CN115108026A - A foldable rotor descent device for high-rise escape - Google Patents
A foldable rotor descent device for high-rise escape Download PDFInfo
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- CN115108026A CN115108026A CN202210585669.6A CN202210585669A CN115108026A CN 115108026 A CN115108026 A CN 115108026A CN 202210585669 A CN202210585669 A CN 202210585669A CN 115108026 A CN115108026 A CN 115108026A
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- 238000010168 coupling process Methods 0.000 claims description 7
- 238000005859 coupling reaction Methods 0.000 claims description 7
- 241000208140 Acer Species 0.000 abstract description 11
- 238000000034 method Methods 0.000 abstract description 5
- 230000000694 effects Effects 0.000 abstract description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 abstract description 2
- 238000002955 isolation Methods 0.000 abstract description 2
- 239000000463 material Substances 0.000 abstract 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D19/00—Non-canopied parachutes
- B64D19/02—Rotary-wing parachutes
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- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62B—DEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
- A62B1/00—Devices for lowering persons from buildings or the like
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Abstract
Description
技术领域technical field
本发明涉及高楼逃生用具技术领域,具体是一种用于高楼逃生的可折叠旋翼缓降装置。The invention relates to the technical field of high-rise escape appliances, in particular to a foldable rotor slow-down device for high-rise escape.
背景技术Background technique
随着我国发展的越来越快,高层建筑普及率大大提升。然而高楼发生险情后的逃生问题一直没有有效的解决方案,传统降落伞、逃生背包无法满足需求。因此发明了一种简易可折叠旋翼缓降装置,可广泛应用于高楼逃生等领域。With the rapid development of our country, the penetration rate of high-rise buildings has greatly increased. However, there has been no effective solution to the escape problem after a dangerous situation occurs in a high-rise building, and traditional parachutes and escape backpacks cannot meet the needs. Therefore, a simple and foldable rotor slow-down device was invented, which can be widely used in the fields of high-rise escape and the like.
自然界中存在的枫树种子则是另一种空中降落减速解决方案。在椭圆形种子的侧面,有一片轻而薄的翼面。在枫树种子从树上落下来的时候,空气推动翼面,使整个枫树种子旋转,在其前缘产生涡流进而产生升力,减缓枫树种子的下落速度,使其能飘向更远的地方。本发明的原理即来自于枫树种子,具有结构简单,有效可靠的特点。Maple seeds found in nature are another airborne deceleration solution. On the sides of the oval seeds, there is a light and thin airfoil. When the maple seeds fall from the tree, the air pushes the airfoil, causing the entire maple seed to rotate, generating eddy currents on its leading edge to generate lift, slowing the falling speed of the maple seeds, allowing them to float farther. place. The principle of the invention comes from the maple seeds, and has the characteristics of simple structure, effective and reliable.
发明内容SUMMARY OF THE INVENTION
本发明为了解决现有技术的问题,提供了一种用于高楼逃生的可折叠旋翼缓降装置,结构简单、节省空间、操作方便、降落稳定、便于携带,不需要过多维护。In order to solve the problems of the prior art, the present invention provides a foldable rotor slow-down device for high-rise escape, which has simple structure, space saving, convenient operation, stable landing, easy portability, and does not require excessive maintenance.
本发明包括通过联接器联接的刚性轴和伸缩翼面,刚性轴连接有背负装置。The present invention includes a rigid shaft and a telescopic airfoil connected by a coupling, and the rigid shaft is connected with a piggyback device.
所述联接器包括底座和旋转轴,其中,底座固定在刚性轴上,旋转轴底部与底座通过轴承连接,旋转轴在底座上绕自身中心轴转动,旋转轴上部为与水平面具有夹角的倾斜段,倾斜段与伸缩翼面连接。The coupling includes a base and a rotating shaft, wherein the base is fixed on the rigid shaft, the bottom of the rotating shaft is connected with the base through a bearing, the rotating shaft rotates around its central axis on the base, and the upper part of the rotating shaft is inclined with an included angle to the horizontal plane. The inclined section is connected with the telescopic airfoil.
所述伸缩翼面包括伸缩杆、拉线、卡环和翼面帆布,伸缩杆底端与旋转轴的倾斜段顶端固定连接,伸缩杆和拉线通过卡环首尾连接,伸缩杆和拉线围成的区域设置有翼面帆布,伸缩杆伸长时拉线拉动伸缩杆顶端使伸缩杆弯曲,此时翼面帆布展开形成类枫树种子的形状。The telescopic airfoil includes a telescopic rod, a pull wire, a snap ring and an airfoil canvas. The bottom end of the telescopic rod is fixedly connected with the top end of the inclined section of the rotating shaft. The telescopic rod and the pull wire are connected end-to-end through the snap ring, and the area enclosed by the telescopic rod and the pull wire An airfoil canvas is provided, and when the telescopic rod is extended, the pulling wire pulls the top end of the telescopic rod to bend the telescopic rod, and at this time, the airfoil canvas unfolds to form a maple-like seed shape.
进一步改进,所述背负装置置包括固定带、环扣、背带,固定带系在环扣上,环扣通过背带与刚性轴连接。In a further improvement, the carrying device includes a fixing strap, a loop buckle and a strap, the fixing strap is fastened on the loop buckle, and the loop buckle is connected with the rigid shaft through the strap.
进一步改进,所述旋转轴的倾斜段与水平位置成19°夹角,使载重发挥配重的作用,减小翼面面积。In a further improvement, the inclined section of the rotating shaft forms an included angle of 19° with the horizontal position, so that the load acts as a counterweight and reduces the airfoil area.
进一步改进,所述旋转轴底部与底座连接的轴承处通过盖子固定。In a further improvement, the bearing where the bottom of the rotating shaft is connected to the base is fixed by a cover.
进一步改进,所述伸缩杆采用手动、气动或弹簧实现伸缩。In a further improvement, the telescopic rod can be extended manually, pneumatically or by spring.
进行高楼逃生时,将固定带系在身上,打开伸缩杆,翼面自然展开成类枫树种子的形状,此时从窗户逃生达到缓降效果,可以实现平稳安全的逃生。When escaping from a high-rise building, tie the fixing belt to the body, open the telescopic rod, and the wing surface naturally unfolds into the shape of a maple seed. At this time, escaping from the window achieves a slow-down effect, which can achieve a smooth and safe escape.
本发明有益效果在于:本发明翼面展开时形似枫树种子,缓降原理与其相似,即在下降过程中自动旋转,在其前缘产生涡流,产生升力减慢其下降速度达到缓降效果。本发明结构简单、节省空间、操作方便、降落稳定、便于携带,不需要过多维护。The beneficial effects of the present invention are: the airfoil of the present invention resembles a maple seed when unfolded, and the principle of slow descent is similar to that, that is, it automatically rotates during the descending process, generates eddy currents at its leading edge, and generates lift to slow down its descending speed to achieve a slow descent effect. The invention has the advantages of simple structure, space saving, convenient operation, stable landing, easy portability, and no need for excessive maintenance.
附图说明Description of drawings
为了更清楚地说明本发明实施例中的技术方案,下面将对实施例中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅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它的附图。In order to illustrate the technical solutions in the embodiments of the present invention more clearly, the following briefly introduces the drawings required in the embodiments. Obviously, the drawings in the following description are only some embodiments of the present invention. For those of ordinary skill in the art, other drawings can also be obtained from these drawings without any creative effort.
图1所示为本发明具体实施例中装置的示意图;1 is a schematic diagram of a device in a specific embodiment of the present invention;
图2所示为发明具体实施例中联接器的放大剖面图;Figure 2 shows an enlarged cross-sectional view of a connector in a specific embodiment of the invention;
图3所示为发明具体实施例中伸缩杆和翼面的放大示意图。FIG. 3 is an enlarged schematic view of a telescopic rod and an airfoil in a specific embodiment of the invention.
图中,固定带1、环扣2、背带3、刚性轴4、联接器5、伸缩翼面6、底座7、旋转轴8、盖子9、伸缩杆10、拉线11、卡环12和翼面帆布13。In the figure, fixed belt 1, loop buckle 2, strap 3, rigid shaft 4, coupling 5, telescopic airfoil 6,
具体实施方式Detailed ways
下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其它实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
如图1所示,可折叠旋翼缓降装置包括固定带1、环扣2、背带3、刚性轴4、联接器5、伸缩翼面6。所述固定带1系在环扣2上,通过背带3与刚性轴4连接,刚性轴4与伸缩杆和翼面6通过联接器5连接,实现运动隔离。伸缩杆可采用手动、气动或弹簧实现伸缩。进行高楼逃生时,将固定带系在身上,打开伸缩杆,翼面自然展开成类枫树种子的形状,此时从窗户逃生达到缓降效果,可以实现平稳安全的逃生。As shown in FIG. 1 , the foldable rotor descending device includes a fixed belt 1 , a loop buckle 2 , a back belt 3 , a rigid shaft 4 , a coupling 5 , and a telescopic airfoil 6 . The fixing belt 1 is tied on the buckle 2 and is connected with the rigid shaft 4 through the back strap 3, and the rigid shaft 4 is connected with the telescopic rod and the airfoil 6 through the coupling 5 to realize motion isolation. The telescopic rod can be extended manually, pneumatically or by spring. When escaping from a high-rise building, tie the fixing belt to the body, open the telescopic rod, and the wing surface naturally unfolds into the shape of a maple seed. At this time, escaping from the window achieves a slow-down effect, which can achieve a smooth and safe escape.
如图2所示,联接器5包括底座7、旋转轴8、盖子9。底座7固定在刚性轴4上,旋转轴8连接伸缩杆和翼面,与水平位置成19°夹角,使载重发挥配重的作用,减小翼面面积,可360°旋转,盖子9可防止底座与旋转轴分离。As shown in FIG. 2 , the coupling 5 includes a
如图3所示,伸缩翼面6包括伸缩杆10、拉线11、卡环12和翼面帆布13。伸缩杆10和拉线11通过卡环12首尾连接,翼面展开时,伸缩杆自然弯曲,翼面帆布13成类枫树种子的形状,通过套筒或铁环与伸缩杆滑动连接。As shown in FIG. 3 , the telescopic airfoil 6 includes a
具体实施时最优化翼面面积和总体重量估计范围如下,由现有人工枫树种子数据等比例放大得到。In the specific implementation, the optimal airfoil area and the estimated range of the overall weight are as follows, which are obtained by proportionally magnifying the existing artificial maple seed data.
载重(kg) 翼面面积(m2) 总体重量(kg)Load (kg) Airfoil area (m2) Overall weight (kg)
20(物资/儿童) 10 2220 (supplies/children) 10 22
40(部分成年女性) 20 4440 (some adult women) 20 44
60(成人) 30 6660 (adult) 30 66
80(部分成年男性) 40 8880 (some adult males) 40 88
本说明书中的各个实施例均采用递进的方式描述,各个实施例之间相同相似的部分互相参见即可,每个实施例重点说明的都是与其他实施例的不同之处。尤其,对于设备实施例而言,以上所述仅是本发明的优选实施方式,由于其基本相似于方法实施例,所以描述得比较简单,相关之处参见方法实施例的部分说明即可。以上所述,仅为本发明的具体实施方式,但本发明的保护范围并不局限于此,任何熟悉本技术领域的技术人员在本发明揭露的技术范围内,对于本技术领域的普通技术人员来说,可轻易想到的变化或替换,在不脱离本发明原理的前提下,都应涵盖在本发明的保护范围之内。因此,本发明的保护范围应该以权利要求的保护范围为准。Each embodiment in this specification is described in a progressive manner, and the same and similar parts between the various embodiments may be referred to each other, and each embodiment focuses on the differences from other embodiments. In particular, for the device embodiments, the above descriptions are only preferred implementations of the present invention. Since they are basically similar to the method embodiments, the description is relatively simple. For relevant details, please refer to the partial descriptions of the method embodiments. The above are only specific embodiments of the present invention, but the protection scope of the present invention is not limited thereto. In other words, any easily conceivable changes or substitutions should be included within the protection scope of the present invention without departing from the principles of the present invention. Therefore, the protection scope of the present invention should be subject to the protection scope of the claims.
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Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3401906A (en) * | 1966-05-03 | 1968-09-17 | Ryan Aeronautical Co | Gyrochute |
US3662978A (en) * | 1970-10-22 | 1972-05-16 | Kaman Aerospace Corp | Aircraft ejection seat vehicle stowed rotor |
DE202004017642U1 (en) * | 2004-11-10 | 2005-02-10 | Pakulov, Anatoliy | Free-fall escape apparatus for high-rise building has two rigid rotors and load attachment point |
CN104386254A (en) * | 2014-10-27 | 2015-03-04 | 南京航空航天大学 | Autorotative rotary-wing parachute |
KR20210131043A (en) * | 2020-04-23 | 2021-11-02 | 청주대학교 산학협력단 | falling type emergency escape apparatus |
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2022
- 2022-05-26 CN CN202210585669.6A patent/CN115108026B/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3401906A (en) * | 1966-05-03 | 1968-09-17 | Ryan Aeronautical Co | Gyrochute |
US3662978A (en) * | 1970-10-22 | 1972-05-16 | Kaman Aerospace Corp | Aircraft ejection seat vehicle stowed rotor |
DE202004017642U1 (en) * | 2004-11-10 | 2005-02-10 | Pakulov, Anatoliy | Free-fall escape apparatus for high-rise building has two rigid rotors and load attachment point |
CN104386254A (en) * | 2014-10-27 | 2015-03-04 | 南京航空航天大学 | Autorotative rotary-wing parachute |
KR20210131043A (en) * | 2020-04-23 | 2021-11-02 | 청주대학교 산학협력단 | falling type emergency escape apparatus |
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