CN201484659U - Fastening rope for airplane rescue - Google Patents
Fastening rope for airplane rescue Download PDFInfo
- Publication number
- CN201484659U CN201484659U CN2009201779629U CN200920177962U CN201484659U CN 201484659 U CN201484659 U CN 201484659U CN 2009201779629 U CN2009201779629 U CN 2009201779629U CN 200920177962 U CN200920177962 U CN 200920177962U CN 201484659 U CN201484659 U CN 201484659U
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- CN
- China
- Prior art keywords
- aircraft
- strap
- rigging
- master tape
- rescue
- 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
A fastening rope for airplane rescue comprises a main strap, an auxiliary strap and a fastening strap. The two ends of the main strap are connected with the auxiliary strap by a detachable device, and one end of the fastening strap is connected with the main strap by the detachable device. A airplane bundling and fastening rope of high performance is made by combining flexible and flat braces and suspending accessories of high strength and high technique. The utility model has the advantages of light weight, high strength and simple operation. The utility model prevents the damage of traditional bundling ropes, such as steel wires, etc to airplane bodies.
Description
Technical field
A kind of rigging that fastens mainly uses when aircraft is rescued.
Background technology
Along with the progress in epoch, the use of aircraft is day by day frequent, and meanwhile, airplane fault increases relatively.When the aircraft et out of order, need rapid enforcement to rescue, rush to repair, and hold in the palm from the scene of the accident rapidly.In the past when aircraft is rescued, the carrying trailer transports out of the position of fault with aircraft after aircraft is held up, because the fuselage deadweight is bigger, center of gravity is higher, and stable extreme difference in the delivery way causes the secondary injury to aircraft easily, the rescue group adopts binding riggings such as steel rope that fuselage is fixed more, because wirerope diameter is less and very hard, thus less with the airframe surface contact area, easily fuselage is weighed wounded.Simultaneously, hard steel wire is unfavorable for the binding operation, and also is difficult to preserve and utilize with the steel wire of crossing.
The utility model content
The purpose of this utility model provides a kind of in light weight, the intensity height, and high performance airplane binding simple to operate fastens the rigging product.The flat suspender belt and the high strength technology suspension member of softness are combined, formed a kind of type aircraft binding and fasten the rigging product, overcome of the injury of tradition binding riggings such as steel wire fuselage.
In order to reach above-mentioned technique effect, the utility model provides following technical scheme:
The aircraft rescue fastens rigging, comprises master tape, subband, tight tying; Described master tape two ends link to each other with the subband two ends respectively by detachable apparatus, and described tight tying one end links to each other with master tape by detachable apparatus.
Master tape comprises flat band, is connected in a plurality of suspension ring on the flat band and is connected in flat fastener with an end.
Subband comprises flat band and is connected in flat suspension hook with an end.
Fasten and have two, comprise flat band, be connected in flat band upper end suspension hook, be connected in the shackle and the fastener of flat band lower end.
During use, around the aircraft top, subband is around aircraft belly with master tape, the suspension ring of correct position link to each other on suspension hook on the subband and the master tape, the subband other end links to each other with fastener on the master tape, and progressively tightens up flat band on the subband by fastener, thereby with firm the tying up of aircraft.The suspension ring of correct position link to each other on the suspension hook of tight tying upper end and the master tape, the shackle of tight tying lower end links to each other with the carrying trailer, progressively tightens up flat band on the tight tying by the fastener on the tight tying, thereby the aircraft solid is got up, aircraft and trailer are become one, guarantee the safety rescue of aircraft.
According to the binding of the aircraft of technical solutions of the utility model manufacturing fasten rigging have in light weight, the intensity height, advantage simple to operate, and bundle easy to operate, long service life.
Description of drawings
Accompanying drawing is used to provide further understanding of the present utility model, and constitutes the part of specification sheets, is used from explanation the utility model with embodiment one of the present utility model, does not constitute restriction of the present utility model.In the accompanying drawings:
What Fig. 1 was that aircraft rescue fastens rigging is scheme drawing;
Fig. 2 is the scheme drawing of master tape;
Fig. 3 is the scheme drawing of subband;
Fig. 4 is the scheme drawing of tight tying.
The specific embodiment
Below in conjunction with accompanying drawing preferred embodiment of the present utility model is described, should be appreciated that preferred embodiment described herein only is used for description and interpretation the utility model, and be not used in qualification the utility model.
According to Fig. 1-shown in Figure 4, realize the utility model moral technical scheme by the following method:
With master tape 1 around the aircraft top, subband 2 is around aircraft belly, the suspension ring 7 of correct position link to each other on suspension hook 9 on the subband 2 and the master tape 1, the master tape of subband 2 other ends and master tape 1 is flat to link to each other with the fastener 6 on 5, and progressively tighten up flat on the subband 2 by fastener 6 and be with 8, thereby with firm the tying up of aircraft.The suspension ring 7 of correct position link to each other on the suspension hook 11 of tight tying 3 upper ends and the master tape 1, the shackle 13 of tight tying 3 lower ends links to each other with carrying trailer 4, progressively tighten up flat on the tight tying 3 by the fastener on the tight tying 3 12 and be with 10, thereby the aircraft solid is got up, aircraft and carrying trailer 4 are become one, guarantee the safety rescue of aircraft.
Claims (4)
1. an aircraft rescue fastens rigging, it is characterized in that: described aircraft rescue fastens rigging and comprises master tape, subband, tight tying; Described master tape two ends link to each other with the subband two ends respectively by detachable apparatus, and described tight tying one end links to each other with master tape by detachable apparatus.
2. aircraft rescue according to claim 1 fastens rigging, and it is characterized in that: described master tape comprises flat band, is connected in a plurality of suspension ring on the flat band and is connected in flat fastener with an end.
3. aircraft rescue according to claim 1 fastens rigging, and it is characterized in that: described subband comprises flat band and is connected in flat suspension hook with an end.
4. aircraft according to claim 1 rescue fastens rigging, and it is characterized in that: described tight tying is two, comprise flat band, be connected in flat band upper end suspension hook, be connected in the shackle and the fastener of flat band lower end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009201779629U CN201484659U (en) | 2009-09-25 | 2009-09-25 | Fastening rope for airplane rescue |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009201779629U CN201484659U (en) | 2009-09-25 | 2009-09-25 | Fastening rope for airplane rescue |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201484659U true CN201484659U (en) | 2010-05-26 |
Family
ID=42423551
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009201779629U Expired - Lifetime CN201484659U (en) | 2009-09-25 | 2009-09-25 | Fastening rope for airplane rescue |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201484659U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112071159A (en) * | 2020-09-21 | 2020-12-11 | 航大联合航空设备有限公司 | Aviation simulator for ground real-practice drilling and simulation use method thereof |
-
2009
- 2009-09-25 CN CN2009201779629U patent/CN201484659U/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112071159A (en) * | 2020-09-21 | 2020-12-11 | 航大联合航空设备有限公司 | Aviation simulator for ground real-practice drilling and simulation use method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20100526 |
|
| CX01 | Expiry of patent term |