KR20160117948A - Wing component rack for aircraft - Google Patents
Wing component rack for aircraft Download PDFInfo
- Publication number
- KR20160117948A KR20160117948A KR1020150046052A KR20150046052A KR20160117948A KR 20160117948 A KR20160117948 A KR 20160117948A KR 1020150046052 A KR1020150046052 A KR 1020150046052A KR 20150046052 A KR20150046052 A KR 20150046052A KR 20160117948 A KR20160117948 A KR 20160117948A
- Authority
- KR
- South Korea
- Prior art keywords
- rack
- support
- connection
- frame
- pin insertion
- Prior art date
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Images
Classifications
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- B64F5/0036—
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
- B60P3/06—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles
- B60P3/11—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles for carrying aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
- B60P3/40—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying long loads, e.g. with separate wheeled load supporting elements
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62B—HAND-PROPELLED VEHICLES, e.g. HAND CARTS OR PERAMBULATORS; SLEDGES
- B62B3/00—Hand carts having more than one axis carrying transport wheels; Steering devices therefor; Equipment therefor
- B62B3/10—Hand carts having more than one axis carrying transport wheels; Steering devices therefor; Equipment therefor characterised by supports specially adapted to objects of definite shape
- B62B3/102—Hand carts having more than one axis carrying transport wheels; Steering devices therefor; Equipment therefor characterised by supports specially adapted to objects of definite shape the objects being of elongated shape, e.g. rods or golf clubs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62B—HAND-PROPELLED VEHICLES, e.g. HAND CARTS OR PERAMBULATORS; SLEDGES
- B62B5/00—Accessories or details specially adapted for hand carts
Abstract
The present invention relates to a rack for detachable aircraft wing parts, and more particularly to a rack for a detachable aircraft wing component which is provided with a detachable member for detachable attachment to an adjacent rack, Lt; / RTI >
Description
The present invention relates to a rack for detachable aircraft wing parts, and more particularly to a rack for detachable aircraft wing parts having a detachable member so that the rack body can be detached from an adjacent rack.
Aircraft wing parts are stringers.
Stringers are longitudinal and circumferential stiffeners used inside the fuselage of an aircraft.
These stringers are formed in a long strip shape and vary in length from 1.5m to 20m.
When a rack for carrying or transporting such a stringer is manufactured, it is manufactured on the basis of the longest wing parts and occupies a lot of space in storage. Further, there is a problem that such a rack must be transported to a large vehicle even when it is transported.
SUMMARY OF THE INVENTION It is an object of the present invention to provide a rack for detachable aircraft wing parts which can be commonly used for various lengths of wing parts and which can facilitate the transportation of racks.
In order to achieve the above object, a rack for detachable aircraft wing parts according to the present invention includes a rack body, and the rack body is provided with a detachable member so as to be detachably attached to an adjacent rack.
The rack is formed with a connecting rod projecting therefrom. The connecting rod is provided with a first connecting pin insertion hole into which the connecting pin is inserted. The adjacent rack includes a connecting rod inserting hole into which the connecting rod is inserted, A second connection pin insertion hole may be formed so as to communicate with the second connection pin insertion hole.
According to the rack for detachable aircraft wing parts of the present invention as described above, the following effects can be obtained.
The rack body is provided with a detachable member so as to be detachably attached to the adjacent rack, and can be commonly used for blade parts of various lengths, so that the rack can be easily transported.
The rack is formed with a connecting rod projecting therefrom. The connecting rod is provided with a first connecting pin insertion hole into which the connecting pin is inserted. The adjacent rack includes a connecting rod inserting hole into which the connecting rod is inserted, The second connection pin insertion hole is formed to be communicated with the first connection pin insertion hole, so that the connection pin can be easily manufactured and the connection operation can be facilitated.
1 is a perspective view of a rack for a detachable aircraft wing component according to a preferred embodiment of the present invention.
2 is an enlarged, fragmentary perspective view of a rack for a detachable aircraft wing component in accordance with a preferred embodiment of the present invention.
Figure 3 is a side view of a rack for detachable aircraft wing parts according to a preferred embodiment of the present invention,
4 is a perspective view showing a folded state of a rack for detachable aircraft wing parts according to a preferred embodiment of the present invention.
5 is a perspective view illustrating a plurality of racks for detachable aircraft wing parts according to a preferred embodiment of the present invention.
FIG. 6 is a perspective view showing a use state of a detachable aircraft wing part rack according to a preferred embodiment of the present invention; FIG.
Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings.
For reference, the same components as those of the conventional art will be described with reference to the above-described prior art, and a detailed description thereof will be omitted.
1 to 6, the detachable aircraft wing component rack of the present embodiment includes a
1 and 2, the
The
The
Four
The support
The support
Therefore, the support stand
The first
The first
The first
The
Two
Preferably, the
The
The
The lower portion of the
The lower end of the
The lower end of the
The
4, the
The second hinge fastening hole is disposed on the upper portion of the second support post fixing
The second hinge fastening hole and the second support post fixing
The hinge (H) is inserted into the first and second hinge fastening holes (122), and the support table (200) is rotatably installed on the bottom (100). In other words, the support table 200 is foldably installed on the
When the support table 200 is erected, the support table fixing pins p are inserted into the first and second support table fixing
The support pin fixing pin p may be a bolt formed with a head portion and may be fixed through a nut after being inserted into the first and second support
As described above, the locking structure for fixing the position of the support table 200 is simple and easy to manufacture.
When the
The
The
The
The plurality of
Therefore, a wing part such as a stringer s can be loaded on each of the plurality of
In addition, the
The
The
A first connection
A connection
The connecting rod insertion holes 113 are formed in the forward and backward directions, and are formed so as to open frontward or rearward.
The second connection
The connection pin may be a bolt formed with a head portion and may be fixed through a nut after being inserted into the first and second connection pin insertion holes 112,
As described above, the connecting rod may be formed in the front of the
As described above, the structure of the detachable member is simple and easy to manufacture, and the connection operation can be facilitated.
A
Further, the
Hereinafter, the operation of the present embodiment having the above-described configuration will be described.
2 and 3, when the rack is used, the support table 200 is vertically installed, and then the support table fixing pin p is inserted into the first and second support table fixing pin insertion holes 123 and 213. As a result, the support table 200 is maintained in an upright state. Further, the support base fixing pin p may be fixed with a nut or the like so as not to be detached. A stringer s having a long length is placed on the
When the rack is not used, the support pin fixing pin p is pulled out from the first and second support pin fixing pin insertion holes 123 and 213 so that the
If you are carrying short stringers (s), use one rack to carry them.
When the stringer s having a long length is to be transported, as shown in FIG. 5, the connection pins are inserted into the first and second connection pin insertion holes 112 and 114 to connect the two racks. Therefore, as shown in Fig. 6, a stringer s having a longer length can be effectively carried. And then a nut or the like may be fastened to the connection pin so that the connection pin is not released.
When the rack is not used or the rack is transported, the connecting pins are pulled out from the first and second connecting pin insertion holes 112 and 114 to separate the two racks. Therefore, the space occupied by the rack can be minimized when the rack is not in use or transported.
It will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the present invention as defined by the following claims .
DESCRIPTION OF REFERENCE NUMERALS
100: bottom part 200: support part
1000: Rack body
Claims (2)
Wherein the rack body is provided with a detachable member so as to be detachable to an adjacent rack.
The rack body is formed with a connecting rod protruding therefrom,
The connection rod may have a first connection pin insertion hole into which the connection pin is inserted,
Wherein the adjacent rack has a connection rod insertion hole into which the connection rod is inserted and a second connection pin insertion hole to communicate with the connection rod insertion hole.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020150046052A KR20160117948A (en) | 2015-04-01 | 2015-04-01 | Wing component rack for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020150046052A KR20160117948A (en) | 2015-04-01 | 2015-04-01 | Wing component rack for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
KR20160117948A true KR20160117948A (en) | 2016-10-11 |
Family
ID=57162018
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1020150046052A KR20160117948A (en) | 2015-04-01 | 2015-04-01 | Wing component rack for aircraft |
Country Status (1)
Country | Link |
---|---|
KR (1) | KR20160117948A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107757672A (en) * | 2017-10-23 | 2018-03-06 | 晨龙飞机(荆门)有限公司 | A kind of adjustable aircraft wing handling device for supporting and lifting position and height |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5477596A (en) | 1992-12-23 | 1995-12-26 | The Boeing Company | Stringer/clip placement and drilling |
-
2015
- 2015-04-01 KR KR1020150046052A patent/KR20160117948A/en not_active Application Discontinuation
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5477596A (en) | 1992-12-23 | 1995-12-26 | The Boeing Company | Stringer/clip placement and drilling |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107757672A (en) * | 2017-10-23 | 2018-03-06 | 晨龙飞机(荆门)有限公司 | A kind of adjustable aircraft wing handling device for supporting and lifting position and height |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
A201 | Request for examination | ||
E902 | Notification of reason for refusal | ||
E601 | Decision to refuse application |