CN112478123B - Nose tower end structure of mooring balloon mooring facility - Google Patents
Nose tower end structure of mooring balloon mooring facility Download PDFInfo
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- CN112478123B CN112478123B CN202011357514.4A CN202011357514A CN112478123B CN 112478123 B CN112478123 B CN 112478123B CN 202011357514 A CN202011357514 A CN 202011357514A CN 112478123 B CN112478123 B CN 112478123B
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- 238000004873 anchoring Methods 0.000 claims abstract description 30
- 230000007246 mechanism Effects 0.000 claims abstract description 21
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- 239000010959 steel Substances 0.000 claims description 5
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- 230000007306 turnover Effects 0.000 claims 2
- 239000000956 alloy Substances 0.000 claims 1
- 229910045601 alloy Inorganic materials 0.000 claims 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims 1
- 229910052782 aluminium Inorganic materials 0.000 claims 1
- 230000009471 action Effects 0.000 description 6
- 238000000034 method Methods 0.000 description 5
- 239000000463 material Substances 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/40—Balloons
- B64B1/50—Captive balloons
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/66—Mooring attachments
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Abstract
本发明提供一种系留气球锚泊设施鼻塔端部结构,包括支架以及设置于支架上的卡圈、第一横轴、第二横轴、第一纵轴、第二纵轴和翻转机构;第一横轴具有第一状态和第二状态,在第一状态下,第一横轴与第二横轴、第一纵轴和第二纵轴之间围成鼻系索通道;在第二状态下,第一横轴在鼻系索通道位于第一横轴一侧形成开口;卡圈上设置有径向缺口,径向缺口延伸至鼻系索通道的延伸路径上;翻转机构用于驱动第一横轴在第一状态和第二状态之间切换。本发明提供的系留气球锚泊设施鼻塔端部结构能够使鼻系索松动时不会卡在结构缝隙中,并且使鼻系索收放阻力更小,不会与其他结构产生摩擦,在地面即可完成鼻系索移入或移出鼻系索通道的操作。
The invention provides a nose tower end structure of a mooring balloon anchoring facility, comprising a bracket and a collar arranged on the bracket, a first transverse axis, a second transverse axis, a first longitudinal axis, a second longitudinal axis and a turning mechanism; The first horizontal axis has a first state and a second state, in the first state, a nasal lanyard channel is enclosed between the first horizontal axis and the second horizontal axis, the first longitudinal axis and the second longitudinal axis; in the second state In the state, the first transverse shaft forms an opening on the side of the nasal lanyard channel on the side of the first transverse shaft; the collar is provided with a radial gap, and the radial gap extends to the extension path of the nasal lanyard channel; the turning mechanism is used to drive the The first horizontal axis switches between the first state and the second state. The nose tower end structure of the mooring balloon anchoring facility provided by the present invention can prevent the nasal lanyard from being stuck in the structure gap when it is loose, and make the nasal lanyard retraction resistance smaller, and it will not cause friction with other structures, and it will not cause friction on the ground. The operation of moving the nasal lanyard in and out of the nasal lanyard channel is completed.
Description
技术领域technical field
本发明涉及浮空器技术领域,尤其涉及一种系留气球锚泊设施鼻塔端部结构。The invention relates to the technical field of aerostats, in particular to a nose tower end structure of a mooring balloon anchoring facility.
背景技术Background technique
系留气球是一种轻于空气的无动力浮空器,具有一个充满轻于空气气体的气囊,并因此而产生向上的浮力。系留气球系统包括系留气球球体、系留缆绳组件、锚泊设施和地面综合保障设施等。系留气球依靠浮力悬浮在空中,球体通过系缆与地面锚泊设施连接,通过调整系索的长度来调整球体的高度,从而为其他设备提供一个准静态的空中平台。A tethered balloon is a lighter-than-air, unpowered aerostat that has a bladder filled with lighter-than-air gas, which creates an upward buoyancy. The mooring balloon system includes mooring balloon spheres, mooring cable assemblies, mooring facilities and ground comprehensive support facilities. The tethered balloon is suspended in the air by buoyancy, and the sphere is connected to the ground anchoring facility through a mooring cable, and the height of the sphere is adjusted by adjusting the length of the lanyard, thereby providing a quasi-static aerial platform for other equipment.
典型的系留气球升空平台以系留气球为核心,包含球体、锚泊设施、系留系缆、有效载荷、地面控制系统等组成。其中系缆分为主缆、鼻系索和侧系索等。在锚泊状态时,通过球体鼻锥处鼻系索与两侧侧系索将球体约束于锚泊设施之上。A typical tethered balloon lift-off platform takes the tethered balloon as the core and consists of a sphere, an anchoring facility, a mooring cable, a payload, and a ground control system. The mooring cable is divided into main cable, nose lanyard and side lanyard. In the mooring state, the sphere is restrained on the mooring facility by the nose lanyard at the nose cone of the sphere and the side lanyards on both sides.
其中锚泊设施上,鼻系索与锚泊设施相连的位置为鼻塔端部。球体锚泊时需要鼻系索逐渐收紧于鼻绞盘上,通常鼻绞盘会放置在锚泊设施底部,方便人员操作。因此鼻塔端部不仅需要限制球体鼻锥部分位置,还需要使鼻系索灵活转向至地面处的鼻绞盘。Among them, on the mooring facility, the position where the nose lanyard is connected to the mooring facility is the end of the nose tower. When the ball is anchored, the nose lanyard needs to be gradually tightened on the nose winch. Usually, the nose winch will be placed at the bottom of the anchoring facility for easy operation by personnel. Therefore, the end of the nose tower not only needs to limit the position of the spherical nose cone, but also needs to flexibly turn the nose lanyard to the nose winch at the ground.
由于球体直径较大,鼻锥位置较高,所以鼻塔较高。而鼻塔端部需要与鼻系索相连接,通常会安排人员在鼻塔端部用手操作,费时费力不安全,是一项难题。另外,鼻系索从鼻塔端部中穿过,转向至下部的鼻绞盘,需要收放自如,且鼻系索有时松懈,鼻塔端部要保证其收放过程不能与周围结构产生相对摩擦,以免损失鼻系索强度,且在鼻系索松懈时不能卡在结构缝隙中,影响后续操作,这是另一难题。Due to the larger diameter of the sphere and the higher position of the nose cone, the nose tower is higher. However, the end of the nose tower needs to be connected with the nose lanyard. Usually, personnel are arranged to operate the end of the nose tower by hand, which is time-consuming, labor-intensive and unsafe, which is a difficult problem. In addition, the nose lanyard passes through the end of the nose tower and turns to the lower nasal winch, which needs to be retracted freely, and the nose lanyard is sometimes loose, and the end of the nose tower must ensure that the retraction process does not produce relative friction with the surrounding structure , so as not to lose the strength of the nasal lanyard, and when the nasal lanyard is loose, it cannot be stuck in the gap of the structure, which affects the subsequent operation, which is another problem.
发明内容SUMMARY OF THE INVENTION
本发明提供一种系留气球锚泊设施鼻塔端部结构,用以解决现有技术中鼻塔端部收放过程鼻系索与周围结构产生相对摩擦且在鼻系索松懈时容易卡在结构缝隙中的问题。The invention provides a nose tower end structure of a mooring balloon anchoring facility, which is used to solve the problem that in the prior art, the nose lanyard and the surrounding structure generate relative friction during the nose tower end retraction process, and the nasal lanyard is easy to be stuck in the structure when the nasal lanyard is loosened. Problems in the gap.
本发明提供一种系留气球锚泊设施鼻塔端部结构,包括:支架以及设置于所述支架上的卡圈、第一横轴、第二横轴、第一纵轴、第二纵轴和翻转机构;所述卡圈用于与系留气球的球体鼻锥接触,所述第一横轴具有第一状态和第二状态,在所述第一状态下,所述第一横轴与第二横轴、第一纵轴和第二纵轴之间围成鼻系索通道,所述鼻系索通道用于穿过所述系留气球的鼻系索;在所述第二状态下,所述第一横轴在所述鼻系索通道位于所述第一横轴一侧形成开口;所述卡圈上设置有径向缺口,所述径向缺口延伸至所述鼻系索通道的延伸路径上;所述翻转机构连接所述第一横轴的一端,所述翻转机构用于驱动所述第一横轴在所述第一状态和所述第二状态之间切换。The invention provides a nose tower end structure of a mooring balloon anchoring facility, comprising: a bracket and a collar arranged on the bracket, a first transverse axis, a second transverse axis, a first longitudinal axis, a second longitudinal axis and a Turning mechanism; the collar is used for contacting with the spherical nose cone of the captive balloon, the first transverse axis has a first state and a second state, and in the first state, the first transverse axis is in contact with the first transverse axis A nasal lanyard channel is formed between the two transverse axes, the first longitudinal axis and the second longitudinal axis, and the nasal lanyard channel is used to pass through the nasal lanyard of the mooring balloon; in the second state, The first transverse shaft forms an opening on one side of the nasal lanyard channel on the side of the first transverse shaft; the collar is provided with a radial gap, and the radial gap extends to the end of the nasal lanyard channel. on the extension path; the turning mechanism is connected to one end of the first horizontal shaft, and the turning mechanism is used to drive the first horizontal shaft to switch between the first state and the second state.
根据本发明提供的一种系留气球锚泊设施鼻塔端部结构,所述翻转机构包括翻转驱动杆、驱动转轴和复位扭簧;According to a nose tower end structure of a mooring balloon anchoring facility provided by the present invention, the inversion mechanism includes an inversion drive rod, a drive shaft and a return torsion spring;
所述驱动转轴转动连接于所述支架;the drive shaft is rotatably connected to the bracket;
所述第一横轴一端与所述驱动转轴转动连接;One end of the first horizontal shaft is rotatably connected with the driving shaft;
所述翻转驱动杆一端与所述驱动转轴固定连接,所述翻转驱动杆用于驱动所述驱动转轴轴向旋转以带动所述翻转驱动杆由第一状态向第二状态切换;One end of the overturning drive rod is fixedly connected with the drive shaft, and the overturning drive rod is used to drive the drive shaft to rotate axially to drive the overturning drive rod to switch from the first state to the second state;
所述复位扭簧连接所述驱动转轴,所述复位扭簧用于为所述驱动转轴提供带动所述第一横轴由第二状态切换至第一状态的弹性作用力。The return torsion spring is connected to the drive shaft, and the return torsion spring is used to provide the drive shaft with an elastic force that drives the first horizontal shaft to switch from the second state to the first state.
根据本发明提供的一种系留气球锚泊设施鼻塔端部结构,所述翻转驱动杆背离所述驱动转轴一端设置有拉环。According to the end structure of the nose tower of a mooring balloon anchoring facility provided by the present invention, a pull ring is provided at one end of the overturning drive rod facing away from the drive shaft.
根据本发明提供的一种系留气球锚泊设施鼻塔端部结构,所述系留气球锚泊设施鼻塔端部结构还包括限位组件,所述限位组件用于使所述第一横轴限制在第一状态或使所述第一横轴能够由第一状态切换至第二状态。According to the end structure of the nose tower of a mooring balloon anchoring facility provided by the present invention, the end structure of the nose tower of the mooring balloon anchoring facility further includes a limit component, and the limit component is used to make the first transverse axis Restricting to the first state or enabling the first transverse axis to be switched from the first state to the second state.
根据本发明提供的一种系留气球锚泊设施鼻塔端部结构,所述限位组件包括驱动拨叉、限位轴和弹性复位件,所述驱动拨叉用于驱动所述限位轴移离所述第一横轴由第一状态切换至第二状态的移动路径,所述弹性复位件用于为所述限位轴提供移动至所述第一横轴由第一状态切换至第二状态的移动路径上的弹性支撑力。According to a nose tower end structure of a mooring balloon anchoring facility provided by the present invention, the limit assembly includes a drive fork, a limit shaft and an elastic reset member, and the drive fork is used to drive the limit shaft to move A moving path from the first horizontal axis to switch from the first state to the second state, and the elastic reset member is used to provide the limit shaft to move to the first horizontal axis to switch from the first state to the second state The elastic support force on the movement path of the state.
根据本发明提供的一种系留气球锚泊设施鼻塔端部结构,所述限位轴轴向滑动连接于所述支架,所述驱动拨叉与所述限位轴铰接,所述弹性复位件沿所述限位轴的滑动方向弹性支撑所述限位轴。According to a nose tower end structure of a mooring balloon anchoring facility provided by the present invention, the limit shaft is axially slidably connected to the bracket, the drive fork is hinged with the limit shaft, and the elastic reset member The limiting shaft is elastically supported along the sliding direction of the limiting shaft.
根据本发明提供的一种系留气球锚泊设施鼻塔端部结构,所述支架上设置有限位槽,在所述第一状态下,所述第一横轴背离所述翻转机构一端位于所述限位槽内。According to the end structure of the nose tower of a mooring balloon anchoring facility provided by the present invention, the bracket is provided with a limiting groove, and in the first state, the end of the first transverse axis facing away from the turning mechanism is located in the in the limit slot.
根据本发明提供的一种系留气球锚泊设施鼻塔端部结构,所述系留气球锚泊设施鼻塔端部结构还包括外壳,所述外壳与所述支架固定连接,且罩设在所述第一横轴、第二横轴、第一纵轴、第二纵轴和翻转机构的外侧。According to a nose tower end structure of a mooring balloon anchoring facility provided by the present invention, the nose tower end structure of a mooring balloon anchoring facility further comprises a shell, the shell is fixedly connected with the bracket, and the cover is provided on the The first horizontal axis, the second horizontal axis, the first vertical axis, the second vertical axis and the outside of the turning mechanism.
根据本发明提供的一种系留气球锚泊设施鼻塔端部结构,所述卡圈由钢管焊接形成,且在所述径向缺口位置形成圆角。According to the end structure of the nose tower of a mooring balloon anchoring facility provided by the present invention, the collar is formed by welding a steel pipe, and a rounded corner is formed at the radial notch position.
根据本发明提供的一种系留气球锚泊设施鼻塔端部结构,所述第一横轴、第二横轴、第一纵轴和第二纵轴采用合金铝或尼龙材质。According to the nose tower end structure of a mooring balloon anchoring facility provided by the present invention, the first transverse axis, the second transverse axis, the first longitudinal axis and the second longitudinal axis are made of aluminum alloy or nylon material.
本发明提供的系留气球锚泊设施鼻塔端部结构,安装在鼻塔端部时,将系留气球的鼻系索穿过径向缺口和鼻系索通道,在第一横轴、第二横轴、第一纵轴和第二纵轴的限制下鼻系索松动时不会卡在结构缝隙中。第一横轴、第二横轴、第一纵轴和第二纵轴能够轴向旋转,使鼻系索收放阻力更小,不会与其他结构产生摩擦。The nose tower end structure of the mooring balloon mooring facility provided by the present invention, when installed at the nose tower end, the nose lanyard of the mooring balloon is passed through the radial gap and the nasal lanyard channel. Under the constraints of the transverse axis, the first longitudinal axis and the second longitudinal axis, the nasal lanyard will not be stuck in the structural gap when it is loose. The first transverse axis, the second transverse axis, the first longitudinal axis and the second longitudinal axis can be axially rotated, so that the resistance of the nose lanyard to be retracted is smaller, and friction with other structures is not generated.
第一横轴能够在第一状态和第二状态下切换,当需要穿入鼻系索或将鼻系索移出时,通过翻转机构驱动第一横轴切换至第二状态,鼻系索能够方便地移入鼻系索通道内或由鼻系索通道移出。将翻转机构通过绳索连接至地面时,还可以在地面通过绳索控制第一横轴的状态,操作方便快捷,从而省去了人员爬高去穿鼻系索,操作更安全。The first horizontal shaft can be switched between the first state and the second state. When the nose lanyard needs to be inserted or removed, the first horizontal shaft can be driven to switch to the second state by the turning mechanism, and the nasal lanyard can be conveniently into or out of the nasal lanyard channel. When the turning mechanism is connected to the ground through the rope, the state of the first horizontal axis can also be controlled through the rope on the ground, and the operation is convenient and quick, thereby eliminating the need for personnel to climb up to wear the nose lanyard, and the operation is safer.
附图说明Description of drawings
为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例或现有技术描述中所需要使用的附图作一简单地介绍,显而易见地,下面描述中的附图是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the accompanying drawings that need to be used in the description of the embodiments or the prior art. Obviously, the accompanying drawings in the following description These are some embodiments of the present invention. For those of ordinary skill in the art, other drawings can also be obtained according to these drawings without creative efforts.
图1是本发明提供的系留气球锚泊设施鼻塔端部结构示意图之一;Fig. 1 is one of the structural schematic diagrams of the nose tower of the mooring balloon anchoring facility provided by the present invention;
图2是本发明提供的系留气球锚泊设施鼻塔端部结构示意图之二(图中隐藏外壳);Fig. 2 is the second structural schematic diagram of the nose tower of the mooring balloon anchoring facility provided by the present invention (the casing is hidden in the figure);
图3是本发明提供的系留气球锚泊设施鼻塔端部结构示意图之三(图中隐藏外壳)。Fig. 3 is the third schematic diagram of the end structure of the nose tower of the mooring balloon anchoring facility provided by the present invention (the shell is hidden in the figure).
附图标记:Reference number:
1、卡圈; 2、支架; 3、外壳;1. Clamp; 2. Bracket; 3. Shell;
4、第一横轴; 5、第一纵轴; 6、第二横轴;4. The first horizontal axis; 5. The first vertical axis; 6. The second horizontal axis;
7、第二纵轴; 8、驱动转轴; 9、翻转驱动杆;7. Second longitudinal axis; 8. Driving shaft; 9. Turning over the driving rod;
10、拉环; 11、驱动拨叉; 12、限位轴;10. Pull ring; 11. Drive fork; 12. Limit shaft;
13、弹性复位件; 14、限位槽; 15、鼻系索通道;13. Elastic reset piece; 14. Limit slot; 15. Nose lanyard channel;
16、径向缺口。16. Radial notch.
具体实施方式Detailed ways
下面结合附图和实施例对本发明的实施方式作进一步详细描述。以下实施例用于说明本发明,但不能用来限制本发明的范围。The embodiments of the present invention will be described in further detail below with reference to the accompanying drawings and examples. The following examples are intended to illustrate the present invention, but not to limit the scope of the present invention.
在本发明实施例的描述中,需要说明的是,术语“中心”、“纵向”、“横向”、“上”、“下”、“前”、“后”、“左”、“右”、“竖直”、“水平”、“顶”、“底”、“内”、“外”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本发明实施例和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本发明实施例的限制。此外,术语“第一”、“第二”、“第三”仅用于描述目的,而不能理解为指示或暗示相对重要性。In the description of the embodiments of the present invention, it should be noted that the terms "center", "portrait", "horizontal", "top", "bottom", "front", "rear", "left", "right" , "vertical", "horizontal", "top", "bottom", "inside", "outside", etc. indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings, only for the convenience of describing this Inventive embodiments and simplified descriptions are not intended to indicate or imply that the devices or elements referred to must have a particular orientation, be constructed and operate in a particular orientation, and therefore should not be construed as limiting the embodiments of the present invention. Furthermore, the terms "first", "second", and "third" are used for descriptive purposes only and should not be construed to indicate or imply relative importance.
在本发明实施例的描述中,需要说明的是,除非另有明确的规定和限定,术语“相连”、“连接”应做广义理解,例如,可以是固定连接,也可以是可拆卸连接,或一体连接;可以是机械连接,也可以是电连接;可以是直接相连,也可以通过中间媒介间接相连。对于本领域的普通技术人员而言,可以具体情况理解上述术语在本发明实施例中的具体含义。In the description of the embodiments of the present invention, it should be noted that, unless otherwise expressly specified and limited, the terms "connected" and "connected" should be understood in a broad sense, for example, it may be a fixed connection or a detachable connection, Or integral connection; it can be mechanical connection or electrical connection; it can be directly connected or indirectly connected through an intermediate medium. Those of ordinary skill in the art can understand the specific meanings of the above terms in the embodiments of the present invention in specific situations.
在本发明实施例中,除非另有明确的规定和限定,第一特征在第二特征“上”或“下”可以是第一和第二特征直接接触,或第一和第二特征通过中间媒介间接接触。而且,第一特征在第二特征“之上”、“上方”和“上面”可是第一特征在第二特征正上方或斜上方,或仅仅表示第一特征水平高度高于第二特征。第一特征在第二特征“之下”、“下方”和“下面”可以是第一特征在第二特征正下方或斜下方,或仅仅表示第一特征水平高度小于第二特征。In the embodiments of the present invention, unless otherwise expressly specified and limited, the first feature "above" or "under" the second feature may be in direct contact with the first and second features, or the first and second features pass through the middle indirect contact with the media. Also, the first feature being "above", "over" and "above" the second feature may mean that the first feature is directly above or obliquely above the second feature, or simply means that the first feature is level higher than the second feature. The first feature being "below", "below" and "below" the second feature may mean that the first feature is directly below or obliquely below the second feature, or simply means that the first feature has a lower level than the second feature.
在本说明书的描述中,参考术语“一个实施例”、“一些实施例”、“示例”、“具体示例”、或“一些示例”等的描述意指结合该实施例或示例描述的具体特征、结构、材料或者特点包含于本发明实施例的至少一个实施例或示例中。在本说明书中,对上述术语的示意性表述不必须针对的是相同的实施例或示例。而且,描述的具体特征、结构、材料或者特点可以在任一个或多个实施例或示例中以合适的方式结合。此外,在不相互矛盾的情况下,本领域的技术人员可以将本说明书中描述的不同实施例或示例以及不同实施例或示例的特征进行结合和组合。In the description of this specification, description with reference to the terms "one embodiment," "some embodiments," "example," "specific example," or "some examples", etc., mean specific features described in connection with the embodiment or example , structures, materials, or features are included in at least one example or example of embodiments of the present invention. In this specification, schematic representations of the above terms are not necessarily directed to the same embodiment or example. Furthermore, the particular features, structures, materials or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. Furthermore, those skilled in the art may combine and combine the different embodiments or examples described in this specification, as well as the features of the different embodiments or examples, without conflicting each other.
下面结合图1-图3描述本发明实施例的系留气球锚泊设施鼻塔端部结构,包括:支架2以及设置于支架2上的卡圈1、第一横轴4、第二横轴6、第一纵轴5、第二纵轴7和翻转机构。The structure of the nose tower of the mooring balloon anchoring facility according to the embodiment of the present invention will be described below with reference to FIGS. 1 to 3 , including: a
其中,支架2由薄钢板焊接形成,用于连接各部分结构,并形成稳定的支撑。Among them, the
卡圈1用于与系留气球的球体鼻锥接触,其与系留气球接触位置位于卡圈1背离支架2一侧。卡圈1由钢管焊接形成,包括外环部分和用于连接外环部分与支架2的连杆部分。卡圈1所用的钢管均为外壁光滑的圆管结构,并且进一步的将卡圈1各部分的连接位置焊接为圆角结构,能够有效避免与系留气球接触时对系留气球的球体造成损害。The
第一横轴4、第二横轴6、第一纵轴5及第二纵轴7均转动连接于支架2背离卡圈1一侧,其中,第二横轴6两端可通过轴承连接支架2,使其具有较小的转动阻力。第一横轴4和第二横轴6平行间隔设置,且在垂直轴线方向上对齐,第一纵轴5和第二纵轴7平行间隔设置,且在垂直轴线方向上对齐。第一横轴4和第二横轴6垂直于第一纵轴5和第二纵轴7,第一横轴4与第二横轴6、第一纵轴5和第二纵轴7之间围成鼻系索通道15,鼻系索通道15沿卡圈1的轴向且垂直于第一横轴4、第二横轴6、第一纵轴5及第二纵轴7,鼻系索通道15用于穿过系留气球的鼻系索。卡圈1上设置有径向缺口16,径向缺口16延伸至鼻系索通道15的延伸路径上。The first horizontal shaft 4 , the second
第一横轴4具有第一状态和第二状态,在第一状态下,第一横轴4与第二横轴6、第一纵轴5和第二纵轴7之间围成鼻系索通道15,鼻系索穿过鼻系索通道15后,第一横轴4、第二横轴6、第一纵轴5和第二纵轴7对鼻系索形成限位,鼻系索无法侧向脱离鼻系索通道15。在第二状态下,第一横轴4在鼻系索通道15位于第一横轴4一侧形成开口,鼻系索能够由卡圈1的径向缺口16的开口位置沿卡圈1的径向移动到达鼻系索通道15,或由鼻系索通道15沿沿卡圈1的径向移动并由卡圈1的径向缺口16的开口位置移出。The first transverse axis 4 has a first state and a second state, and in the first state, a nose lanyard is enclosed between the first transverse axis 4 and the second
第一横轴4、第一纵轴5和第二纵轴7采用合金铝或尼龙材质,具有轻质、易加工和不损坏鼻系索的优点。The first transverse shaft 4, the first
翻转机构连接第一横轴4的一端,翻转机构用于驱动第一横轴4在第一状态和第二状态之间切换,从而能够方便地控制鼻系索通道15的侧向开口的开闭。The flipping mechanism is connected to one end of the first horizontal shaft 4, and the flipping mechanism is used to drive the first horizontal shaft 4 to switch between the first state and the second state, so as to conveniently control the opening and closing of the lateral opening of the
在本发明一个实施例中,翻转机构包括翻转驱动杆9、驱动转轴8和复位扭簧(图中未示出)。其中驱动转轴8转动连接于支架2,使其可产生轴向旋转,驱动转轴8的轴线方向垂直于第一横轴4的轴线方向。第一横轴4一端与驱动转轴8转动连接,第一横轴4与驱动转轴8的连接位置可以为驱动转轴8的轴向中心位置。In one embodiment of the present invention, the turning mechanism includes a turning driving rod 9, a driving shaft 8 and a return torsion spring (not shown in the figure). The drive shaft 8 is rotatably connected to the
翻转驱动杆9垂直于驱动转轴8,其一端与驱动转轴8固定连接,翻转驱动杆9绕驱动转轴8的轴线方向旋转时能够带动驱动转轴8轴向旋转以带动翻转驱动杆9由第一状态向第二状态切换。The inversion drive rod 9 is perpendicular to the drive shaft 8, and one end thereof is fixedly connected with the drive shaft 8. When the inversion drive rod 9 rotates around the axis of the drive shaft 8, it can drive the drive shaft 8 to rotate axially to drive the inversion drive rod 9 from the first state. Switch to the second state.
复位扭簧连接驱动转轴8,复位扭簧用于为驱动转轴8提供带动翻转驱动杆9由第二状态切换至第一状态的弹性作用力。The return torsion spring is connected to the drive shaft 8 , and the return torsion spring is used to provide the drive shaft 8 with an elastic force to drive the overturning drive rod 9 to switch from the second state to the first state.
在未向翻转驱动杆9施加外力时,在复位扭簧的作用下能够使第一横轴4持续维持在第一状态;在向翻转驱动杆9施加外力后,能够使第一横轴4由第一状态向第二状态切换,打开鼻系索通道15的侧向开口,此过程中,复位扭簧的弹性形变量逐渐增大,去除对翻转驱动杆9施加的外力后,复位扭簧的弹性作用下使第一横轴4恢复至第一状态。When no external force is applied to the inversion driving rod 9, the first transverse shaft 4 can be continuously maintained in the first state under the action of the return torsion spring; after the external force is applied to the inversion driving rod 9, the first transverse shaft 4 can be made The first state is switched to the second state, and the lateral opening of the
翻转驱动杆9背离驱动转轴8一端设置有拉环10,该拉环10能够用于连接绳索,操作人员在地面位置通过拉动绳索即可实现使第一横轴4由第一状态向第二状态切换的操作。A
在本发明一个实施例中,系留气球锚泊设施鼻塔端部结构还包括限位组件,限位组件用于使第一横轴4限制在第一状态或使第一横轴4能够由第一状态切换至第二状态。由此,可在不需要将第一横轴4切换至第二状态时,通过限位组件使第一横轴4稳定地处在第一状态位置,避免鼻系索在非人为操作下自行脱离鼻系索通道15。In an embodiment of the present invention, the end structure of the nose tower of the mooring balloon anchorage facility further includes a limit component, and the limit component is used to limit the first transverse shaft 4 in the first state or to enable the first transverse shaft 4 to pass from the first A state switches to a second state. Therefore, when the first horizontal shaft 4 does not need to be switched to the second state, the first horizontal shaft 4 can be stably placed in the first state position through the limiting assembly, so as to prevent the nose lanyard from being disengaged by itself without manual operation.
在本发明一个实施例中,限位组件包括驱动拨叉11、限位轴12和弹性复位件13,驱动拨叉11用于驱动限位轴12移离第一横轴4由第一状态切换至第二状态的移动路径,弹性复位件13用于为限位轴12提供移动至第一横轴4由第一状态切换至第二状态的移动路径上的弹性支撑力。驱动拨叉11未提供驱动力时,限位轴12在弹性复位件13的作用下始终位于第一横轴4由第一状态切换至第二状态的移动路径上,此时能够对第一横轴4形成阻挡作用,进而使第一横轴4能够维持在第一状态下。In one embodiment of the present invention, the limit assembly includes a
限位轴12滑动连接于支架2,并垂直于第一横杆,限位轴12的滑动方向沿其轴线方向。弹性复位件13可采用压缩弹簧,将弹性复位件13套设在限位轴12上,使其一端与支架2抵接,另一端与设置在限位轴12上的插销或垫片等结构抵接,为限位轴12提供轴向的弹性支撑力。在弹性复位件13的作用下能够使限位轴12的一端位于第一横轴4由第一状态切换至第二状态的移动路径上。驱动拨叉11的一端与限位轴12铰接,且支架2在驱动拨叉11的中部形成支点,拨动驱动拨叉11时,能够带动限位轴12轴向移动,限位轴12的端部移离第一横轴4由第一状态切换至第二状态的移动路径后,第一横轴4能够由第一状态切换至第二状态。The limiting
可选的,支架2上设置有限位槽14,在第一状态下,第一横轴4背离翻转机构一端位于限位槽14内,使第一横轴4能够稳定地轴向旋转。进一步地,可将限位轴12设置在限位槽14的上方,并且使限位轴12在压缩弹簧的作用下能够滑动至限位槽14的开口位置,实现对第一横轴4的稳定限位。Optionally, the
在本发明一个实施例中,系留气球锚泊设施鼻塔端部结构还包括外壳3,外壳3与支架2固定连接,且罩设在第一横轴4、第二横轴6、第一纵轴5、第二纵轴7和翻转机构的外侧。外壳3能够为各部分提供防尘的作用,同时也使外形更加整齐美观。外壳3可通过螺栓连接或卡接等可拆卸连接方式与支架2连接固定,以便于拆除维护。外壳3上形成有开口,能够便于将翻转驱动杆9和驱动拨叉11的端部漏在外面,或便于将绳索穿入外壳3中连接翻转驱动杆9和驱动拨叉11。外壳3为尼龙板或塑料板等非技术材料的薄板,降低系留气球锚泊设施鼻塔端部结构的整体重量。In an embodiment of the present invention, the end structure of the nose tower of the mooring balloon anchorage facility further includes a
使用过程中,使鼻系索穿过径向缺口16及鼻系索通道15后与鼻绞盘相连,鼻绞盘安置在锚泊设施底端,方便人员操作。分别通过绳索连接翻转驱动杆9和驱动拨叉11,在需要使鼻系索穿入鼻塔端部时,不用接触鼻塔端部,在地面操作翻转驱动杆9和驱动拨叉11的连接绳索即可,不需要人员爬高操作,能够提高操作安全。During use, the nasal lanyard is connected to the nasal winch after passing through the
最后应说明的是:以上实施例仅用以说明本发明的技术方案,而非对其限制;尽管参照前述实施例对本发明进行了详细的说明,本领域的普通技术人员应当理解:其依然可以对前述各实施例所记载的技术方案进行修改,或者对其中部分技术特征进行等同替换;而这些修改或者替换,并不使相应技术方案的本质脱离本发明各实施例技术方案的精神和范围。Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention, but not to limit them; although the present invention has been described in detail with reference to the foregoing embodiments, those of ordinary skill in the art should understand that it can still be The technical solutions described in the foregoing embodiments are modified, or some technical features thereof are equivalently replaced; and these modifications or replacements do not make the essence of the corresponding technical solutions deviate from the spirit and scope of the technical solutions of the embodiments of the present invention.
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