CN107131809A - One kind digitlization adjustment gauge posture adapter - Google Patents
One kind digitlization adjustment gauge posture adapter Download PDFInfo
- Publication number
- CN107131809A CN107131809A CN201710266354.4A CN201710266354A CN107131809A CN 107131809 A CN107131809 A CN 107131809A CN 201710266354 A CN201710266354 A CN 201710266354A CN 107131809 A CN107131809 A CN 107131809A
- Authority
- CN
- China
- Prior art keywords
- gauge
- cylinder
- commutation rod
- face
- small cylinder
- 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.)
- Pending
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B3/00—Measuring instruments characterised by the use of mechanical techniques
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Length Measuring Devices By Optical Means (AREA)
Abstract
A kind of digitlization adjustment gauge posture adapter of the invention belongs to aircraft mounting technology field, the technical scheme is that enabling gauge to use laser to be installed by increasing gauge intersection point locator adapter, so as to improve the installation accuracy of gauge, so as to reach the interchangeability requirement for improving product, the advantage of invention is that of avoiding the product resetting difficulty that gauge is caused by the installation site disunity on different process equipment caused by artificial origin, improve the harmony that related type frame submits spot locator, the product for improving assembling coordinates interchangeability, reliable means are provided for aircraft assembly coordination and quality control, it is simultaneously a large amount of to save installation period.
Description
Technical field
The invention belongs to measure with switching component, it is related to tradition mark work during digitlization posture adjustment, belongs to aircraft dress
With technical field.
Background technology
With the development of digitizing technique, aircraft is installed e measurement technology and improved constantly, the installation side of original technological equipment
Formula can not meet Fast Installation, remodel and installation accuracy requirement.Due to there is related coordination technological equipment, such as gauge,
Because there is and produced the rapport of aircraft, it be still the coordination foundation of assembly tooling from now on that correlation, which coordinates technological equipment,.
With advances in technology, the installation method of gauge is also changing, and the installation of traditional gauge is all to borrow water
Level, theodolite are installed, and are mostly installed now using laser tracker, because most of gauge in design is all
It is, according to processing at that time and mounting technique level, to cause its structure can not meet its requirement for using laser to install, use biography
The method of system installs that gauge is especially big by human factor, and result difference is larger caused by different people installs, due to gauge
Coordinate technological equipment more, if posture of the gauge in each technological equipment is inconsistent, cause product to coordinate technique dress in correlation
Multiple bearing in standby has difficulties, feasible in the structural theory of the terminal position of traditional approach design, as shown in figure 1, amount
Rule only use notch and hole, and sizes of the intersection point C relative to each related benchmark is adjusted using optical instrument, meet size requirement；Use
Laser is installed, and gauge width of rebate is unsatisfactory for the size requirement of laser ball, and gauge joint itself has various errors, for example
A, B face are green surface, and size L deviations are big etc., cause A, B face to use face directly as laser ball, causing can only be by biography
System method installs gauge, be easily caused occur the product that takes in different process equipment can not multiple bearing the problem of, cause
The coordination inspection repeatedly of the intersection point position point of different process equipment, influences the smooth development of follow-up work.
The content of the invention
The object of the invention：Solving traditional gauge can not use laser to install it.
Technical scheme：It is a kind of to digitize the measurement laser that adjustment gauge posture adapter uses laser tracker
The target of ball 5 is used to carry out gauge 1 position adjustment, and the converter includes commutation rod 2, inserted sheet 3, nut 4.Commutation rod 2 is by two
The coaxially connected composition of cylinder, it is the blind of circle to offer a section perpendicular to the end face on big one end face of cylinder
Hole, the diameter of the blind hole is identical with the diameter of laser ball 5；One end face of another end face of big cylinder and small cylinder connects
Connect, the outer surface close to joint face one end on small cylinder is provided with the annular groove coaxial with small cylinder, small cylinder
External screw thread is provided with close to the outer surface of the small cylinder other end；A breach is provided with inserted sheet 3, and the notch geometry and annular are recessed
The shape of groove matches；Nut 4 has the internal thread matched with the external screw thread of commutation rod 2；The small cylinder of commutation rod 2 is carried
Externally threaded one end is inserted through the hole on gauge 1, the breach of inserted sheet 3 is inserted into the annular groove of commutation rod 2, it is ensured that commutation rod
2 relative gauges 1 are static；Nut 4 is threadedly coupled with commutation rod 2；Rotating nut 4 is until commutation rod 2 is no longer along size
The axis direction movement of cylinder；Laser ball 5 is inserted in the blind hole of the big cylinder of commutation rod 2 until laser ball 5 and big cylinder
Fit in body end face.
Advantages of the present invention：Using this method, the position of intersection point is accurately moved outside using the use face of gauge notch, it is to avoid
The installation site disunity on different process equipment that gauge self reason is caused and the product resetting that causes is difficult, carry
High correlation type frame submits the harmony of spot locator, and the product for improving assembling coordinates interchangeability, is aircraft assembly coordination and matter
Amount control provides reliable means, while largely saving installation period.
Brief description of the drawings
Fig. 1 is the structure type schematic diagram of gauge terminal position,
Fig. 2 is the structural representation of commutation rod 2,
Fig. 3 is the structural representation of inserted sheet 3,
Fig. 4 is that adapter installs and uses schematic diagram,
Wherein 1 is gauge, and 2 be commutation rod, and 3 be inserted sheet, and 4 be nut, and 5 be laser ball
Embodiment
The present invention will be described in detail below in conjunction with the accompanying drawings.
A kind of adjustment gauge posture adapter that digitizes is used for gauge using the target of measurement laser ball 5 of laser tracker
1 carries out position adjustment, it is characterised in that the converter includes commutation rod 2, inserted sheet 3, nut 4.Commutation rod 2 is by two cylinders
Coaxially connected composition, as shown in Fig. 2 it is circular to offer a section perpendicular to the end face on big one end face of cylinder
Blind hole, the diameter of the blind hole is identical with the diameter of laser ball 5；One end face of another end face of big cylinder and small cylinder connects
Connect, the outer surface close to joint face one end on small cylinder is provided with the annular groove coaxial with small cylinder, small cylinder
External screw thread is provided with close to the outer surface of the small cylinder other end；A breach is provided with inserted sheet 3, as shown in figure 3, and the breach shape
The shape of shape and annular groove matches；Nut 4 is had to the internal thread matched with the external screw thread of commutation rod 2 according to Fig. 4；According to
The small cylinder of commutation rod 2 is inserted through the hole on gauge 1 by Fig. 4 with externally threaded one end, and the breach of inserted sheet 3 is inserted
The annular groove of commutation rod 2, it is ensured that commutation rod 2 is static with respect to gauge 1；Nut 4 is threadedly coupled with commutation rod 2；Rotate spiral shell
Mother 4 is until commutation rod 2 is no longer along the axis direction movement of big small cylinder；Laser ball 5 is inserted into the big cylinder of commutation rod 2
Until laser ball 5 is fitted with big cylindrical end face in blind hole.
Operating process is as follows：
1st, the commutation rod 2 in the present invention, inserted sheet 3, nut 4 are manufactured；
2nd, by the position of drawing coarse adjustment gauge 1；
The 3rd, the small cylinder of commutation rod 2 is inserted through to the hole on gauge 1 with externally threaded one end, by inserted sheet 3
Breach inserts the annular groove of commutation rod 2, it is ensured that commutation rod 2 is static with respect to gauge 1；
4th, nut 4 is threadedly coupled with commutation rod 2；Rotating nut 4 is until commutation rod 2 is no longer along big small cylinder
Axis direction movement；
5th, laser ball 5 is inserted in the blind hole of the big cylinder of commutation rod 2 until laser ball 5 is fitted with big cylindrical end face；
6th, by laser ball 5 theoretical position accurate adjustment gauge 1 position.
Claims (1)
1. a kind of adjustment gauge posture adapter that digitizes is used for gauge using measurement laser ball (5) target of laser tracker
(1) position adjustment is carried out, it is characterised in that the converter includes commutation rod (2), inserted sheet (3), nut (4).Commutation rod (2) by
The coaxially connected composition of two cylinders, it is circular to offer a section perpendicular to the end face on big one end face of cylinder
Blind hole, the diameter of the blind hole is identical with the diameter of laser ball (5)；Another end face and one end face of small cylinder of big cylinder
Connection, the outer surface close to joint face one end on small cylinder is provided with the annular groove coaxial with small cylinder, small cylinder
The upper outer surface close to the small cylinder other end is provided with external screw thread；A breach, and the notch geometry and ring are provided with inserted sheet (3)
The shape of connected in star matches；Nut (4) has the internal thread matched with commutation rod (2) external screw thread；By the small of commutation rod (2)
Cylinder is inserted through the hole on gauge (1) with externally threaded one end, and the breach of inserted sheet (3) is inserted into commutation rod (2) ring
Connected in star, it is ensured that commutation rod (2) is static with respect to gauge (1)；Nut (4) is threadedly coupled with commutation rod (2)；Rotating nut
(4) until commutation rod (2) is no longer along the axis direction movement of big small cylinder；Laser ball (5) is inserted into commutation rod (2) great circle
Until laser ball (5) is fitted with big cylindrical end face in the blind hole of cylinder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710266354.4A CN107131809A (en) | 2017-04-21 | 2017-04-21 | One kind digitlization adjustment gauge posture adapter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710266354.4A CN107131809A (en) | 2017-04-21 | 2017-04-21 | One kind digitlization adjustment gauge posture adapter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107131809A true CN107131809A (en) | 2017-09-05 |
Family
ID=59716012
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710266354.4A Pending CN107131809A (en) | 2017-04-21 | 2017-04-21 | One kind digitlization adjustment gauge posture adapter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107131809A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108016632A (en) * | 2017-10-27 | 2018-05-11 | 哈尔滨飞机工业集团有限责任公司 | Increase the method for measuring basis ERS points on analog quantity manufacturing gauge |
| CN111776245A (en) * | 2020-06-12 | 2020-10-16 | 陕西飞机工业（集团）有限公司 | Clamping plate and mounting method thereof |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101850850A (en) * | 2010-03-30 | 2010-10-06 | 浙江大学 | Layout method of central airframe digital assembly of big plane |
| CN102416581A (en) * | 2011-08-30 | 2012-04-18 | 北京航空航天大学 | Hybrid measurement positioning method of part to be assembled in flexible assembly of airplane components |
| WO2012084199A1 (en) * | 2010-12-23 | 2012-06-28 | Straumann Holding Ag | Cassette for storage of medical instruments |
| US8230612B1 (en) * | 2010-04-12 | 2012-07-31 | The United States Of America As Represented By The Secretary Of The Air Force | Installed flight control rod straightness check tool |
| CN204255289U (en) * | 2014-11-14 | 2015-04-08 | 陕西飞机工业（集团）有限公司 | A kind of type frame installs switching measurement mechanism |
| CN205715090U (en) * | 2016-04-01 | 2016-11-23 | 中航飞机股份有限公司西安飞机分公司 | Ear structure is inserted in a kind of adjustable intersection point location |
-
2017
- 2017-04-21 CN CN201710266354.4A patent/CN107131809A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101850850A (en) * | 2010-03-30 | 2010-10-06 | 浙江大学 | Layout method of central airframe digital assembly of big plane |
| US8230612B1 (en) * | 2010-04-12 | 2012-07-31 | The United States Of America As Represented By The Secretary Of The Air Force | Installed flight control rod straightness check tool |
| WO2012084199A1 (en) * | 2010-12-23 | 2012-06-28 | Straumann Holding Ag | Cassette for storage of medical instruments |
| CN102416581A (en) * | 2011-08-30 | 2012-04-18 | 北京航空航天大学 | Hybrid measurement positioning method of part to be assembled in flexible assembly of airplane components |
| CN204255289U (en) * | 2014-11-14 | 2015-04-08 | 陕西飞机工业（集团）有限公司 | A kind of type frame installs switching measurement mechanism |
| CN205715090U (en) * | 2016-04-01 | 2016-11-23 | 中航飞机股份有限公司西安飞机分公司 | Ear structure is inserted in a kind of adjustable intersection point location |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108016632A (en) * | 2017-10-27 | 2018-05-11 | 哈尔滨飞机工业集团有限责任公司 | Increase the method for measuring basis ERS points on analog quantity manufacturing gauge |
| CN111776245A (en) * | 2020-06-12 | 2020-10-16 | 陕西飞机工业（集团）有限公司 | Clamping plate and mounting method thereof |
| CN111776245B (en) * | 2020-06-12 | 2023-09-05 | 陕西飞机工业（集团）有限公司 | Clamping plate and mounting method thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104139321B (en) | Large-sized structural parts in site measurement automatic capturing system and aligning method thereof | |
| CN103759646B (en) | A kind of method utilizing threaded hole location and installation keeper | |
| CN103063135B (en) | Three-dimensional laser scanner posture high-precision calibration method and device | |
| CN101774051A (en) | Inclined hole electrosparking processing device and method for adjusting position and angle of electrode | |
| CN106584513A (en) | Industrial robot repeated positioning accuracy testing method and industrial robot repeated positioning accuracy testing device | |
| CN103837100A (en) | Application of a laser tracker in the measurement of coaxiality of hollow shafts of a large-scale ball mill | |
| CN108195275A (en) | A kind of application method for the tooling for being used to detect rudder carrier base installation accuracy | |
| CN103921170A (en) | Rotary-table center positioning method for spindle-driving-five-shafts machining center | |
| CN107131809A (en) | One kind digitlization adjustment gauge posture adapter | |
| CN109341533B (en) | Process method for measuring seat ring wire hole | |
| CN103009194B (en) | Non-contact inner parallel plane distance measuring method for large-sized workpiece | |
| CN109291029B (en) | Multi-point lofting tool and lofting method based on space coordinate measurement | |
| CN103115544B (en) | Male thread effective length and ending linear measure longimetry frock | |
| CN209783542U (en) | Dual-purpose target ball of total station scanner | |
| CN104677281A (en) | Method for mounting and measuring space connecting pipes | |
| CN106595498B (en) | A kind of antenna house wall thickness measuring and inner mold face process integration device and method | |
| CN106441103A (en) | Laser tracker assisted positioning device capable of being self-adaptive to hole diameter | |
| CN106392206B (en) | A kind of major diameter multiple thread ring gauge on-line machining tooth form geometric parameter measurement method | |
| CN106840130B (en) | High-precision engineering measurement lofting and point placing method | |
| CN201034530Y (en) | Deep inner hole ring groove diameter on-line measuring device | |
| CN206493337U (en) | A kind of test device of industrial robot repetitive positioning accuracy | |
| CN103557848B (en) | Positioning and measuring method for mounting large-sized barrel type base | |
| CN103528574B (en) | Locating measuring tool with large barrel type base | |
| CN102423860B (en) | Locating machining method of fixture for milling reverser holes on internal circulation ball nut | |
| CN201348484Y (en) | Tubing and casing coupling master gage |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170905 |