CN204125013U - A kind of erecting by overhang - Google Patents
A kind of erecting by overhang Download PDFInfo
- Publication number
- CN204125013U CN204125013U CN201420564567.7U CN201420564567U CN204125013U CN 204125013 U CN204125013 U CN 204125013U CN 201420564567 U CN201420564567 U CN 201420564567U CN 204125013 U CN204125013 U CN 204125013U
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- hanging
- suspension ring
- crossbeam
- connecting panel
- poly
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Abstract
The utility model belongs to transporation by plane technical field, relates to a kind of erecting by overhang for transporation by plane docking.A kind of erecting by overhang, comprise a hanging crossbeam, suspension ring and poly-ester fibres band, it is characterized in that, two grooved parts (1), hanging board (2) and two pieces of connecting panels (3) are coupled together by bolt and form hanging crossbeam, two grooved part (1) dos-à-doss are placed, centre is added with hanging board (2) and connecting panel (3), hanging board (2) there is hanging hole (7), connecting panel (3) is positioned at hanging crossbeam two ends, respectively there are two suspension ring stringed together (4) at hanging crossbeam two ends, suspension ring (4) one end hangs on connecting panel (3), the other end hangs with set square (5), the two ends of poly-ester fibres band (6) are fixed on the groove on set square (5).The utility model is simple and easy to combination, can regulate length by demand, and docking installed by the aircraft components being applicable to different size, also can be used for short range transport.
Description
Technical field
The utility model belongs to transporation by plane technical field, relates to a kind of erecting by overhang for transporation by plane docking.
Background technology
When transporation by plane, because each segment body of fuselage is long-pending large, mobile difficulty, not easily dock, cause transporation by plane to be wasted time and energy, also easily collide with airplane component.
Summary of the invention
The purpose of this utility model is to provide a kind of erecting by overhang of transporation by plane, to ensure the simple and safe of transporation by plane.Can not be worn and torn aircraft configuration and enamelled coating, need not design the sling point being specifically designed to assembling aboard.
The utility model comprises hanging crossbeam, suspension ring and a poly-ester fibres band, two grooved parts 1, hanging board 2 and two pieces of connecting panels 3 are coupled together by bolt and form hanging crossbeam, two grooved part 1 dos-à-doss are placed, centre is added with hanging board 2 and connecting panel 3, hanging board 2 has hanging hole 7, connecting panel 3 is positioned at hanging crossbeam two ends.Respectively there are two suspension ring stringed together 4 at hanging crossbeam two ends, and suspension ring 4 one end hangs on connecting panel 3, and the other end hangs with set square 5, and the two ends of poly-ester fibres band 6 are fixed on the groove on set square 5.
The utility model hanging adopts poly-ester fibres band, can not cause damage, can not cause scratch of colliding with to the aircraft skin sprayed paint during lifting aircraft to aircraft skin profile; Two hanging with the use of, for large aircraft components assembling docking safe and reliable, save time, save manpower, reduce costs; Hanging is simple and easy to combination, can regulate length by demand, and docking installed by the aircraft components being applicable to different size, also can be used for short range transport.
Accompanying drawing explanation
Accompanying drawing 1 is schematic diagram of the present invention;
Accompanying drawing 2 is suspension ring 4 of the present invention and connecting panel 3 connection diagram.
Detailed description of the invention
The utility model is made up of hanging crossbeam, 4 suspension ring and a poly-ester fibres band.Two grooved parts 1, hanging board 2 and two pieces of connecting panels 3 are coupled together by bolt and form hanging crossbeam, two grooved part 1 dos-à-doss are placed, and centre is added with hanging board 2 and connecting panel 3, and hanging board 2 is positioned in the middle of hanging crossbeam, hanging board 2 has hanging hole 7, connecting panel 3 is positioned at hanging crossbeam two ends.Respectively there are two suspension ring stringed together 4 at hanging crossbeam two ends, and suspension ring 4 one end hangs on connecting panel 3, and the other end hangs with set square 5, and poly-ester fibres band 6 is through the groove on set square 5, and poly-ester fibres band 6 is coupled together with hanging crossbeam by set square 5 and suspension ring 4.Connect suspension ring 4 bolt 8 safety locking of set square 5, unthread bolts 8, can take off poly-ester fibres band 6, during use, can choose the poly-ester fibres band 6 of different size by demand.
Hanging can regulate length by demand, unthread bolts 8, just can pull down poly-ester fibres band, the poly-ester fibres band of a configurable multiple size of hanging crossbeam, and docking installed by the aircraft components being applicable to different size.If two hangings are with the use of, the large long body parts safety and reliability of lifting diameter.
Claims (1)
1. an erecting by overhang, comprise a hanging crossbeam, suspension ring and poly-ester fibres band, it is characterized in that, two grooved parts (1), hanging board (2) and two pieces of connecting panels (3) are coupled together by bolt and form hanging crossbeam, two grooved part (1) dos-à-doss are placed, centre is added with hanging board (2) and connecting panel (3), hanging board (2) there is hanging hole (7), connecting panel (3) is positioned at hanging crossbeam two ends, respectively there are two suspension ring stringed together (4) at hanging crossbeam two ends, suspension ring (4) one end hangs on connecting panel (3), the other end hangs with set square (5), the two ends of poly-ester fibres band (6) are fixed on the groove on set square (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420564567.7U CN204125013U (en) | 2014-09-28 | 2014-09-28 | A kind of erecting by overhang |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420564567.7U CN204125013U (en) | 2014-09-28 | 2014-09-28 | A kind of erecting by overhang |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204125013U true CN204125013U (en) | 2015-01-28 |
Family
ID=52381388
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420564567.7U Active CN204125013U (en) | 2014-09-28 | 2014-09-28 | A kind of erecting by overhang |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204125013U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106429797A (en) * | 2016-12-15 | 2017-02-22 | 南通华夏飞机工程技术股份有限公司 | Vertical-fin hanger |
-
2014
- 2014-09-28 CN CN201420564567.7U patent/CN204125013U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106429797A (en) * | 2016-12-15 | 2017-02-22 | 南通华夏飞机工程技术股份有限公司 | Vertical-fin hanger |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |