CN104890894A - Length and stiffness-adjustable aircraft mooring system - Google Patents
Length and stiffness-adjustable aircraft mooring system Download PDFInfo
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- CN104890894A CN104890894A CN201510197111.0A CN201510197111A CN104890894A CN 104890894 A CN104890894 A CN 104890894A CN 201510197111 A CN201510197111 A CN 201510197111A CN 104890894 A CN104890894 A CN 104890894A
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- rope
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Abstract
The invention provides a length and stiffness-adjustable aircraft mooring system, comprising a hook, a spring, a hoop, a connecting rod, a rope and a bolt, wherein one end of the hook is connected to an aircraft mooring point, and the other end of the hook is connected to the spring; the other end of the spring is connected to the connecting rod; the hoop sleeves on the connecting rod; the other end of the connecting rod is connected to the rope; the other end of the rope is connected to the bolt; adjustment holes for adjusting the length of the rope are formed in the connecting rod. By applying the length and stiffness-adjustable aircraft mooring system, the length of the mooring rope can be simply and rapidly adjusted and the buffer performance of the mooring rope is improved.
Description
Technical field
The present invention relates to a kind of for the anchor fitting of aircraft when Ground Mooring.
Background technology
When aircraft rests on ground, owing to there is wind-force effect, need by special mooring gear, aircraft to be fixed on the ground.Because each stop position of aircraft is different, the mooring gear adopted at present generally regulates the length of mooring rope by screw rod.Distance variation range between mooring point and ground attachment point is comparatively large, and therefore mooring rope lengths needs to regulate in a big way, but regulates length by screw rod, and speed is slow and work capacity is large, adds the time that tying airplane needs.Screw rod is comparatively firm simultaneously, and cushion characteristic is poor, and when aircraft wind-engaging is carried, tie-down loads is comparatively large, adds aero-structure weight and design difficulty.
Summary of the invention
Regulating to solve existing mooring Abseiling device the problem that rope lengths speed is slow, work capacity large and mooring rope cushion characteristic is poor, the invention provides a kind of simple, quick adjustment mooring rope lengths and increasing the aircraft picketing device of mooring rope cushion characteristic.
The present invention is realized by following technical proposals: this aircraft picketing device comprises hook, spring, clip, connecting rod, rope, latch, wherein link up with one end to be connected with aircraft picketing point, the other end is connected with spring, the spring other end is connected with connecting rod, hoop sleeve is on connecting rod, the connecting rod other end is connected with rope, and the rope other end is connected with latch, and described connecting rod is provided with the adjustment hole regulating rope lengths.
Described spring can be dismantled, and can select the spring of corresponding rigidity according to load condition suffered by aircraft, regulates the rigidity of mooring rope.
Described latch cross section is slightly less than adjustment hole, in zigzag, has certain taper, and front elevational sectional is less than rear end section.
Described latch can insert in the adjustment hole of connecting rod, being retrained fixing, changing the length of mooring rope by inserting different adjustment hole by clip.
Beneficial effect of the present invention: structure of the present invention is simple, and reliability is high, and cost is lower, and easy and simple to handle when regulating rope lengths, laborsavingly saves time.Rope rigidity regulates by changing spring, can improve rope cushion characteristic, extend the service life of rope, and can reduce tie-down loads.Therefore practicality is better, is easy to apply, has larger value of service.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention;
Fig. 2 is the schematic diagram of clip of the present invention;
Fig. 3 is the schematic diagram of connecting rod of the present invention;
Fig. 4 is the schematic diagram of latch of the present invention;
Fig. 5 is the block diagram of Fixed latches in the present invention;
Fig. 6 is the front elevation of Fixed latches in the present invention;
Fig. 7 is the lateral plan of Fixed latches in the present invention;
Fig. 8 is the birds-eye view of Fixed latches in the present invention;
In the drawings: 1-hook; 2-spring; 3-clip; 4-connecting rod; 5-rope; 6-latch; 7-aircraft picketing point; 8-ground attachment point.
Detailed description of the invention
As shown in Figure 1, this aircraft picketing device comprises hook (1), spring (2), clip (3), connecting rod (4), rope (5), latch (6).Wherein link up with (1) one end to be connected with aircraft picketing point, the other end is connected with spring (2), spring (2) other end is connected with connecting rod (4), clip (3) is enclosed within connecting rod (4), connecting rod (4) other end is connected with rope (5), rope (5) other end is connected with latch (6), and as shown in Figure 3, described connecting rod (4) is provided with the adjustment hole regulating rope lengths.
Described spring (2) can be dismantled, and can select the spring of corresponding rigidity according to load condition suffered by aircraft, regulates the rigidity of mooring rope.
As shown in Figure 4, described latch (6) cross section is slightly less than adjustment hole, in zigzag, has certain taper, and front elevational sectional is less than rear end section.
As Fig. 5,6, shown in 7 and 8, described latch (6) can insert in the adjustment hole of connecting rod (4), being retrained by clip (3) fixing, changing the length of mooring rope by inserting different adjustment hole.
The present invention is the mooring Abseiling device for connecting aircraft picketing point and ground attachment point, can be fixed on the ground when the effect of aircraft by wind by this device.Wherein link up with (1) to be connected with aircraft picketing point (7), the other end is connected with spring (2), spring (2) can be dismantled, the spring of different-stiffness can be selected according to tie-down loads situation suffered by aircraft, thus change the rigidity of mooring Abseiling device, improve the cushion characteristic of mooring rope, make aircraft be subject to obtain certain buffering during larger prominent wind load, reduce tie-down loads.The reduction of tie-down loads can alleviate the structural weight of aircraft picketing point and then improve the performance of aircraft, has the service life that good cushion characteristic can extend rope equally.Spring (2) other end is connected with connecting rod (4), connecting rod (4) has the adjustment hole regulating mooring rope lengths, because connecting rod (4) length can be longer, therefore regulate the scope of rope lengths larger relative to screw mechanism linkage.Connecting rod (4) other end is connected with rope (5), and rope (5) is through ground attachment point (8), and the other end is connected with latch (6).Latch (6) is fixed by clip (3) through connecting rod (4) adjustment hole, no matter setting range length only needs a step simple operations just can complete the adjustment of rope lengths and fix, simple and reliable for structure relative to screw mechanism, cost is lower, easy and simple to handle, laborsavingly to save time.
Claims (4)
1. the aircraft picketing device of an adjustable length and rigidity, comprise hook, spring, clip, connecting rod, rope, latch, it is characterized in that, wherein link up with one end to be connected with aircraft picketing point, the other end is connected with spring, and the spring other end is connected with connecting rod, hoop sleeve is on connecting rod, the connecting rod other end is connected with rope, and the rope other end is connected with latch, and described connecting rod is provided with the adjustment hole regulating rope lengths.
2. aircraft picketing device according to claim 1, is characterized in that, described spring can be dismantled.
3. aircraft picketing device according to claim 1, is characterized in that, described latch cross section is slightly less than adjustment hole, in zigzag, has certain taper, and front elevational sectional is less than rear end section.
4. the aircraft picketing device according to claim 1,2 or 3, is characterized in that, described latch can insert in the adjustment hole of connecting rod, being retrained fixing, changing the length of mooring rope by inserting different adjustment hole by clip.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510197111.0A CN104890894A (en) | 2015-04-24 | 2015-04-24 | Length and stiffness-adjustable aircraft mooring system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510197111.0A CN104890894A (en) | 2015-04-24 | 2015-04-24 | Length and stiffness-adjustable aircraft mooring system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104890894A true CN104890894A (en) | 2015-09-09 |
Family
ID=54023963
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510197111.0A Pending CN104890894A (en) | 2015-04-24 | 2015-04-24 | Length and stiffness-adjustable aircraft mooring system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104890894A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106516151A (en) * | 2016-12-07 | 2017-03-22 | 青海利高智能设备有限公司 | Unmanned aerial vehicle mooring base |
| CN106672236A (en) * | 2016-08-26 | 2017-05-17 | 航宇救生装备有限公司 | Rapid tethering and separating device |
| CN112861450A (en) * | 2021-02-18 | 2021-05-28 | 江西洪都航空工业集团有限责任公司 | Airplane mooring scheme evaluation method based on multi-body model |
| CN113859571A (en) * | 2021-11-30 | 2021-12-31 | 中国飞机强度研究所 | Airplane mooring device and mooring method |
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| KR20080013841A (en) * | 2007-12-28 | 2008-02-13 | 주식회사 빌드썬 | Wire fixing apparatus |
| CN102390541A (en) * | 2011-09-08 | 2012-03-28 | 上海航空机械有限公司 | Anti-typhoon fixing device for helicopter |
| CN203143013U (en) * | 2013-03-29 | 2013-08-21 | 成都飞机设计研究所 | Aircraft plateau mooring device |
| CN203173683U (en) * | 2013-01-30 | 2013-09-04 | 巨力索具股份有限公司 | Length-adjustable fiber rope sling |
| CN203545451U (en) * | 2013-11-15 | 2014-04-16 | 中航飞机股份有限公司西安飞机分公司 | Suspender adjusting device |
| CN103935882A (en) * | 2014-04-25 | 2014-07-23 | 中石化宁波工程有限公司 | Holding-lifting method for large thin-wall dryer |
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2015
- 2015-04-24 CN CN201510197111.0A patent/CN104890894A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20080013841A (en) * | 2007-12-28 | 2008-02-13 | 주식회사 빌드썬 | Wire fixing apparatus |
| CN102390541A (en) * | 2011-09-08 | 2012-03-28 | 上海航空机械有限公司 | Anti-typhoon fixing device for helicopter |
| CN203173683U (en) * | 2013-01-30 | 2013-09-04 | 巨力索具股份有限公司 | Length-adjustable fiber rope sling |
| CN203143013U (en) * | 2013-03-29 | 2013-08-21 | 成都飞机设计研究所 | Aircraft plateau mooring device |
| CN203545451U (en) * | 2013-11-15 | 2014-04-16 | 中航飞机股份有限公司西安飞机分公司 | Suspender adjusting device |
| CN103935882A (en) * | 2014-04-25 | 2014-07-23 | 中石化宁波工程有限公司 | Holding-lifting method for large thin-wall dryer |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106672236A (en) * | 2016-08-26 | 2017-05-17 | 航宇救生装备有限公司 | Rapid tethering and separating device |
| CN106672236B (en) * | 2016-08-26 | 2023-05-02 | 航宇救生装备有限公司 | Device for quick mooring and releasing |
| CN106516151A (en) * | 2016-12-07 | 2017-03-22 | 青海利高智能设备有限公司 | Unmanned aerial vehicle mooring base |
| CN112861450A (en) * | 2021-02-18 | 2021-05-28 | 江西洪都航空工业集团有限责任公司 | Airplane mooring scheme evaluation method based on multi-body model |
| CN113859571A (en) * | 2021-11-30 | 2021-12-31 | 中国飞机强度研究所 | Airplane mooring device and mooring method |
| CN113859571B (en) * | 2021-11-30 | 2022-03-01 | 中国飞机强度研究所 | Airplane mooring device and mooring method |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20150909 |
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| RJ01 | Rejection of invention patent application after publication |