CN201484667U - Universal combined frame for vertical assembling jig - Google Patents
Universal combined frame for vertical assembling jig Download PDFInfo
- Publication number
- CN201484667U CN201484667U CN200920216057XU CN200920216057U CN201484667U CN 201484667 U CN201484667 U CN 201484667U CN 200920216057X U CN200920216057X U CN 200920216057XU CN 200920216057 U CN200920216057 U CN 200920216057U CN 201484667 U CN201484667 U CN 201484667U
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- connecting panel
- face
- vertical
- steel tube
- square steel
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Abstract
The utility model belongs to aircraft assembling technology and relates to the improvement of an aircraft assembling jig. The universal combined frame for a vertical assembling jig comprises two identical crossbeams [1] and two identical support saddles [2], which are connected together. Each crossbeam [1] consists of a square steel tube [4], two end face connecting plate [3] and two cross connecting plates [5] and each support saddle [2] consists of an upright post [6], a base [7] and a longitudinal connecting plate [8]. The end face connecting plate [3] at one end of each crossbeam [1] is connected with the upper end and the lower end of the longitudinal connecting plate [8] of one support saddle [2] through positioning bolts and nuts, and the end face connecting plate [3] at the other end of the crossbeam [1] is connected with the upper end and the lower end of the longitudinal connecting plate [8] of the other support saddle [2] through positioning bolts and nuts. The utility model has strong universality and greatly reduces the number of the frames of the jig, reduces the manufacturing cost and shortens the manufacturing period.
Description
Technical field
The utility model belongs to the aircraft assembly technique, relates to the improvement to the aircraft assembling fixture.
Background technology
In the aircraft fitting process, the quantity of needed assembling fixture is appreciiable, and especially the frame-type anchor clamps occupy sizable ratio, and every kind of anchor clamps all need framework separately, and framework does not have commonality.Along with type is on the increase, the number of components of aircraft also increases gradually, and the quantity of required like this jig frame also rolls up, and causes the manufacturing cost of aircraft to strengthen, and the manufacturing cycle prolongs.
Summary of the invention
The purpose of this utility model is: a kind of compound type assembling fixture framework of highly versatile is provided, to reduce the quantity of jig frame, reduces manufacturing cost, shorten the manufacturing cycle.
The technical solution of the utility model is: a kind of general combined vertical assembling fixture framework is characterized in that it is connected to form with two identical bearings of structure by two identical crossbeams of structure; Crossbeam is made up of square steel tube, two end face connecting panels and two horizontal connecting panels, the end face connecting panel is the square plate of area greater than the square steel tube cross section, the end face connecting panel near the wide position that goes out on four limits have at interval evenly, the positioning screw hole of straight-though arrangement, the end face of end face connecting panel and crossbeam is welded as integral body; Horizontal connecting panel is the rectangular plate of length less than square steel tube, horizontal connecting panel is welded on two relative sides of square steel tube, the width of horizontal connecting panel is greater than the length of side in square steel tube cross section, has at interval evenly on the wide plate face that goes out of horizontal connecting panel near two long limits, the positioning screw hole of straight-though arrangement; Bearing is by column, base and vertical connecting panel are formed, column and base are made by square steel tube, the lower end and the base of column are welded as integral body, vertical connecting panel is the rectangular plate that width equates with the length of side of end face connecting panel, near on the plate face on two long limits two registration screw holes are arranged at vertical connecting panel, even and the arrangement that is in line in the interval of every registration screw hole, width between centers on the vertical connecting panel between the two registration screw holes equals the width between centers of relative two registration screw holes on the end face connecting panel, the interval of every registration screw hole equates that with interval on the end face connecting panel vertical connecting panel is welded on the column on the vertical connecting panel; The end face connecting panel of two crossbeam one ends is connected with the two ends up and down of the vertical connecting panel of a bearing respectively by fixing screw and nut, and the end face connecting panel of two crossbeam other ends is connected with the two ends up and down of the vertical connecting panel of another bearing respectively by fixing screw and nut.
The utility model has the advantages that: highly versatile, significantly reduced the quantity of jig frame, reduced manufacturing cost, shortened the manufacturing cycle.The utility model adopts the box-like jig frame of a kind of common group that various assembling fixture is installed, make in the aircraft fitting process, need not make jig frame more in a large number, thereby saved the anchor clamps manufacturing cost, shorten the manufacturing cycle, also solved the problem of the usable floor area growing tension in assembling worker-house.
Description of drawings
Fig. 1 is a structural representation of the present utility model.
Fig. 2 is the beam structure scheme drawing in the utility model.
Fig. 3 is the seat structure scheme drawing in the utility model.
The specific embodiment
Below the utility model is described in further details.Referring to Fig. 1～3, a kind of general combined vertical assembling fixture framework is characterized in that, it is connected to form with two identical bearings 2 of structure by two identical crossbeams 1 of structure; Crossbeam 1 is made up of square steel tube 4, two end face connecting panels 3 and two horizontal connecting panels 5, end face connecting panel 3 is the square plate of area greater than square steel tube 4 cross sections, end face connecting panel 3 near the wide position that goes out on four limits have at interval evenly, the positioning screw hole of straight-though arrangement, end face connecting panel 3 is welded as integral body with the end face of crossbeam 1; Horizontal connecting panel 5 is the rectangular plate of length less than square steel tube 4, horizontal connecting panel 5 is welded on 4 two relative sides of square steel tube, the width of horizontal connecting panel 5 is greater than the length of side in square steel tube 4 cross sections, has at interval evenly on the wide plate face that goes out of horizontal connecting panel 5 near two long limits, the positioning screw hole of straight-though arrangement; Bearing 2 is by column 6, base 7 and vertical connecting panel 8 are formed, column 6 and base 7 are made by square steel tube, the lower end of column 6 and base 7 are welded as integral body, vertical connecting panel 8 is rectangular plates that width equates with the length of side of end face connecting panel 3, near on the plate face on two long limits two registration screw holes are arranged at vertical connecting panel 8, even and the arrangement that is in line in the interval of every registration screw hole, width between centers on the vertical connecting panel 8 between the two registration screw holes equals the width between centers of relative two registration screw holes on the end face connecting panel 3, the interval of every registration screw hole equates with interval on the end face connecting panel 3 on the vertical connecting panel 8, indulges connecting panel 8 and is welded on the column 6; The end face connecting panel 3 of two crossbeam 1 one ends is connected with the two ends up and down of the vertical connecting panel 8 of a bearing 2 respectively by fixing screw and nut, and the end face connecting panel 3 of two crossbeam 1 other ends is connected with the two ends up and down of the vertical connecting panel 8 of another bearing 2 respectively by fixing screw and nut.
Using method of the present utility model is: select the crossbeam 1 of required size and bearing 2 to form jig frame earlier, then clamp part such as needed various multi-form anchor clamps locationss, compressing members, be contained in the location positioning hole suitable on crossbeam 1 and the bearing 2, so just formed needed assembling fixture.
Claims (1)
1. a general combined vertical assembling fixture framework is characterized in that, it is connected to form with two identical bearings [2] of structure by two identical crossbeams [1] of structure; Crossbeam [1] is made up of square steel tube [4], two end face connecting panels [3] and two horizontal connecting panels [5], end face connecting panel [3] is the square plate of area greater than square steel tube [4] cross section, end face connecting panel [3] near the wide position that goes out on four limits have at interval evenly, the positioning screw hole of straight-though arrangement, end face connecting panel [3] is welded as integral body with the end face of crossbeam [1]; Horizontal connecting panel [5] is the rectangular plate of length less than square steel tube [4], horizontal connecting panel [5] is welded on [4] two relative sides of square steel tube, the width of horizontal connecting panel [5] is greater than the length of side in square steel tube [4] cross section, has at interval evenly on the wide plate face that goes out of horizontal connecting panel [5] near two long limits, the positioning screw hole of straight-though arrangement; Bearing [2] is by column [6], base [7] and vertical connecting panel [8] are formed, column [6] and base [7] are made by square steel tube, the lower end of column [6] and base [7] are welded as integral body, vertical connecting panel [8] is the rectangular plate that width equates with the length of side of end face connecting panel [3], near on the plate face on two long limits two registration screw holes are arranged at vertical connecting panel [8], even and the arrangement that is in line in the interval of every registration screw hole, width between centers between the vertical last two registration screw holes of connecting panel [8] equals the width between centers that end face connecting panel [3] is gone up relative two registration screw holes, the interval of the last every registration screw hole of vertical connecting panel [8] equates that with the interval on the end face connecting panel [3] vertical connecting panel [8] is welded on the column [6]; The end face connecting panel [3] of two crossbeam [1] one ends is connected with the two ends up and down of the vertical connecting panel [8] of a bearing [2] respectively by fixing screw and nut, and the end face connecting panel [3] of two crossbeams [1] other end is connected with the two ends up and down of the vertical connecting panel [8] of another bearing [2] respectively by fixing screw and nut.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200920216057XU CN201484667U (en) | 2009-09-14 | 2009-09-14 | Universal combined frame for vertical assembling jig |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200920216057XU CN201484667U (en) | 2009-09-14 | 2009-09-14 | Universal combined frame for vertical assembling jig |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201484667U true CN201484667U (en) | 2010-05-26 |
Family
ID=42423558
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN200920216057XU Expired - Fee Related CN201484667U (en) | 2009-09-14 | 2009-09-14 | Universal combined frame for vertical assembling jig |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201484667U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103522346A (en) * | 2012-07-06 | 2014-01-22 | 哈尔滨飞机工业集团有限责任公司 | General cutting mould base support |
| CN103878511A (en) * | 2014-04-10 | 2014-06-25 | 太仓斯普宁精密机械有限公司 | Support of precise welding robot |
| CN104340376A (en) * | 2013-08-05 | 2015-02-11 | 哈尔滨飞机工业集团有限责任公司 | Anti-instability structure for composite plate part during airworthiness verification tests |
| CN104511866A (en) * | 2013-09-30 | 2015-04-15 | 哈尔滨飞机工业集团有限责任公司 | Fishbone-shaped assembly clamp |
| CN110815077A (en) * | 2019-11-14 | 2020-02-21 | 昌河飞机工业（集团）有限责任公司 | Irregular frame type part clamping device and method |
-
2009
- 2009-09-14 CN CN200920216057XU patent/CN201484667U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103522346A (en) * | 2012-07-06 | 2014-01-22 | 哈尔滨飞机工业集团有限责任公司 | General cutting mould base support |
| CN104340376A (en) * | 2013-08-05 | 2015-02-11 | 哈尔滨飞机工业集团有限责任公司 | Anti-instability structure for composite plate part during airworthiness verification tests |
| CN104511866A (en) * | 2013-09-30 | 2015-04-15 | 哈尔滨飞机工业集团有限责任公司 | Fishbone-shaped assembly clamp |
| CN103878511A (en) * | 2014-04-10 | 2014-06-25 | 太仓斯普宁精密机械有限公司 | Support of precise welding robot |
| CN110815077A (en) * | 2019-11-14 | 2020-02-21 | 昌河飞机工业（集团）有限责任公司 | Irregular frame type part clamping device and method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100526 Termination date: 20140914 |
|
| EXPY | Termination of patent right or utility model |