CN109866910A - A kind of captive balloon monoblock type empennage - Google Patents
A kind of captive balloon monoblock type empennage Download PDFInfo
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- CN109866910A CN109866910A CN201711272030.8A CN201711272030A CN109866910A CN 109866910 A CN109866910 A CN 109866910A CN 201711272030 A CN201711272030 A CN 201711272030A CN 109866910 A CN109866910 A CN 109866910A
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- Prior art keywords
- empennage
- covering
- root rib
- air bag
- rib
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Abstract
The present invention relates to a kind of captive balloon monoblock type empennages, it is characterized by: the empennage is by covering (1), root rib (2), tip rib (3) composition, the covering (1) of empennage is connected by heat seal item (8), setting partition (4) guarantees empennage shape inside empennage, partition (4) and covering (1), root rib (2) is connected by partition T-shaped piece (5), the covering (1) of empennage is connect by covering T-shaped piece (7) with root rib (2) and forms closed empennage, the root rib (2) of empennage is connect by heat seal item (8) with air bag.Captive balloon empennage of the present invention provides a kind of new type of attachment, eliminates the installation of empennage root rib and air bag in use, shortens captive balloon inflation time.A set of pressure regulating system can be shared with air bag, simplified the complexity of system, alleviated construction weight.
Description
Technical field
The invention patent relates to a kind of captive balloon monoblock type empennages, belong to aerostatics technical field.
Background technique
Captive balloon is widely used in military-civil field now, plays positive work for national defense construction and economic development
With.Traditional captive balloon empennage is using the form being separately separated with air bag.Some empennages are connected to air bag using outside
Form, need in addition to design communicating pipe and jointing, soft or hard connection considers that type of attachment and air-tightness design again;Have
Empennage fills air, to guarantee empennage shape and rigidity in use, needs individually to increase pressure regulating system.Both sides
Formula increases the complexity of design and processing, meanwhile, it was both increased while increasing complexity as one kind of aircraft
Weight also virtually increases failure risk point, is unfavorable for safety.
In addition, separate type empennage operates also inconvenience in use.Due to empennage and the one of the use of air bag junction
As be velcro fastener, empennage and air bag after processing is completed is all bigger, and weight is installed often relatively difficult also than heavier, has
When also need to do over again.
Summary of the invention
The purpose of invention
Facilitate the later period to use, simplify system complexity, mitigates weight.
Technical solution
A kind of captive balloon monoblock type empennage, the empennage are made of covering 1, root rib 2, tip rib 3, and the covering 1 of empennage is logical
The connection of heat seal item 8 is crossed, setting partition 4 guarantees empennage shape inside empennage, and partition 4 and covering 1, root rib 2 pass through partition T-shaped piece 5
The covering 1 of connection, empennage connect and forms closed empennage by covering T-shaped piece 7 with root rib 2, and the root rib 2 of empennage passes through heat seal
Item 8 is connect with air bag.In order to meet the connection of empennage and air bag, there is communication port 6 in the design of 2 taper of empennage root rib.To guarantee to connect
Intensity after port opening, design, which has, at communication port 6 reinforces lining cloth 9.The 2 theoretical size incorporation engineering of root rib for pressing empennage calculates
And it cuts out and removes corresponding covering on air bag.Empennage after processing is completed, can carry out independent air-tight test.
The effect of invention
Captive balloon empennage provides a kind of new type of attachment, eliminates the peace of empennage root rib and air bag in use
Dress shortens captive balloon inflation time.
Detailed description of the invention
Fig. 1 is structure of the invention main body schematic diagram;
Fig. 2 is root rib connection partial schematic diagram of the present invention;
Fig. 3 is empennage of the present invention and air bag connection schematic diagram;
Specific embodiment
As shown in Figure 1-3, empennage is mainly made of covering 1, root rib 2, tip rib 3 and partition 4, empennage root rib 2 is pressed on air bag
Theoretical size incorporation engineering, which is calculated, removes corresponding covering by sanction.In addition for empennage to be connected to air bag, there is company in the design of empennage root rib 2
Port 6.Empennage after processing is completed, can carry out independent air-tight test, finally with heat seal item 8 by empennage and air bag be linked to be one it is whole
Body.
The present invention provides a kind of new type of attachment, eliminates the installation of empennage root rib and air bag in use, contracts
Short captive balloon inflates time.A set of pressure regulating system can be shared with air bag, simplifies the complexity of system, mitigated
Construction weight.It ensure that the intensity of tail structure, there is stronger popularization and application foreground.
Claims (5)
1. a kind of captive balloon monoblock type empennage, it is characterised in that: the empennage is by covering (1), root rib (2), tip rib (3) group
At for the covering (1) of empennage by heat seal item (8) connection, empennage inside setting partition (4) guarantees empennage shape, partition (4) and illiteracy
Skin (1), root rib (2) are connected by partition T-shaped piece (5), and the covering (1) of empennage is connect with root rib (2) by covering T-shaped piece (7)
And closed empennage is formed, the root rib (2) of empennage is connect by heat seal item (8) with air bag.
2. empennage as described in claim 1, it is characterised in that: in order to meet the connection of empennage and air bag, in empennage root rib (2)
Taper design has communication port (6).
3. empennage as claimed in claim 2, it is characterised in that: to guarantee the intensity after communication port opening, at communication port (6)
Design has reinforcement lining cloth (9).
4. empennage as described in claim 1, it is characterised in that: root rib (2) the theoretical size incorporation engineering for pressing empennage calculates simultaneously
Sanction removes corresponding covering on air bag.
5. empennage as described in claim 1, it is characterised in that: empennage after processing is completed, can carry out independent air-tight test.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711272030.8A CN109866910A (en) | 2017-12-04 | 2017-12-04 | A kind of captive balloon monoblock type empennage |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711272030.8A CN109866910A (en) | 2017-12-04 | 2017-12-04 | A kind of captive balloon monoblock type empennage |
Publications (1)
Publication Number | Publication Date |
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CN109866910A true CN109866910A (en) | 2019-06-11 |
Family
ID=66915230
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201711272030.8A Pending CN109866910A (en) | 2017-12-04 | 2017-12-04 | A kind of captive balloon monoblock type empennage |
Country Status (1)
Country | Link |
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CN (1) | CN109866910A (en) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201338725Y (en) * | 2008-12-27 | 2009-11-04 | 中国特种飞行器研究所 | Captive balloon platform system with lightening protecting device |
CN102092471A (en) * | 2009-12-12 | 2011-06-15 | 襄樊宏伟航空器有限责任公司 | Floating platform for mooring hot air airship |
CN201980413U (en) * | 2010-12-22 | 2011-09-21 | 中国特种飞行器研究所 | A soft and semi-hard novel airship air bag |
CN205931211U (en) * | 2016-07-20 | 2017-02-08 | 湖南航天远望科技有限公司 | Tail wing structure and staying ship are aerifyd to staying ship |
CN206623981U (en) * | 2016-12-27 | 2017-11-10 | 东莞前沿技术研究院 | Attachment structure and aerostatics for aerostatics |
-
2017
- 2017-12-04 CN CN201711272030.8A patent/CN109866910A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201338725Y (en) * | 2008-12-27 | 2009-11-04 | 中国特种飞行器研究所 | Captive balloon platform system with lightening protecting device |
CN102092471A (en) * | 2009-12-12 | 2011-06-15 | 襄樊宏伟航空器有限责任公司 | Floating platform for mooring hot air airship |
CN201980413U (en) * | 2010-12-22 | 2011-09-21 | 中国特种飞行器研究所 | A soft and semi-hard novel airship air bag |
CN205931211U (en) * | 2016-07-20 | 2017-02-08 | 湖南航天远望科技有限公司 | Tail wing structure and staying ship are aerifyd to staying ship |
CN206623981U (en) * | 2016-12-27 | 2017-11-10 | 东莞前沿技术研究院 | Attachment structure and aerostatics for aerostatics |
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PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
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RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190611 |
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RJ01 | Rejection of invention patent application after publication |