CN2441738Y - Mooring device for aviation goods - Google Patents
Mooring device for aviation goods Download PDFInfo
- Publication number
- CN2441738Y CN2441738Y CN 00240581 CN00240581U CN2441738Y CN 2441738 Y CN2441738 Y CN 2441738Y CN 00240581 CN00240581 CN 00240581 CN 00240581 U CN00240581 U CN 00240581U CN 2441738 Y CN2441738 Y CN 2441738Y
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- CN
- China
- Prior art keywords
- goods
- utility
- model
- swivel arm
- caused
- 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.)
- Expired - Lifetime
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Abstract
The utility model relates to a mooring device for aviation goods. At present, ropes are widely used for fixing aviation goods in markets; because of the expansion and contraction of the ropes, the goods are caused to swing so that danger is caused; the utility model uses the organic match of a rotating arm, a rotating shaft and a support bar; when the rotating arm rotates to a certain position, a fixing strap is caused to generate self-lock in use; when the rotating arm rotates to another position, the self-lock of the fixing strap is relieved to pull the fixing strap so as to avoid harm brought by using knots. The utility model has the advantages of easy use, no knot, no looseness, etc.
Description
The utility model relates to a kind of aviation goods mooring gear.
At present, widely used on the market is with cable goods to be fixed in the phase box, in its use, owing to knot causes retractility largely, so after goods rocks, make whole hawser produce to a certain degree loosening, cause institute's restraint of loads loosening even rock, cause great danger.Therefore, people urgently wish to have a kind of novel goods mooring gear to come out, and it is restraint of loads easily, can not produce loosening again.
The purpose of this utility model is to provide a kind of aviation goods mooring gear.
The utility model is achieved through the following technical solutions, it comprises: formations such as permanent seat, swivel arm, connecting panel, spring clip, spring, dead bolt, snap close, strut bar, rotating shaft, partition rod, restraint zone, spring clip, spring, dead bolt, strut bar are arranged on the swivel arm, partition rod, connecting panel, snap close, rotating shaft are arranged on the permanent seat, and swivel arm is connected with permanent seat by rotating shaft.
The utility model is described in further detail below in conjunction with accompanying drawing:
Fig. 1 is the part sectional view under the utility model releasing orientation
Fig. 2 is the part sectional view under the utility model tension
In the accompanying drawing, 1 is that permanent seat, 2 is that spring clip, 3 is that spring, 4 is that dead bolt, 5 is that swivel arm, 6 is that turning cylinder, 7 is that strut bar, 8 is that connecting panel, 9 is that snap close, 10 is that partition rod, 11 is a restraint zone.
As shown in Figure 1, an end of a restraint zone 11 passes partition rod 10, around the outside of two strut bars 7, rotating shaft 6, passes wherein strut bar 7 inboards again and is clipped in and turns back between clamping band 11 and the strut bar 7 and become free end (as shown in Figure 1); One end of another clamping band 11 is fixed on the connecting panel 8.Article two, the other end of clamping band 11 is respectively equipped with the groove button.During use, the hold down groove internal fixation that clamping band 11 is provided with on the tank top plate of groove button one end reeve aircraft storehouse is good, the fixed network that makes clamping band 11 be covered in restraint of loads puts, and swivel arm 5 is placed position shown in Figure 1, the free end of pulling clamping band 11, make the loose part tension of clamping band 12, rotate swivel arm 5, become state shown in Figure 2, the antagonistic force of the upper limb circular arc of snap close 9 retreats dead bolt 4, and compression spring 3 puts in the snap close 9 dead bolt 4 under the elastic force effect at spring 3 when the position of dead bolt arrives snap close 9 simultaneously, and locking swivel arm 5 makes it and can not rotate.At this moment, clamping band 11 is further strained, and the free end of clamping band 11 forms self-locking owing to be subjected to outside clamping band 11 pressure effects, thereby stretchy clamping band 11 not.When promoting dead bolt 4 compression springs 3, make dead bolt 4 leave snap close 9 with external force.Thereby when allowing swivel arm 5 turn to as shown in Figure 1 state, can make clamping band 11 loose with the free end opposite end on the pulling clamping band 11, thereby untie whole mooring gear.
The utlity model has easy to use, no knot, do not produce loosening etc. excellent The point.
Claims (1)
1, a kind of aviation goods mooring gear, it comprises: permanent seat (1), swivel arm (5), spring clip (2), spring (3), restraint zone (11), partition rod (10), connecting panel compositions such as (8), it is characterized in that swivel arm (5) is provided with dead bolt (4), strut bar (7), permanent seat (1) is provided with snap close (9), and permanent seat (1) is connected by turning cylinder (6) with swivel arm (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 00240581 CN2441738Y (en) | 2000-10-11 | 2000-10-11 | Mooring device for aviation goods |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 00240581 CN2441738Y (en) | 2000-10-11 | 2000-10-11 | Mooring device for aviation goods |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2441738Y true CN2441738Y (en) | 2001-08-08 |
Family
ID=33601199
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 00240581 Expired - Lifetime CN2441738Y (en) | 2000-10-11 | 2000-10-11 | Mooring device for aviation goods |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2441738Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101758922B (en) * | 2008-12-23 | 2012-04-25 | 江西洪都航空工业集团有限责任公司 | Retractable external equipment hanging bracket |
| CN101711213B (en) * | 2007-06-15 | 2013-06-19 | 空中客车运营公司 | Conveyor device intended in particular for luggage in an aircraft hold |
-
2000
- 2000-10-11 CN CN 00240581 patent/CN2441738Y/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101711213B (en) * | 2007-06-15 | 2013-06-19 | 空中客车运营公司 | Conveyor device intended in particular for luggage in an aircraft hold |
| CN101758922B (en) * | 2008-12-23 | 2012-04-25 | 江西洪都航空工业集团有限责任公司 | Retractable external equipment hanging bracket |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |