CN105665599B - A kind of antenna reflective face framework clinching method and device - Google Patents
A kind of antenna reflective face framework clinching method and device Download PDFInfo
- Publication number
- CN105665599B CN105665599B CN201510948327.6A CN201510948327A CN105665599B CN 105665599 B CN105665599 B CN 105665599B CN 201510948327 A CN201510948327 A CN 201510948327A CN 105665599 B CN105665599 B CN 105665599B
- Authority
- CN
- China
- Prior art keywords
- riveting
- covering
- plate
- trapezoidal
- screw rod
- 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.)
- Active
Links
- 238000000034 method Methods 0.000 title claims abstract description 9
- 230000006835 compression Effects 0.000 claims abstract description 13
- 238000007906 compression Methods 0.000 claims abstract description 13
- 238000003825 pressing Methods 0.000 claims description 4
- 238000010276 construction Methods 0.000 abstract description 3
- 238000009434 installation Methods 0.000 abstract description 3
- 238000003754 machining Methods 0.000 description 3
- 238000005266 casting Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J15/00—Riveting
- B21J15/10—Riveting machines
- B21J15/14—Riveting machines specially adapted for riveting specific articles, e.g. brake lining machines
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J15/00—Riveting
- B21J15/02—Riveting procedures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J15/00—Riveting
- B21J15/38—Accessories for use in connection with riveting, e.g. pliers for upsetting; Hand tools for riveting
- B21J15/42—Special clamping devices for workpieces to be riveted together, e.g. operating through the rivet holes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aerials With Secondary Devices (AREA)
- Tyre Moulding (AREA)
Abstract
The invention discloses a kind of antenna reflective face framework clinching method and device, the aerial panel skeleton riveting set is made up of trapezoidal riveting die tire, the locating surface of covering can be placed by being provided with trapezoidal riveting die tire, angle location-plate and rib positioning compression plate are respectively arranged with locating surface, rotary compacting device is provided with the seamed edge of trapezoidal riveting die tire, the present invention not only has simple in construction, the advantages of easy for installation, it is and ingenious in design, securely and reliably, stiffness is good, after being compressed by the positioning of trapezoidal riveting die tire and rib positioning compression plate and rotary compacting device, covering is attached with skeleton with rivet, manual processing means than before are faster and better, and the advantages that can guarantee that its required precision.
Description
Technical field
The present invention relates to a kind of antenna reflective face framework clinching method and device, belong to reflector processing technique field.
Background technology
At present, for medium-and-large-sized antenna, in order to which installation and transportation are convenient, antenna is designed as piecemeal panel type reflector, single
Block Reflector Panel precision prescribed is high, stiffness is good, and interchangeability is good, and existing panel machining is all to be carried out by hand on mould tire
Riveting work, the shortcomings of panel precision is difficult to ensure that, workload is big, so existing clinching method is still not perfect enough.
The content of the invention
It is an object of the invention to：A kind of riveting processing work simple in construction, practical, convenient antenna Reflector Panel is provided
A kind of the antenna reflective face framework clinching method and device that make, aerial panel machining accuracy can be ensured, ensure its interchangeability, with
Overcome the deficiencies in the prior art.
The present invention forms as follows：A kind of antenna reflective face framework riveting set, the aerial panel skeleton riveting set
It is made up of trapezoidal riveting die tire, the locating surface that can place covering is provided with trapezoidal riveting die tire, is set respectively on locating surface
Angle location-plate and rib positioning compression plate are equipped with, rotary compacting device is provided with the seamed edge of trapezoidal riveting die tire.
The rotary compacting device includes bottom support bracket, and two stands are provided with bottom support bracket, two stands it
Between rotor plate is provided with by bearing pin, cursor is provided with rotor plate, rotor plate screw rod is provided with rotor plate, is being turned
Pressure strip is provided with dynamic plate screw rod, cursor screw rod is provided with cursor, compact heap is provided with cursor screw rod.
The rib positioning compression plate is connected by rotary screw with pressing plate to be formed.
6~10 rotary compacting devices are provided with trapezoidal riveting die tire.
A kind of clinching method of antenna reflective face framework riveting set, is placed on trapezoidal riveting by the covering of Reflector Panel first
Connect on mould tire, then rib is placed on covering, adjustment good position enters the bearing of rotary compacting device installed in correct position
Row is fixed, and rotor plate first is turned into the back side during riveting, covering and rib are put well, then rotor plate is rotated to come to use pressure strip
And the fixed covering of screw rod rotation and rib on compact heap, riveted, riveted after all ribs and covering are all fixed
The screw rod of compact heap and pressure strip is unclamped afterwards, and rotary motion plate can decontrol panel, and riveting work can be completed by removing panel.
By adopting the above-described technical solution, compared with prior art, the present invention not only have it is simple in construction, it is easy for installation
The advantages of, and it is ingenious in design, safe and reliable, stiffness is good, pass through trapezoidal riveting die tire positioning and rib positioning compression plate
After being compressed with rotary compacting device, covering is attached with skeleton with rivet, manual processing means than before are faster and better,
And the advantages that can guarantee that its required precision.
Brief description of the drawings
Fig. 1 is the structural representation of the present invention；
Structural representation when Fig. 2 is present invention assembling；
Fig. 3 is Fig. 2 A zoomed-in views；
Fig. 4 is Fig. 2 B zoomed-in views；
Fig. 5 is Fig. 2 C zoomed-in views；
Fig. 6 is the structural representation of rotary compacting device；
Fig. 7 is the structural representation of rotor plate；
Fig. 8 is the structural representation of rib positioning compression plate；
Description of reference numerals：The trapezoidal riveting die tires of 1-, 2- locating surfaces, 3- angles location-plate, 4- rotary compacting devices, 5- bottoms
Bearing, 6- stands, 7- bearing pins, 8- rotor plates, 9- cursors, 10- rotor plate screw rods, 11- pressure strips, 12- cursor screw rods,
13- compact heaps, 14- rib positioning compression plates, 15- rotary screws, 16- pressing plates, 17- skeletons.
Embodiment
The present invention is described in further detail with reference to the accompanying drawings and examples.
The implementation of the present invention：A kind of antenna reflective face framework riveting set, the aerial panel skeleton riveting set by
Trapezoidal riveting die tire 1 is formed, and the locating surface 2 that can place covering is provided with trapezoidal riveting die tire 1, on locating surface 2 respectively
Angle location-plate 3 and rib positioning compression plate 14 are provided with, rotary compacting device 4 is provided with the seamed edge of trapezoidal riveting die tire 1.
The rotary compacting device 4 includes bottom support bracket 5, and two stands 6 are provided with bottom support bracket 5, vertical at two
Rotor plate 8 is provided with by bearing pin 7 between seat 6, cursor 9 is provided with rotor plate 8, rotation is provided with rotor plate 8
Plate screw rod 10, pressure strip 11 is provided with rotor plate screw rod 10, cursor screw rod 12 is provided with cursor 9, rotated
Compact heap 13 is provided with arm screw rod 12.
The rib positioning compression plate 14 is made up of rotary screw 15 and the connection of pressing plate 16.
6~10 rotary compacting devices 4 are provided with trapezoidal riveting die tire 1.
The covering of Reflector Panel is placed on trapezoidal riveting die tire first, then rib is placed on covering, adjusts good position
The bearing of rotary compacting device is fixed installed in correct position, can after all rotary compacting devices are all installed
Rotor plate is first turned into the back side to carry out the riveting work of panel, during riveting, covering and rib are put well, then by rotor plate
The fixed covering of screw rod rotation and rib to come with pressure strip and compact heap is rotated, after all ribs and covering are all fixed
Riveted, the screw rod of compact heap and pressure strip is unclamped after riveting is good, rotary motion plate can decontrol panel, remove panel
Complete riveting work.
In the structure of the present invention, antenna surface coordinates locating and machining is pressed by numerical control after the trapezoidal casting of riveting die tire 1
Face 2, rib positioning hole and rib wire casing are processed by rib position, install rotary compacting device 4 and rib positioning compression plate
14, first all ribs are put well by setting-out position and determined with rotary compacting device 4 and rib positioning compression plate 14 during riveting
Position, is attached into skeleton by rib with angle Support and connecting plate, takes down skeleton, covering is placed on mould tire, then by skeleton 17
It is placed on covering, adjusts good position and positioned with rotary compacting device, covering and skeleton are attached with rivet.
Claims (4)
- A kind of 1. antenna reflective face framework riveting set, it is characterised in that：The antenna reflective face framework riveting set by Trapezoidal riveting die tire（1）Composition, in trapezoidal riveting die tire（1）On be provided with the locating surface that can place covering（2）, in locating surface （2）On be respectively arranged with angle location-plate（3）With rib positioning compression plate（14）, in trapezoidal riveting die tire（1）Seamed edge on set There is rotary compacting device（4）, the rotary compacting device（4）Including bottom support bracket（5）, in bottom support bracket（5）On be provided with two Individual stand（6）, in two stands（6）Between pass through bearing pin（7）It is provided with rotor plate（8）, in rotor plate（8）On be provided with rotation Arm（9）, in rotor plate（8）On be provided with rotor plate screw rod（10）, in rotor plate screw rod（10）On be provided with pressure strip（11）, Cursor（9）On be provided with cursor screw rod（12）, in cursor screw rod（12）On be provided with compact heap（13）.
- 2. antenna reflective face framework riveting set according to claim 1, it is characterised in that：The rib positioning compression Plate（14）By rotary screw（15）And pressing plate（16）Connection composition.
- 3. antenna reflective face framework riveting set according to claim 1, it is characterised in that：In trapezoidal riveting die tire （1）On be provided with 6~10 rotary compacting devices（4）.
- 4. according to the clinching method of the antenna reflective face framework riveting set as described in any one of claims 1 to 3, its spy Sign is：The covering of Reflector Panel is placed on trapezoidal riveting die tire first, then rib is placed on covering, adjustment good position is The bottom support bracket of rotary compacting device is fixed installed in correct position, first by the rotor plate of rotary compacting device during riveting The back side is turned to, covering and rib are put well, then rotor plate is rotated to come to be rotated admittedly with the screw rod on pressure strip and compact heap Determine covering and rib, riveted after all ribs and covering are all fixed, compact heap and pressure strip are unclamped after riveting is good Screw rod, rotary motion plate can decontrol panel, and riveting work can be completed by removing panel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510948327.6A CN105665599B (en) | 2015-12-17 | 2015-12-17 | A kind of antenna reflective face framework clinching method and device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510948327.6A CN105665599B (en) | 2015-12-17 | 2015-12-17 | A kind of antenna reflective face framework clinching method and device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105665599A CN105665599A (en) | 2016-06-15 |
| CN105665599B true CN105665599B (en) | 2017-12-19 |
Family
ID=56297613
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510948327.6A Active CN105665599B (en) | 2015-12-17 | 2015-12-17 | A kind of antenna reflective face framework clinching method and device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105665599B (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106827308B (en) * | 2016-12-12 | 2018-11-09 | 武汉滨湖电子有限责任公司 | A kind of high-precision Shaped-beam reflector antenna processing mold and its processing method |
| CN108666762B (en) * | 2018-05-11 | 2020-06-09 | 中国电子科技集团公司第五十四研究所 | High-precision lightweight triangular antenna panel and manufacturing method thereof |
| CN115502663A (en) * | 2022-09-26 | 2022-12-23 | 沈阳飞机工业（集团）有限公司 | Preparation method of large-scale fork-shaped skin contour |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0956915A2 (en) * | 1998-05-05 | 1999-11-17 | Manuel Torres Martinez | Process and installation for the construction of wings or stabilisers for aeroplanes |
| US6961983B1 (en) * | 2002-08-20 | 2005-11-08 | Cessna Aircraft Company | Tooling for rivet gun |
| CN202934338U (en) * | 2012-11-19 | 2013-05-15 | 中航成飞民用飞机有限责任公司 | Automatic drill-rivet guide device of stringer |
| CN202951825U (en) * | 2012-10-31 | 2013-05-29 | 上海航天精密机械研究所 | Device for rivet pressing launch vehicle tail-end crossbeam and skin |
| CN203061746U (en) * | 2013-01-28 | 2013-07-17 | 上海上飞飞机装备制造有限公司 | Riveting fixture for nose gear door |
| CN205200443U (en) * | 2015-12-17 | 2016-05-04 | 贵州振华天通设备有限公司 | Antenna plane of reflection tabulare frame riveting set |
-
2015
- 2015-12-17 CN CN201510948327.6A patent/CN105665599B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0956915A2 (en) * | 1998-05-05 | 1999-11-17 | Manuel Torres Martinez | Process and installation for the construction of wings or stabilisers for aeroplanes |
| US6961983B1 (en) * | 2002-08-20 | 2005-11-08 | Cessna Aircraft Company | Tooling for rivet gun |
| CN202951825U (en) * | 2012-10-31 | 2013-05-29 | 上海航天精密机械研究所 | Device for rivet pressing launch vehicle tail-end crossbeam and skin |
| CN202934338U (en) * | 2012-11-19 | 2013-05-15 | 中航成飞民用飞机有限责任公司 | Automatic drill-rivet guide device of stringer |
| CN203061746U (en) * | 2013-01-28 | 2013-07-17 | 上海上飞飞机装备制造有限公司 | Riveting fixture for nose gear door |
| CN205200443U (en) * | 2015-12-17 | 2016-05-04 | 贵州振华天通设备有限公司 | Antenna plane of reflection tabulare frame riveting set |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105665599A (en) | 2016-06-15 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105665599B (en) | A kind of antenna reflective face framework clinching method and device | |
| CN203350016U (en) | Rapidly-replaceable wallboard for sub-transonic speed wind tunnel | |
| CN205200443U (en) | Antenna plane of reflection tabulare frame riveting set | |
| CN209491473U (en) | A kind of protective net frame welding tooling | |
| CN204081464U (en) | Ruggedized construction bottom a kind of aluminum alloy mould plate | |
| CN205464941U (en) | Automobile threshold roof beam welding jig | |
| CN204314776U (en) | Frame before detachable touch interactive all-in-one machine | |
| CN208304632U (en) | A kind of LED lamp circular frame automatically grinding mechanism | |
| CN205615011U (en) | All -round squeeze riveter | |
| CN205393352U (en) | Rotatory closing device of antenna panel skeleton riveting | |
| CN205439510U (en) | Anchor clamps of DOME membrane are pasted in vacuum | |
| CN207080767U (en) | Micro-control computer support is used on a kind of intelligent automobile | |
| CN204898075U (en) | A device for panel beating takes shape | |
| CN204935147U (en) | A kind of novel adjustable floating supports | |
| CN104259845A (en) | Mounting tooling for automobile lamp adjusting mechanism | |
| CN105926481B (en) | A kind of fastener for road traffic direction board | |
| CN105736528B (en) | A kind of simplification road traffic direction board fastener | |
| CN201402132Y (en) | Multifunctional detection test table for turning plate of bus | |
| CN210967301U (en) | Plate cutting device for building model | |
| CN205520512U (en) | Large -scale wind -powered electricity generation bearing processing tool | |
| CN205325123U (en) | Gyro wheel disassembling equipment | |
| CN209310707U (en) | A kind of comprehensive detection device of roof of the vehicle | |
| CN203737796U (en) | Punching die for angle iron notches of stainless steel electric control cabinet framework | |
| CN104175138B (en) | The frock of the processing oblique installing hole of thrust block | |
| CN209623542U (en) | A kind of driver's cabin mounting base special gauge |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of invention: A riveting method and device for antenna reflector panel framework Effective date of registration: 20231102 Granted publication date: 20171219 Pledgee: China Construction Bank Corporation Guiyang Chengbei sub branch Pledgor: GUIZHOU ZHENHUA COMMUNICATION EQUIPMENT CO.,LTD. Registration number: Y2023520000062 |