CN207374702U - A kind of helicopter high wind mooring mast - Google Patents
A kind of helicopter high wind mooring mast Download PDFInfo
- Publication number
- CN207374702U CN207374702U CN201721473244.7U CN201721473244U CN207374702U CN 207374702 U CN207374702 U CN 207374702U CN 201721473244 U CN201721473244 U CN 201721473244U CN 207374702 U CN207374702 U CN 207374702U
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- lower beam
- upper boom
- perforate
- block
- high wind
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Abstract
The utility model discloses a kind of helicopter high wind mooring masts, including upper boom and lower beam, the lower end of the lower beam is equipped with lower beam perforate, it is equipped in the lower beam perforate and is tethered at hook, the upper end of the lower beam is equipped with lower beam plush copper, the lower beam plush copper is " V "-shaped, the top of the lower beam plush copper is welded with columned No.1 block, the surface of the No.1 block is equipped with No. two identical blocks of shape size therewith, No. two blocks and No.1 block are in be symmetrical arranged and be each provided in sleeve up and down, the upper end of No. two blocks is welded with upper boom plush copper, the upper boom plush copper top is equipped with upper boom, the upper boom top is equipped with upper boom perforate, stud is equipped in the upper boom perforate.For the utility model by applying mooring mast upper boom, mooring mast lower beam and hook connect the simple component such as part device, this device feature it is of low cost, it is simple for process, it is convenient for production, reduce production cost.
Description
Technical field
The utility model is related to helicopters to safeguard equipment technology field more particularly to a kind of helicopter high wind mooring mast.
Background technology
Aircraft on coastal, plateau when the land for having high wind weather is parked, in order to avoid aircraft is turned over, propeller rotation
Loss, need to use mooring device caused by turning.Aircraft particularly in highlands, which is parked, has been tethered at the characteristics of it is unique:Wind-force
Greatly, up to 11 grades of strong wind, mooring device must have enough intensity that could resist wind load, and satisfaction is tethered at requirement；Highlands is empty
Gas is thin, influences the action edge of operating personnel, it is therefore desirable to which light device could meet requirement.
Through retrieval, Chinese patent grant number CN1040977877A discloses one kind and is tethered at grid, airborne mooring mast and fast
Fast mooring device including airborne mooring mast and is tethered at grid.Airborne mooring mast includes attachment device, elastic rod and sphere；Wherein,
Attachment device is used to airborne mooring mast being mounted on the installation pedestal of unmanned plane.Being tethered at grid includes upper grid plate, lower part
Flase floor, stent and drive component；Wherein, upper grid plate is fixed on stent, and lower grid plate is arranged on upper grid plate
Lower section；Upper grid plate is provided with multiple entrance holes；Lower grid plate is provided with multiple card holes, when in the first working condition
When, the driving component drives the lower grid plate operation, and entrance hole and card hole formation meet airborne mooring mast disengaging requirement
Passage；When in the second working condition, the driving component drives the lower grid plate operation, and entrance hole and card hole will
Airborne mooring mast, which blocks, makes it that can not extract.
Above-mentioned quick mooring device has the following disadvantages：Mooring device it is complicated, production hour is longer, cost compared with
Height is that the production efficiency of enterprise is relatively low, and the construction to building airplane parking area proposes harsh requirement so that the practicality is not
By force, it is impossible to which universalness uses.
Utility model content
The purpose of this utility model is to provide a kind of helicopter high wind mooring mast, possess it is simple in structure, it is of low cost,
The advantages of airplane parking area requirement of make-up even is low solves the airplane parking area requirement that mooring device is complicated, and cost is higher, and make-up connects
The problem of harsh.
According to a kind of helicopter high wind mooring mast of the utility model embodiment, including upper boom and lower beam, the lower beam
Lower end be equipped with lower beam perforate, be equipped in the lower beam perforate and be tethered at hook, the upper end of the lower beam is equipped with lower beam plush copper, under described
Bar plush copper is " V "-shaped, and the top of the lower beam plush copper is welded with columned No.1 block, the surface of the No.1 block
Equipped with No. two identical blocks of shape size therewith, No. two blocks and No.1 block are in be symmetrical arranged and be each provided at set up and down
In cylinder, the upper end of No. two blocks is welded with upper boom plush copper, and the upper boom plush copper top is equipped with upper boom, and the upper boom top is set
Have a upper boom perforate, stud be equipped in the upper boom perforate, be equipped with captive band between the stud and upper boom perforate, the captive band with
It is sewed up together by nylon wire one end of drawing cloth.
Further, the downside for being tethered at hook is equipped with the fixing device for being fixed on airplane parking area edge, the fixing device
Including retainer ring.
Further, the retainer ring lower end is equipped with surface fixed block upper end, and the surface fixed block is arranged on ground end.
Further, the sleeve is made of two pieces of arc concave blocks, is equipped with screw hole on the side wall of each concave block, and two
Arc concave block is mutually fixed by screw described in block.
Further, it is described to be tethered on hook upper outside wall with being equipped with external screw thread, the external screw thread on the outer wall of stud
It is equipped with and the matched internal thread of external screw thread with lower beam perforate and upper boom perforate inner wall.
Further, the depth of the lower beam perforate is 15-20cm.
The utility model has an advantageous effect in that compared with prior art：
1st, by applying mooring mast upper boom, mooring mast lower beam and hook connect the simple component such as part device, can be so as to go straight up to
Machine is fixed under the natural environment of high wind on airplane parking area, this device feature it is of low cost, it is simple for process, it is convenient for production,
Reduce production cost；
2nd, set by simple mechanism, when installing and using, can be easy to be debugged, when making mooring of helicopter more
Add efficient and convenient, by setting simple apron surface fixed block, reduce requirement of this mooring device to airplane parking area, stop
The expenditure of construction on machine level ground reduces, and adds benefit.
Description of the drawings
Attached drawing is used to provide a further understanding of the present invention, and a part for constitution instruction, with this practicality
New embodiment for explaining the utility model, does not form the limitation to the utility model together.In the accompanying drawings：
Fig. 1 be the utility model proposes a kind of helicopter high wind mooring mast structure diagram.
Fig. 2 be the utility model proposes a kind of upper boom of helicopter high wind mooring mast and the sectional view of lower beam.
Fig. 3 is that A goes out structural profile illustration in Fig. 1.
Fig. 4 be the utility model proposes a kind of helicopter high wind mooring mast sleeve cross-sectional view
Fig. 5 be the utility model proposes the hook of helicopter high wind mooring mast a kind of connect portion's structure diagram.
In figure：1- be tethered at hook, the perforate of 2- lower beams, 3- lower beams, 4- lower beams plush copper, 5- No.1s block, No. bis- blocks of 6-, on 7-
Bar plush copper, 8- sleeves, 9- upper booms, the perforate of 10- upper booms, 11- studs, 12- captive bands, 13- drawings cloth, 14- apron surfaces are consolidated
Determine block, 15- hooks connect portion, 16- retainer rings.
Specific embodiment
The following is a combination of the drawings in the embodiments of the present utility model, and the technical scheme in the embodiment of the utility model is carried out
It clearly and completely describes, it is clear that the described embodiments are only a part of the embodiments of the utility model rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are without making creative work
All other embodiments obtained shall fall within the protection scope of the present invention.
With reference to Fig. 1-5, a kind of helicopter high wind mooring mast, including upper boom 9 and lower beam 3, the lower end of lower beam 3 is equipped with lower beam
Perforate 2, interior be equipped with of lower beam perforate 2 are tethered at hook 1, and the upper end of lower beam 3 is equipped with lower beam plush copper 4, and lower beam plush copper 4 is " V "-shaped, lower beam
The top of plush copper 4 is welded with columned No.1 block 5, and the surface of No.1 block 5 is equipped with identical two of shape size therewith
Number block 6, No. two blocks 6 and No.1 block 5 in being symmetrical arranged and be each provided in sleeve 8 up and down, the upper end welding of No. two blocks 6
There is upper boom plush copper 7,7 top of upper boom plush copper is equipped with upper boom 9, and 9 top of upper boom is equipped with upper boom perforate 10, spiral shell is equipped in upper boom perforate 10
Column 11, is equipped with captive band 12 between stud 11 and upper boom perforate 10, captive band 12 is sewed up with pulling one end of cloth 13 by nylon wire
Together, by applying mooring mast upper boom 9, mooring mast lower beam 3 and hook connect the simple components such as 15 device of portion, can be so as to go straight up to
Machine is fixed under the natural environment of high wind on airplane parking area, this device feature it is of low cost, it is simple for process, it is convenient for production,
Reduce production cost.
The downside for being tethered at hook 1 is equipped with the fixing device for being fixed on airplane parking area edge, and fixing device includes retainer ring 16, fixed
16 lower end of ring is equipped with 14 upper end of surface fixed block, and surface fixed block 14 is arranged on ground end, and sleeve 8 is made of two pieces of arc concave blocks,
Screw hole is equipped on the side wall of each concave block, two pieces of arc concave blocks are mutually fixed by screw, are tethered on 1 upper outside wall of hook and spiral shell
External screw thread is equipped on the outer wall of column 11, external screw thread is equipped with lower beam perforate 2 and 10 inner wall of upper boom perforate to match with external screw thread
The internal thread of conjunction, the depth of lower beam perforate 2 is 15-20cm, is set by simple mechanism, when installing and using, can held very much
Easily debugged, it is more efficient and convenient when making mooring of helicopter, by setting simple apron surface fixed block 14, make this
Requirement of the mooring device to airplane parking area reduces, and the expenditure of construction of airplane parking area reduces, and adds benefit.
In use, drawing cloth 13 is sleeved on helicopter upper surface, 13 both ends of cloth then will be pulled in helicopter both sides respectively
Captive band 12 be fixed on by stud 11 in the upper boom perforate 10 on 9 top of upper boom, hook then is connected 15 part of portion again fixes, will
The hook 1 that is tethered at that hook connects portion 15 is hooked in the retainer ring 18 that apron surface fixed block 14 is equipped with, and is then opened the lower beam of lower beam 3
Hole 2 is directed at the top for being tethered at hook 1, while rotates lower beam 3 so that is tethered in 1 upper end precession lower beam perforate 2 of hook, by lower beam 3 into one
The rotation of step tenses the mooring mast of helicopter both sides, when helicopter both sides are after being tethered at hook 1 and tense, stops turn lower beam 3.
Part is not described in detail for the utility model, is the known technology of those skilled in the art.
While there has been shown and described that the embodiment of the utility model, for the ordinary skill in the art,
It is appreciated that in the case where not departing from the principle of the utility model and spirit can these embodiments be carried out with a variety of variations, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of helicopter high wind mooring mast, it is characterised in that：Including upper boom (9) and lower beam (3), under the lower beam (3)
End is equipped with lower beam perforate (2), is equipped in the lower beam perforate (2) and is tethered at hook (1), and the upper end of the lower beam (3) is convex equipped with lower beam
Head (4), the lower beam plush copper (4) is " V "-shaped, and the top of the lower beam plush copper (4) is welded with columned No.1 block
(5), the surface of the No.1 block (5) is equipped with No. two identical blocks (6) of shape size therewith, No. two blocks (6)
With No.1 block (5) in being symmetrical arranged and being each provided in sleeve (8) up and down, the upper end of No. two blocks (6) is welded with upper boom
Plush copper (7), upper boom plush copper (7) top be equipped with upper boom (9), upper boom (9) top be equipped with upper boom perforate (10), it is described on
Stud (11) is equipped in bar perforate (10), captive band (12) is equipped between the stud (11) and upper boom perforate (10), it is described to be tethered at
Together with band (12) is sewed up with one end of drawing cloth (13) by nylon wire.
2. a kind of helicopter high wind mooring mast according to claim 1, it is characterised in that：It is described to be tethered under hook (1)
Side is equipped with the fixing device for being fixed on airplane parking area edge, and the fixing device includes retainer ring (16).
3. a kind of helicopter high wind mooring mast according to claim 2, it is characterised in that：Retainer ring (16) lower end
Equipped with surface fixed block (14) upper end, the surface fixed block (14) is arranged on ground end.
4. a kind of helicopter high wind mooring mast according to claim 1, it is characterised in that：The sleeve (8) is by two pieces
Arc concave block forms, and is equipped with screw hole on the side wall of each concave block, two pieces of arc concave blocks are mutually fixed by screw.
5. a kind of helicopter high wind mooring mast according to claim 1, it is characterised in that：It is described to be tethered at hook (1) top
With being equipped with external screw thread, the external screw thread and lower beam perforate (2) and upper boom perforate (10) on the outer wall of stud (11) on lateral wall
Inner wall is equipped with and the matched internal thread of external screw thread.
6. a kind of helicopter high wind mooring mast according to claim 1, it is characterised in that：The lower beam perforate (2)
Depth is 15-20cm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721473244.7U CN207374702U (en) | 2017-11-07 | 2017-11-07 | A kind of helicopter high wind mooring mast |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721473244.7U CN207374702U (en) | 2017-11-07 | 2017-11-07 | A kind of helicopter high wind mooring mast |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207374702U true CN207374702U (en) | 2018-05-18 |
Family
ID=62335290
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721473244.7U Active CN207374702U (en) | 2017-11-07 | 2017-11-07 | A kind of helicopter high wind mooring mast |
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| CN (1) | CN207374702U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110884675A (en) * | 2019-12-04 | 2020-03-17 | 中国直升机设计研究所 | Helicopter blade mooring device |
| CN110979720A (en) * | 2019-11-29 | 2020-04-10 | 重庆交通大学 | A collapsible formula high wind damping mooring rod for fixing helicopter rotor |
| CN111452967A (en) * | 2019-08-15 | 2020-07-28 | 北京理工大学 | Bearing position adjustable bearing frame and mooring cable connection position are along with traction mechanism of mooring unmanned aerial vehicle gesture self-adaptation |
-
2017
- 2017-11-07 CN CN201721473244.7U patent/CN207374702U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111452967A (en) * | 2019-08-15 | 2020-07-28 | 北京理工大学 | Bearing position adjustable bearing frame and mooring cable connection position are along with traction mechanism of mooring unmanned aerial vehicle gesture self-adaptation |
| CN111452967B (en) * | 2019-08-15 | 2021-06-25 | 北京理工大学 | Mooring cable connecting position is along with traction mechanism of mooring unmanned aerial vehicle gesture self-adaptation |
| CN110979720A (en) * | 2019-11-29 | 2020-04-10 | 重庆交通大学 | A collapsible formula high wind damping mooring rod for fixing helicopter rotor |
| CN110884675A (en) * | 2019-12-04 | 2020-03-17 | 中国直升机设计研究所 | Helicopter blade mooring device |
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