CN206243505U - A kind of special mooring device of helistop - Google Patents
A kind of special mooring device of helistop Download PDFInfo
- Publication number
- CN206243505U CN206243505U CN201621256430.0U CN201621256430U CN206243505U CN 206243505 U CN206243505 U CN 206243505U CN 201621256430 U CN201621256430 U CN 201621256430U CN 206243505 U CN206243505 U CN 206243505U
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- CN
- China
- Prior art keywords
- deck
- package assembly
- helistop
- constraint
- mooring device
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Abstract
A kind of special mooring device of helistop; deck including airplane parking area; several binders are plugged on deck; binder is located on several reference circles with center deck as the center of circle and is uniformly distributed in a ring around the center on deck; described binder includes the package assembly of cylinder; the screwed hole through package assembly top surface is formed in package assembly; flange is formed on the outer wall on package assembly top; flange is pressed against on the upper surface on deck; vertical stud is formed on the bottom surface of package assembly, the bottom surface of stud overhanging deck is bolted with clamp nut；Crimp is bolted with the screwed hole of the package assembly, the upper end of crimp forms flat-shaped arc constraint head, constraint hole is formed on constraint head, and protection cap is bolted with the top of package assembly.The restraint device that it is used can carry out activity adjustment, can change the length of constraint, be used so as to be applicable to the constraint of helicopter of different type of machines.
Description
Technical field：
The utility model is related to the technical field of airplane parking area, more specifically to a kind of helistop it is special be
Stay device.
Background technology：
Airplane parking area, refers generally to the place of helicopter landing.Influence of the environment to airplane parking area is very big, such as strong wind, not only
In view of airplane parking area support strength in itself, while needing to consider influence of the environment to the helicopter on airplane parking area.So as to existing
Restraint device typically is installed on some airplane parking areas, the shadow for using restraint device and cable wire etc. to fix helicopter to resist environment
Ring.But the restraint device on existing airplane parking area is typically using fixed, the constraint dress that such as patent No. 201420458941.5 is proposed
Put, because of what is fixed, the constraint that can only be typically suitable for the helicopter of equal size is used its restraint device.
Utility model content：
, aiming at the deficiency of prior art, and it is special to provide a kind of helistop for the purpose of this utility model
Mooring device, it uses movable restraint device, is applicable to the helicopter of different type of machines.
A kind of special mooring device of helistop, including airplane parking area deck, plugged on deck several constraint
Device, binder is located on several reference circles with center deck as the center of circle and is uniformly distributed in a ring around the center on deck, institute
The binder stated includes the package assembly of cylinder, and the screwed hole through package assembly top surface, package assembly top are formed in package assembly
Outer wall on form flange, flange is pressed against on the upper surface on deck, and vertical stud, spiral shell are formed on the bottom surface of package assembly
The bottom surface of post overhanging deck is bolted with clamp nut；Crimp, the upper end of crimp are bolted with the screwed hole of the package assembly
Flat-shaped arc constraint head is formed, constraint hole is formed on constraint head, protection cap is bolted with the top of package assembly.
Described protection cap is T-shaped, and the lower surface of protection cap forms shrinkage pool, is formed on the upper surface of protection cap some
Road anti-slip tank.
Stud upper sleeve between the deck and clamp nut has buckle and packing ring, and buckle is pressed against the bottom surface on deck
On.
Depth of the length of crimp less than package assembly upper screwed hole in the binder.
Mark circle is provided with described deck, binder is distributed in the inner side of mark circle.
Level ground side cover plate is fixed with the outside on the deck, illuminator is fixed with the cover plate of level ground side.
The beneficial effects of the utility model are：
1st, the restraint device that it is used can carry out activity adjustment, can change the length of constraint, so as to be applicable to difference
The constraint of the helicopter of type is used.
2nd, the crimp in the restraint device that it is used can be stretched, more convenient for the constraint of helicopter is fixed；Simultaneously
When not using, it is placed in restraint device, does not interfere with parking for helicopter.
Brief description of the drawings：
Fig. 1 is the structural representation of the utility model binder distribution；
Fig. 2 is the structural representation that the utility model binder and deck connect；
Fig. 3 is the schematic cross-sectional view that the utility model binder is amplified；
Fig. 4 is the structural representation that crimp stretches out package assembly in the utility model binder.
In figure：1st, deck；2nd, level ground side cover plate；3rd, illuminator；4th, mark circle；5th, binder；51st, package assembly；511st, method
It is blue；512nd, stud；52nd, crimp；521st, head is fettered；522nd, hole is fettered；53rd, protection cap；531st, shrinkage pool；532nd, anti-slip tank；6、
Buckle；7th, packing ring；8th, clamp nut.
Specific embodiment：
Embodiment：As shown in Fig. 1 to 4, a kind of special mooring device of helistop, including airplane parking area deck 1,
Several binders 5 are plugged on deck 1, binder 5 is located on several reference circles with the center of deck 1 as the center of circle and around deck
1 center is uniformly distributed in a ring, and described binder 5 includes the package assembly 51 of cylinder, is formed in package assembly 51 and run through
The screwed hole of the top surface of package assembly 51, forms flange 511 on the outer wall on the top of package assembly 51, flange 511 is pressed against the upper of deck 1
On surface, vertical stud 512 is formed on the bottom surface of package assembly 51, the bottom surface of the overhanging deck 1 of stud 512 is bolted with fastening spiral shell
Female 8；Crimp 52 is bolted with the screwed hole of the package assembly 51, the upper end of crimp 52 forms flat-shaped arc constraint head
521, constraint hole 522 is formed in constraint first 521, the top of package assembly 51 is bolted with protection cap 53.
Described protection cap 53 is T-shaped, and the lower surface of protection cap 53 forms shrinkage pool 531, on the upper surface of protection cap 53
If forming arterial highway anti-slip tank 532.
The upper sleeve of stud 512 between the deck 1 and clamp nut 8 has buckle 6 and packing ring 7, and buckle 6 is pressed against deck
On 1 bottom surface.
Depth of the length of crimp 52 less than the upper screwed hole of package assembly 51 in the binder 5.
Mark circle 4 is provided with described deck 1, binder 5 is distributed in the inner side of mark circle 4.
Level ground side cover plate 2 is fixed with the outside on the deck 1, illuminator 3 is fixed with level ground side cover plate 2.
Operation principle：The utility model is the mooring device on airplane parking area, and mooring device is equal to shutdown Pingshan
Binder 5, i.e. restraint device, its technical characterstic is for movable constraint by original fixed restraint device rectification
Device, its restraint device is mainly binder 5, and binder 5 is made up of package assembly 51 and crimp 52, and package assembly 51 is fixed, beam
Tie up part 52 to be connected with package assembly 51 by screw thread, so that crimp 52 can be installed in package assembly 51, it is also possible to stretch out package assembly
51 such that it is able to change the length of constraint, it is adaptable to which the constraint of the helicopter of different type of machines is used.
Claims (6)
1. a kind of deck (1) of the special mooring device of helistop, including airplane parking area, it is characterised in that：On deck (1)
Several binders (5) are plugged, binder (5) is on several reference circles with deck (1) center as the center of circle and around deck
(1) center is uniformly distributed in a ring, described binder (5) include in the package assembly (51) of cylinder, package assembly (51) into
Type has the screwed hole through package assembly (51) top surface, and flange (511), flange are formed on the outer wall on package assembly (51) top
(511) it is pressed against on the upper surface of deck (1), vertical stud (512), stud is formed on the bottom surface of package assembly (51)
(512) bottom surface of overhanging deck (1) is bolted with clamp nut (8)；Crimp is bolted with the screwed hole of the package assembly (51)
(52), the upper end of crimp (52) forms flat-shaped arc and fetters head (521), and constraint hole is formed in constraint head (521)
(522), it is bolted with protection cap (53) at the top of package assembly (51).
2. the special mooring device of a kind of helistop according to claim 1, it is characterised in that：Described protection
Lid (53) is T-shaped, and the lower surface of protection cap (53) forms shrinkage pool (531), is formed on the upper surface of protection cap (53) some
Road anti-slip tank (532).
3. the special mooring device of a kind of helistop according to claim 1, it is characterised in that：The deck
(1) stud (512) upper sleeve and between clamp nut (8) has buckle (6) and packing ring (7), and buckle (6) is pressed against deck (1)
Bottom surface on.
4. the special mooring device of a kind of helistop according to claim 1, it is characterised in that：The binder
(5) depth of the length of crimp (52) less than package assembly (51) upper screwed hole on.
5. the special mooring device of a kind of helistop according to claim 1, it is characterised in that：Described deck
(1) mark circle (4) is provided with, binder (5) is distributed in the inner side of mark circle (4).
6. the special mooring device of a kind of helistop according to claim 1, it is characterised in that：The deck
(1) level ground side cover plate (2) is fixed with outside, illuminator (3) is fixed with level ground side cover plate (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621256430.0U CN206243505U (en) | 2016-11-23 | 2016-11-23 | A kind of special mooring device of helistop |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621256430.0U CN206243505U (en) | 2016-11-23 | 2016-11-23 | A kind of special mooring device of helistop |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206243505U true CN206243505U (en) | 2017-06-13 |
Family
ID=59001563
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621256430.0U Active CN206243505U (en) | 2016-11-23 | 2016-11-23 | A kind of special mooring device of helistop |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206243505U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113445439A (en) * | 2021-05-21 | 2021-09-28 | 中国海洋石油集团有限公司 | Intelligent marine helicopter deck |
-
2016
- 2016-11-23 CN CN201621256430.0U patent/CN206243505U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113445439A (en) * | 2021-05-21 | 2021-09-28 | 中国海洋石油集团有限公司 | Intelligent marine helicopter deck |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20180409 Address after: 311800 Zhu Village, five Xie village, five Xie Town, Zhuji City, Shaoxing, Zhejiang Patentee after: Zhejiang Xiang Xiang Aviation Technology Co., Ltd. Address before: 311800 Zhejiang city of Shaoxing province Zhuji city streets Wen Feng Tao Zhu Road No. 15 Patentee before: Wang Qiuli |