CN201350969Y - Tethered balloon bowknot device - Google Patents
Tethered balloon bowknot device Download PDFInfo
- Publication number
- CN201350969Y CN201350969Y CNU2008202411978U CN200820241197U CN201350969Y CN 201350969 Y CN201350969 Y CN 201350969Y CN U2008202411978 U CNU2008202411978 U CN U2008202411978U CN 200820241197 U CN200820241197 U CN 200820241197U CN 201350969 Y CN201350969 Y CN 201350969Y
- Authority
- CN
- China
- Prior art keywords
- bow tie
- bowknot
- bowknots
- pair
- rope
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
Disclosed is a tethered balloon bowknot device. Bearing strips (1-1) are fixed on pull rings (1-2), the bearing strips (1-1) are reversely folded in a pair of bowknots (1), a bowknot rope (3) is threaded in a ring (3), two ends of the bowknot rope are respectively connected with the pull rings (1-2) of the bowknots (1), and one end of a travel rope (4) is connected with the ring (3). The tethered balloon bowknot device has the advantages that the structural form and force loading of the bowknots are arranged symmetrically no matter the bowknots are forwards or reversely arranged because the bearing strips are reversely folded in the pair of bowknots, the bowknot device has simple structure, has the general function of a tethered balloon bowknot device, and has more reasonable structure and improves the loading and force transferring capabilities of the bowknots.
Description
Technical field
The utility model relates to the aerial mooring gear field that the utility model relates to aerostatics.Relate in particular to a kind of captive balloon bow tie device.
Background technology
Captive balloon bow tie device is mainly used in the aerial mooring of aerostatics.The folding layout bar of load bar has very big randomness in the existing captive balloon bow tie device, and it often is arranged to the past edge contraction (see figure 2) of both sides load bar in a pair of bow tie.Its weak point is to cause bow tie stressed and power transmission is uneven, causes the bow tie load-carrying capacity to descend.
The utility model content
The purpose of this utility model is exactly at the existing above-mentioned deficiency of bow tie device, and a kind of captive balloon bow tie device is provided.
The utility model is by a kind of captive balloon bow tie device, and it is made up of a pair of bow tie, bow tie rope, the collar, drag-line, and a pair of bow tie is made up of load bar and draw ring respectively; Be fixed on the draw ring after the load bar is folding, and the load bar becomes folded inverted in a pair of bow tie, the bow tie rope is through in the collar, and two ends link to each other with the draw ring of a pair of bow tie respectively, and drag-line one end links to each other with the collar.The utility model has the advantages that: because the load bar becomes folded inverted in a pair of bow tie, so no matter its version of the positive and negative layout of bow tie and the stressed symmetric arrangement that all is, it is simple in structure, not only satisfied the general function of captive balloon bow tie, and structure is more reasonable, improves the load-carrying capacity and the power transmission ability of bow tie.
Description of drawings
Accompanying drawing 1 is the utility model structural representation.Accompanying drawing 2 is the folding scheme drawing of former bow tie load bar.Accompanying drawing 3 is the folding scheme drawing of the utility model bow tie load bar.
The specific embodiment
As shown in Figure 1, after load bar 1-1 is folding folding point is fixed on the draw ring 1-2, and load bar 1-1 becomes folded inverted (see figure 3) in a pair of bow tie 1, bow tie rope 3 is through in the collar 3, two ends link to each other with the draw ring 1-2 of a pair of bow tie 1 respectively, and drag-line 4 one ends link to each other with the collar 3.Using method is with former bow tie device.
Can on original captive balloon bow tie device basic, reequip.Become folded inverted symmetric arrangement to get final product both sides load bar in original captive balloon bow tie device.
Claims (1)
1, a kind of captive balloon bow tie device is characterized in that it is made up of a pair of bow tie (1), bow tie rope (2), the collar (3), drag-line (4), and a pair of bow tie is made up of load bar (1-1) and draw ring (1-2) respectively; Be fixed on the draw ring (1-2) after load bar (1-1) is folding, and it is folded inverted that load bar (1-1) becomes in a pair of bow tie (1), bow tie rope (3) is through in the collar (3), and two ends link to each other with the draw ring (1-2) of a pair of bow tie (1) respectively, and drag-line (4) one ends link to each other with the collar (3).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNU2008202411978U CN201350969Y (en) | 2008-12-27 | 2008-12-27 | Tethered balloon bowknot device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNU2008202411978U CN201350969Y (en) | 2008-12-27 | 2008-12-27 | Tethered balloon bowknot device |
Publications (1)
Publication Number | Publication Date |
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CN201350969Y true CN201350969Y (en) | 2009-11-25 |
Family
ID=41374355
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNU2008202411978U Expired - Fee Related CN201350969Y (en) | 2008-12-27 | 2008-12-27 | Tethered balloon bowknot device |
Country Status (1)
Country | Link |
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CN (1) | CN201350969Y (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102285444A (en) * | 2011-06-07 | 2011-12-21 | 北方电科集团有限公司 | Kite airship attitude adjusting device |
CN105667753A (en) * | 2016-03-03 | 2016-06-15 | 上海交通大学 | Multi-point bearing loop for aerostat |
CN106654519A (en) * | 2016-12-12 | 2017-05-10 | 中国特种飞行器研究所 | Arrangement structure of captive balloon-carrying antenna |
CN110920852A (en) * | 2019-12-04 | 2020-03-27 | 中国特种飞行器研究所 | Mooring balloon anchoring assembly |
CN111776192A (en) * | 2020-06-01 | 2020-10-16 | 中国科学院空天信息创新研究院 | Captive balloon main node posture adjusting mechanism |
-
2008
- 2008-12-27 CN CNU2008202411978U patent/CN201350969Y/en not_active Expired - Fee Related
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102285444A (en) * | 2011-06-07 | 2011-12-21 | 北方电科集团有限公司 | Kite airship attitude adjusting device |
CN105667753A (en) * | 2016-03-03 | 2016-06-15 | 上海交通大学 | Multi-point bearing loop for aerostat |
CN106654519A (en) * | 2016-12-12 | 2017-05-10 | 中国特种飞行器研究所 | Arrangement structure of captive balloon-carrying antenna |
CN106654519B (en) * | 2016-12-12 | 2019-01-25 | 中国特种飞行器研究所 | A kind of captive balloon carries the arragement construction of antenna |
CN110920852A (en) * | 2019-12-04 | 2020-03-27 | 中国特种飞行器研究所 | Mooring balloon anchoring assembly |
CN111776192A (en) * | 2020-06-01 | 2020-10-16 | 中国科学院空天信息创新研究院 | Captive balloon main node posture adjusting mechanism |
CN111776192B (en) * | 2020-06-01 | 2021-09-28 | 中国科学院空天信息创新研究院 | Captive balloon main node posture adjusting mechanism |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C56 | Change in the name or address of the patentee | ||
CP02 | Change in the address of a patent holder |
Address after: 448001 No. 8, air route, Hubei, Jingmen Patentee after: China Special Vehicle Research Institute Address before: 448001 No. 8, air route, Shayang County, Hubei Province Patentee before: China Special Vehicle Research Institute |
|
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20091125 Termination date: 20161227 |