device, it is characterized in that, one end of described pedestal (10) is arranged in the hole (51) of described seat slide (50) by straight pin (70), and the other end of described pedestal (10) is arranged in the chute (52) of described seat slide (50) by straight pin (70).
5. the full machine docking collimation according to any one of claim 1 to 4 and level measurement device, is characterized in that, also comprising the binding clasp (60) for being clamped to by described pedestal (10) in described seat slide (50).
6. the full machine docking collimation according to any one of claim 1 to 4 and level measurement device, it is characterized in that, described generating laser (20) is adsorbed on described pedestal (10) by magnetic bases.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420637843.8U CN204240995U (en) | 2014-10-29 | 2014-10-29 | A kind of full machine docking collimation and level measurement device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420637843.8U CN204240995U (en) | 2014-10-29 | 2014-10-29 | A kind of full machine docking collimation and level measurement device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204240995U true CN204240995U (en) | 2015-04-01 |
Family
ID=52770478
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420637843.8U Expired - Lifetime CN204240995U (en) | 2014-10-29 | 2014-10-29 | A kind of full machine docking collimation and level measurement device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204240995U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105182354A (en) * | 2015-07-16 | 2015-12-23 | 山东钢铁股份有限公司 | Continuously-casted slab measuring device and use method thereof |
| CN109592067A (en) * | 2017-10-03 | 2019-04-09 | 波音公司 | Make the mobile alignment system and method for assembling alignment of the airframe structure of aerospace carrier |
| CN113466791A (en) * | 2021-07-14 | 2021-10-01 | 深圳市武测空间信息有限公司 | Laser mapping and positioning equipment and method |
-
2014
- 2014-10-29 CN CN201420637843.8U patent/CN204240995U/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105182354A (en) * | 2015-07-16 | 2015-12-23 | 山东钢铁股份有限公司 | Continuously-casted slab measuring device and use method thereof |
| CN109592067A (en) * | 2017-10-03 | 2019-04-09 | 波音公司 | Make the mobile alignment system and method for assembling alignment of the airframe structure of aerospace carrier |
| CN113466791A (en) * | 2021-07-14 | 2021-10-01 | 深圳市武测空间信息有限公司 | Laser mapping and positioning equipment and method |
| CN113466791B (en) * | 2021-07-14 | 2022-05-20 | 深圳市武测空间信息有限公司 | Laser mapping and positioning equipment and method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN204240995U (en) | A kind of full machine docking collimation and level measurement device | |
| CN104029192B (en) | Multipoint positioning servicing unit | |
| CN102155928A (en) | Fixture for three-coordinate measuring machine of blade and method for establishing measuring coordinate system | |
| MX2013000992A (en) | Multi-vessel seismic acquisition with undulating navigation lines. | |
| CN104180761A (en) | Wall thickness measuring instrument | |
| CN107843166A (en) | A kind of brake disc bounce, DTV detecting tools and application process | |
| CN207717010U (en) | Profile tolerance verifying attachment | |
| CN203586993U (en) | spatial positioning device | |
| CN103273339A (en) | Ball head positioning device for positioning irregular workpieces in combined clamp and positioning method of ball head positioning device | |
| CN203687848U (en) | Deflection angle measuring tool of flat hole | |
| CN104316007B (en) | The accurate physical dimension measuring system of large scale based on witness mark battle array | |
| CN204944494U (en) | A kind of vehicle location calibration console | |
| CN106323144B (en) | A kind of emitter bias detecting method | |
| CN202877766U (en) | Overall splicing and welding fixture | |
| CN104990476A (en) | Instrument desk test tool end surface simulation positioning device | |
| CN208653424U (en) | A kind of novel three dimension coordinate measurement axis auxiliary detection tool | |
| WO2015102705A3 (en) | Systems and methods for combining triaxial geophone data for localizing nearby transient seismic sources | |
| CN204214351U (en) | The tape head hook structure of tape measure | |
| CN102445175B (en) | Angle measuring device | |
| CN202793345U (en) | Quick gauge for waist-shaped precision hole of aluminous flower board | |
| CN103759616B (en) | A kind of air bag and the assembling detection device of steering wheel | |
| CN103148782B (en) | Comprehensive inspection tool for simulating component assembly position relation structure | |
| CN203672286U (en) | Assembling detecting device for air bag and steering wheel | |
| CN205300427U (en) | Utensil is examined to automobile -used face guard assembly | |
| CN105737757B (en) | A kind of aircraft configuration line detecting method |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |