KR101684420B1 - Dolly device for moving a parts assembly for aircraft - Google Patents
Dolly device for moving a parts assembly for aircraft Download PDFInfo
- Publication number
- KR101684420B1 KR101684420B1 KR1020150079676A KR20150079676A KR101684420B1 KR 101684420 B1 KR101684420 B1 KR 101684420B1 KR 1020150079676 A KR1020150079676 A KR 1020150079676A KR 20150079676 A KR20150079676 A KR 20150079676A KR 101684420 B1 KR101684420 B1 KR 101684420B1
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- KR
- South Korea
- Prior art keywords
- frame
- supporting
- assembly
- contact support
- stopper
- Prior art date
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- B64F5/0036—
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- B64F5/0009—
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Abstract
The present invention proposes a Dolly device for moving aircraft airframe parts. A dolly device according to the present invention comprises a frame (20) comprising a plurality of metal square pipes assembled and having a sloped upper surface (22) and a plurality of casters (30) provided on the bottom surface; A plurality of non-slip stoppers (12) provided on a sloped upper surface of the frame, the stoppers (12) having a stopper contact support portion (12e) of a synthetic resin material which contacts and supports the assembly so that the aircraft gas subassembly (A) does not descend along an inclined surface; A plurality of support blocks 14 provided on the upper surface of the frame and having a side block contact support portion 14d of synthetic resin material for supporting the bottom surface of the assembly A; And a plurality of side blocks provided on the upper surface of the frame and including side wall block supporting portions 16d and 16e of a synthetic resin material for supporting the bottom surface and one side surface of the assembly A together. Therefore, the bottom inclined assembly can be moved horizontally and can be sufficiently protected from external impacts.
Description
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an apparatus for moving a gas component of an aircraft, and more particularly, to an apparatus for moving an aircraft component, .
It can be said that an aircraft is assembled by assembling a plurality of parts, and a plurality of parts constituting such an aircraft can be said to have substantially various shapes and sizes. Among these parts, there are many parts which are inclined like an inboard product which is a gas subassembly. Considering the transportation and assembly place and the assembling process, it is preferable that such an inclined assembly is transported while keeping the upper surface horizontal.
However, as a device for transporting such an aircraft component, it can not be found as a transporting tool for transporting a slanted component in a horizontal state as described above. For example, it is possible to consider transferring by using a carrier device for transferring other general parts, which is not preferable in consideration of the characteristics of the parts and the posture when moving.
SUMMARY OF THE INVENTION The present invention has been proposed in view of this point and aims at providing a dolly device particularly suitable for transporting an aircraft assembly having an inclined shape.
It is another object of the present invention to provide a dolly device capable of transporting an assembly in a stable posture and state by preventing inclined aircraft parts from being pushed in the course of transportation.
It is another object of the present invention to provide a dolly device in which an aircraft part to be assembled is not damaged by external force or contact with the transfer device during the transfer process.
According to the present invention, there is provided a dolly device for moving an aircraft airframe component, comprising: a frame including a plurality of metal square pipes assembled therein and having an inclined upper surface and a plurality of casters provided on the bottom surface; A plurality of non-slip stoppers provided on an inclined upper surface of the frame and having a stopper contact support portion of a synthetic resin material that contacts and supports the assembly so that the aircraft gas subassembly does not descend along an inclined surface; A plurality of support blocks provided on the upper surface of the frame and having a side block contact support portion of a synthetic resin material for supporting a bottom surface of the assembly; And a plurality of side blocks provided on the upper surface of the frame and having a side block contact support portion of synthetic resin material for supporting the bottom surface and one side surface of the assembly.
And a handle formed on one side of the frame to be pushed and held by the user.
According to the non-slip stopper of the present invention, the stopper stopper is fixed to the frame. The stopper stopper is fixed to the upper portion of the stopper stopper. The stopper stopper is connected to the stopper stopper, do. Here, the upper plate and the fixing portion are connected by a bolt, and the through-hole of the upper plate through which the bolt passes is shaped into a long hole having a predetermined length. The upper plate can be changed in a certain range, Can respond.
According to the embodiment of the support block in the present invention, the support block is constituted by a support member for supporting the side block contact support portion and a first support means for supporting the support member at the upper portion of the frame.
According to an embodiment of the side block of the present invention, it comprises second support means for supporting the side block contact support on the frame. Wherein the side block contact support comprises a first contact support portion fixed on the second support means and in contact with the upper surface of the assembly, a second contact support portion fixed on the first contact support portion, .
Here, the first contact supporting portion and the second contact supporting portion are fixed by bolts, the through holes of the first contact supporting portion through which the bolts pass are formed in the shape of a long hole having a predetermined length, It is possible to sufficiently absorb the size or position change of the assembly.
According to the present invention as described above, it is possible to maximize the ease of movement by constructing the metal pipe, and it is also understood that the assembled product with the inclined bottom face can be moved while maintaining the horizontal state. Also, it is expected that the parts that come into contact with the assemblies can be sufficiently protected by molding them with synthetic resin material. In addition, according to the present invention, it is expected that an advantage of absorbing a change in size and position of an assembly can be expected.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 shows a dolly device of the present invention, wherein (a) is a plan view and (b) is a side view.
2 is an exemplary view of a non-slip stopper used in the dolly device of the present invention.
3 is an illustration of a base block used in the dolly device of the present invention;
4 is an illustration of a side block used in the dolly device of the present invention.
5 is an exemplary view showing another embodiment of a side block used in the dolly device of the present invention;
Hereinafter, the present invention will be described in more detail based on the embodiments shown in the drawings. First, as shown in FIG. 1, the
A plurality of metal pipes (pipes) are connected to the
As shown in FIG. 1B, when the user holds the
It can be seen that the
First, a plurality of
The
The
A plurality of such
Next, the
A
Next, the
The
Shaped supporting member 16c is fixed to an upper portion of the
On the upper portion of the first
The second
The side blocks 16 having the above-described configuration are provided on the upper surface of the
5 shows a
As described above, according to the present invention, it can be seen that a dolly device is proposed which can most preferably move a part of the assembly A of the aircraft. And, the dolly device of the present invention is expected to have the
It will be apparent to those skilled in the art that various modifications and variations can be made in the present invention without departing from the spirit and scope of the present invention as defined by the appended claims. It is also natural that it should be.
10 ..... dolly unit
12 ..... Non-slip stopper
12a ..... stopper fixing unit
12b .... top plate of stopper
12c ..... extension
12e ..... stopper contact support
14 ..... Bearing block
14a ..... a support block fixing part
14b ..... Base block top plate
14d ..... support block contact support
16 ..... side block
16a ..... side block fixing portion
16b ..... side block top plate
16d.
16e ..... second contact support
20 ..... frame
22 ..... the upper surface of the frame
Claims (6)
A plurality of non-slip stoppers (12) provided on a sloped upper surface of the frame, the stoppers having a stopper contact support portion (12e) of a synthetic resin material that contacts and supports the assembly so that the aircraft gas subassembly (A) does not descend along an inclined surface;
A plurality of support blocks 14 provided on the upper surface of the frame and having a side block contact support portion 14d of synthetic resin material for supporting the bottom surface of the assembly A; And
And a plurality of side blocks provided on the upper surface of the frame and having side wall block support portions (16d, 16e) of a synthetic resin material for supporting the bottom surface and one side surface of the assembly (A).
Further comprising a handle (32) formed on one side of the frame for the user to hold and push.
The non-slip stopper includes a stopper fixing part 12a fixed to the frame, a stopper upper plate 12b fixed to the upper part of the stopper fixing part, and an extension part connecting and supporting the stopper contact supporting part 12e and the upper plate (12c)
Wherein the top plate and the fixing portion are connected by a bolt and the through hole of the top plate through which the bolt passes is formed into a long hole having a predetermined length so that the top plate can be changed in a predetermined range.
The supporting block includes a supporting member 14c for supporting the side block contact supporting portion 14d and a first supporting means for supporting the supporting member 14c at an upper portion of the frame.
Wherein the side block includes second support means for supporting the side block contact support portion on the frame,
The side block contact support comprises a first contact support (16d) fixed on the second support means and in contact with an upper surface of the assembly, a second contact support (16d) fixed on the first contact support and having a second And a contact support portion (16e).
The first contact support portion and the second contact support portion are fixed by bolts and the through holes of the second contact support portion through which the bolt is passed are formed into a long hole having a predetermined length, A possible dolly for moving aircraft parts.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020150079676A KR101684420B1 (en) | 2015-06-05 | 2015-06-05 | Dolly device for moving a parts assembly for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020150079676A KR101684420B1 (en) | 2015-06-05 | 2015-06-05 | Dolly device for moving a parts assembly for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
KR101684420B1 true KR101684420B1 (en) | 2016-12-08 |
Family
ID=57576853
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1020150079676A KR101684420B1 (en) | 2015-06-05 | 2015-06-05 | Dolly device for moving a parts assembly for aircraft |
Country Status (1)
Country | Link |
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KR (1) | KR101684420B1 (en) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0359434A (en) * | 1989-07-27 | 1991-03-14 | Kobe Steel Ltd | Sealing confirming method for pressure-reduced, sealed container |
JP3059434B2 (en) | 1998-03-11 | 2000-07-04 | 三星電子株式会社 | Optical transmission module |
US20050140107A1 (en) * | 2001-04-20 | 2005-06-30 | Gruber Robert V. | Tray and dolly assembly |
JP2006205964A (en) * | 2005-01-31 | 2006-08-10 | Shingo Nishikawa | Article conveying unit |
KR20140020869A (en) * | 2011-01-25 | 2014-02-19 | 웽 성 찬 | Handling and transport system |
-
2015
- 2015-06-05 KR KR1020150079676A patent/KR101684420B1/en active IP Right Grant
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0359434A (en) * | 1989-07-27 | 1991-03-14 | Kobe Steel Ltd | Sealing confirming method for pressure-reduced, sealed container |
JP3059434B2 (en) | 1998-03-11 | 2000-07-04 | 三星電子株式会社 | Optical transmission module |
US20050140107A1 (en) * | 2001-04-20 | 2005-06-30 | Gruber Robert V. | Tray and dolly assembly |
JP2006205964A (en) * | 2005-01-31 | 2006-08-10 | Shingo Nishikawa | Article conveying unit |
KR20140020869A (en) * | 2011-01-25 | 2014-02-19 | 웽 성 찬 | Handling and transport system |
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Payment date: 20191202 Year of fee payment: 4 |