KR200484987Y1 - Rivetting device for aircraft body - Google Patents
Rivetting device for aircraft body Download PDFInfo
- Publication number
- KR200484987Y1 KR200484987Y1 KR2020150002259U KR20150002259U KR200484987Y1 KR 200484987 Y1 KR200484987 Y1 KR 200484987Y1 KR 2020150002259 U KR2020150002259 U KR 2020150002259U KR 20150002259 U KR20150002259 U KR 20150002259U KR 200484987 Y1 KR200484987 Y1 KR 200484987Y1
- Authority
- KR
- South Korea
- Prior art keywords
- frame
- rod
- supported
- cam
- upper frame
- Prior art date
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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
-
- 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
- B21J15/142—Aerospace structures
-
- 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
- B21J15/30—Particular elements, e.g. supports; Suspension equipment specially adapted for portable riveters
Abstract
The present invention relates to a device for riveting aircraft airframe components. The apparatus of the present invention comprises: a frame (F) having an upper frame and a lower frame; A hydraulic cylinder (14) having a hydraulic booster (12) amplified by pneumatic pressure and having a cylinder rod (16) linearly reciprocating in the horizontal direction and supported by the frame; A cam rod 20 which performs a linear reciprocating motion in the same direction by the hydraulic cylinder and has a cam curved surface formed on the bottom surface and supported by the upper frame; A needle bearing provided at an upper end portion thereof can be moved downward due to rolling contact with the curved surface of the cam, and is supported so as to be movable in the vertical direction by the upper frame, and an upper jaw 52 for pressing the upper end of the rivet A vertically moving rod 30; A screw shaft 40 screwed to the lower frame and adjustable in a vertical direction, and a lower jaw 54 for supporting a lower end of the rivet at an upper end thereof; And a spring (34) interposed between the upper and lower moving rods and the upper frame to move the downwardly moved up and down moving rod upward.
Description
The present invention relates to an riveting device for an aircraft, and more particularly, to an riveting device for an aircraft, which is capable of providing sufficient pressure while having a compact size while converting a leftward / rightward motion into a vertical motion, To an adjustable riveting device for an aircraft airframe.
The airframe of the aircraft has many parts made by connecting several plates with rivets. It can be said that the riveting for forming such an aircraft airframe is practically carried out by a skilled person. However, it is more desirable to have a device having a condition such as a stroke for riveting and a most desirable force in practice.
Korean Patent No. 10-0915372 discloses a riveting device for a skins of a warping machine, but this is only a detailed description of a shooting device including a supply of rivets and a pneumatic machine. In other words, there is no technical proposal regarding the mechanical construction for pressing the rivet.
In the case of riveting a plate-like member forming the airframe of an aircraft, riveting is preferably carried out with a constant force and with a constant stroke. And it is expected that such a riveting device can be more advantageously practically miniaturized.
The object of the present invention is to provide a device capable of riveting the aircraft airframe by optimally adjusting the distance between the upper jaw and the lower jaw as it is possible to rivet with a certain force .
Another object of the present invention is to provide a riveting device for a compact aircraft airframe.
The aircraft gas riveting apparatus of the present invention comprises: a frame having an upper frame and a lower frame; A hydraulic cylinder having a hydraulic booster amplified by pneumatic pressure and having a cylinder rod reciprocating linearly in a horizontal direction and supported by the frame; A cam rod that performs a linear reciprocating motion in the same direction by the hydraulic cylinder and has a cam curved surface formed on the bottom surface thereof and supported by the upper frame; A needle bearing provided at an upper end portion of the needle bar can be moved downward by rolling contact with the cam curved surface and is supported so as to be movable up and down by the upper frame, ; A screw shaft which is screwed to the lower frame and is adjustable in the vertical direction, and a lower jaw supporting the lower end of the rivet is installed at an upper end; And a spring interposed between the upper and lower moving rods and the upper frame to move the downwardly moved up and down moving rod upward.
The cam rod is preferably supported by a plurality of needle bearings rotatably supported on the upper frame such that the upper and lower surfaces thereof are in rolling contact with each other.
And a clamping means for holding the screw shaft screwed to the lower frame in a fixed position.
According to the present invention as described above, riveting is performed with a predetermined force and stroke by the up-and-down moving rod moving downward with the hydraulic cylinder as a power source. Therefore, it can be said that there is a merit that the rivetting with high reliability of the product becomes possible.
Further, by installing the hydraulic cylinder in the horizontal direction, it is possible to lower the overall height of the apparatus, and it is also expected that a compact apparatus can be provided. In addition, since the vertical height of the screw shaft can be easily adjusted, it is easy to control the height of the riveting space where the riveting is practically performed.
In the present invention, since a component reciprocating in the left and right horizontal directions is held in rolling contact by a needle bearing, a riveting device is realized that minimizes wear and damage based on the noise while minimizing noise.
1 is a side view of the inventive device;
2 is a front view of the inventive device;
3 is an enlarged view of the upper part of the inventive device;
4 is an enlarged view of the lower part of the inventive device;
Hereinafter, the present invention will be described in more detail based on the embodiments shown in the drawings. As shown in FIGS. 1 and 2, the riveting apparatus of the present invention includes a frame F fixed on a table T having a predetermined height, Is moved in the vertical direction toward the
The frame F is provided on the table T and a plurality of foot switches FS are provided on the table T. A solenoid valve S ) Are also installed. The foot switch FS is for allowing a pneumatic pressure supplied from a pneumatic source (compressor) AC to be distributed by a solenoid valve S, for example. For example, when the first foot switch FSa is turned on, the solenoid valve S causes the air pressure (compressed air) supplied from the air pressure source AC to flow through the first path La, When the switch FSc is turned on, the solenoid valve S causes the pneumatic pressure supplied from the pneumatic source AC to be supplied through the second path Lb. When the second foot switch FSb is turned on, the solenoid valve S S operate to stop the supply of air pressure.
The first path La is connected to the
3, which is an enlarged view of FIG. 2, will be described below. The
A cam
A needle bearing 32 is rotatably supported at an upper end of the up-and-down moving
It will be appreciated that the up-and-down moving
A
Here, the
Therefore, when the
As can be seen from the above description, the
The provision of the
As shown in Fig. 4, a
A fixed
The
At the upper end of the
Hereinafter, a process of performing riveting using the apparatus of the present invention will be briefly described. First, the two plates to be subjected to riveting are substantially drilled, and they are put between the
Therefore, the
By this process, the two plates forming the airframe of the aircraft can be riveted. When this process is completed, the third foot switch FSc is depressed so that the compressed air in the air pressure source AC flows through the second path La . By the air inflow in this direction, the
At this time, as the force pressing the
It will be appreciated that various modifications are possible to those of ordinary skill in the art within the scope of the basic technical idea of the present invention having the above-described constitution, and the scope of protection of the present invention is not limited to the scope of the appended utility model registration request And the like.
12 ..... Hydraulic booster
14 ..... Hydraulic cylinder
16 ..... cylinder rod
17 ..... Connection pin
20 ..... Camload
22 ..... cam curved surface
24a, 24b ..... Needle bearings
30 ..... Moving up and down
32 ...... Needle bearing
34 ..... spring
52 ..... Top Joo
54 ..... Hajo Joo
F ..... frame
Fd ..... subframe
Fu ..... upper frame
FS ..... Footswitch
T ..... table
Claims (3)
A hydraulic cylinder having a hydraulic booster amplified by pneumatic pressure and having a cylinder rod reciprocating linearly in a horizontal direction and supported by the frame;
A cam rod that performs a linear reciprocating motion in the same direction by the hydraulic cylinder and has a cam curved surface formed on the bottom surface thereof and supported by the upper frame;
A needle bearing provided at an upper end portion of the needle bar can be moved downward by rolling contact with the cam curved surface and is supported so as to be movable up and down by the upper frame, ;
A screw shaft which is screwed to the lower frame and is adjustable in the vertical direction, and a lower jaw supporting the lower end of the rivet is installed at an upper end; And
And a spring interposed between the upper and lower moving rods and the upper frame to move the downwardly moved up and down rod upward;
Wherein the cam rod is supported by a plurality of needle bearings rotatably supported on the upper frame such that the upper surface and the lower surface thereof are in rolling contact with each other.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR2020150002259U KR200484987Y1 (en) | 2015-04-09 | 2015-04-09 | Rivetting device for aircraft body |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR2020150002259U KR200484987Y1 (en) | 2015-04-09 | 2015-04-09 | Rivetting device for aircraft body |
Publications (2)
Publication Number | Publication Date |
---|---|
KR20160003603U KR20160003603U (en) | 2016-10-19 |
KR200484987Y1 true KR200484987Y1 (en) | 2017-11-15 |
Family
ID=57234153
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR2020150002259U KR200484987Y1 (en) | 2015-04-09 | 2015-04-09 | Rivetting device for aircraft body |
Country Status (1)
Country | Link |
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KR (1) | KR200484987Y1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR102292568B1 (en) | 2021-02-25 | 2021-08-24 | (주)한얼시스템 | Jig system for aircraft assembly |
Families Citing this family (7)
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CN108971411B (en) * | 2018-08-27 | 2023-10-10 | 福州大学 | Electromagnetic riveting device and method with controllable projectile body position |
CN109261881A (en) * | 2018-10-30 | 2019-01-25 | 福州大学 | High speed nailing attachment device and connection method |
CN109248964A (en) * | 2018-10-30 | 2019-01-22 | 福州大学 | A kind of no rivet connector and its working method |
CN109079079A (en) * | 2018-10-30 | 2018-12-25 | 福州大学 | Electromagnetism self-piercing riveting device and clinching method |
KR102005228B1 (en) * | 2019-03-29 | 2019-10-01 | 한경무 | Caulking device for probe pin using inspecting electronic parts |
KR102164448B1 (en) | 2019-08-21 | 2020-10-13 | 이경근 | Riveting device |
CN114769439A (en) * | 2022-01-06 | 2022-07-22 | 宁夏宇成蓝天环保输送设备有限公司 | Fan impeller riveting device |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2000135541A (en) * | 1998-10-28 | 2000-05-16 | Fuji Heavy Ind Ltd | Riveting method and device therefor |
JP2002178087A (en) * | 2000-12-07 | 2002-06-25 | Sakamura Mach Co Ltd | Heading forming machine |
KR200349914Y1 (en) * | 2004-01-30 | 2004-05-17 | (주)마이크로 갤럭시 | A riveting machine with a hydraulic booster |
-
2015
- 2015-04-09 KR KR2020150002259U patent/KR200484987Y1/en active IP Right Grant
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2000135541A (en) * | 1998-10-28 | 2000-05-16 | Fuji Heavy Ind Ltd | Riveting method and device therefor |
JP2002178087A (en) * | 2000-12-07 | 2002-06-25 | Sakamura Mach Co Ltd | Heading forming machine |
KR200349914Y1 (en) * | 2004-01-30 | 2004-05-17 | (주)마이크로 갤럭시 | A riveting machine with a hydraulic booster |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR102292568B1 (en) | 2021-02-25 | 2021-08-24 | (주)한얼시스템 | Jig system for aircraft assembly |
Also Published As
Publication number | Publication date |
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KR20160003603U (en) | 2016-10-19 |
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