CN206766370U - A kind of unmanned plane high-pressure air source launches separator - Google Patents
A kind of unmanned plane high-pressure air source launches separator Download PDFInfo
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- CN206766370U CN206766370U CN201720342915.XU CN201720342915U CN206766370U CN 206766370 U CN206766370 U CN 206766370U CN 201720342915 U CN201720342915 U CN 201720342915U CN 206766370 U CN206766370 U CN 206766370U
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- unmanned plane
- sealing ring
- inlet cylinder
- pressure air
- air source
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Abstract
The utility model discloses a kind of unmanned plane high-pressure air source to launch separator, including inlet cylinder, two sprues are equipped with push rod in the middle part of relative end face, and blowing mouth is stretched out in the end of push rod, connected between two push rod opposite ends by fixture block with neck, and fixture block is in truncated cone-shaped, the upper end of the gas outlet is circumferentially with the sealing ring of annular, and inlet cylinder is provided with annular seal groove corresponding with sealing ring, and the second sealing ring is equipped with the interior outer face that the seal groove contacts with sealing ring.The unmanned plane high-pressure air source launches separator, inlet cylinder and gas outlet are equipped with blowing mouth, and blowing mouth is in circular platform type, is inside plugged with the sprue of circular platform type, like this internally extruded in the presence of gas tighter, it is not easy gas leakage, the spring top clamping that passes behind of sprue seals, relatively simple for structure, also allow for safeguarding, cost is also than relatively low, and fixture block and neck are in order to easy to connect, and sealing ring and seal groove are then to play sealing function.
Description
Technical field
Unmanned plane transmitting separation technology field is the utility model is related to, specially a kind of unmanned plane high-pressure air source transmitting separation
Device.
Background technology
Current unmanned plane is generally using whirlpool spray or fanjet (hereinafter referred to as engine), in ground start
When need high-pressure air source blow and to turn.Under high altitude condition, oxygen, ground are required supplementation with inspiring the engine of motor to start
High-pressure air source to engine using most important.After engine starts successfully, implement unmanned plane transmitting when, it is necessary to cutoff high
Source of the gas simultaneously separates with unmanned plane.The high-pressure air source separate mode used at present is vertical separation, i.e., isolating construction is perpendicular to nobody
Machine body, the separation of high-pressure air source is realized by manual operation or motor drive mechanism.Because engine has run at high speed, manual operation
With security risk, and motor drive mechanism complex designing, and exist and safeguard and the problems such as reliability.Therefore, in practical application
Need a kind of easy and reliable source of the gas separate mode.In the market also has unmanned plane high-pressure air source to launch separator, such as
Notification number is the U of CN 202728580 patent, and still, its separator structure is too complicated, and thermal capacitance is fragile over time,
Production cost is also higher.
Utility model content
A kind of the defects of technical problem that the utility model solves is to overcome prior art construction complexity, there is provided unmanned plane
High-pressure air source launches separator.The unmanned plane high-pressure air source transmitting separator has the characteristics that simple in construction.
To achieve the above object, the utility model provides following technical scheme：A kind of unmanned plane high-pressure air source transmitting separation
Device, including inlet cylinder, the inlet cylinder is fixed on the rear end of unmanned plane, and unmanned plane is located on guide rail, the inlet cylinder
Rear end is connected with gas outlet, and gas outlet is fixed on guide rail, and the upper end of the inlet cylinder is connected with the engine of unmanned plane, and
The lower end of gas outlet is connected with high-pressure air source, and the gas transmission of circular platform type is offered on the relative end face of the inlet cylinder and gas outlet
Mouthful, and the small head end of two blowing mouths is relative, and the sprue for the circular platform type being engaged is plugged with the blowing mouth, and after sprue
Side is connected with support frame by spring, and two support frames are separately fixed on inlet cylinder and gas outlet, the circumferential card of the sprue
The first sealing ring is connected to, is equipped with push rod in the middle part of the relative end face of two sprues, and blowing mouth is stretched out in the end of push rod, two
Connected between push rod opposite end by fixture block with neck, and fixture block is in truncated cone-shaped, the upper end of the gas outlet is circumferentially with annular
Sealing ring, and inlet cylinder is provided with annular seal groove corresponding with sealing ring, and the seal groove contacts interior with sealing ring
The second sealing ring is equipped with outer face.
Preferably, the inside of the sprue is in hollow structure.
Preferably, the openend of the seal groove is provided with chamfering.
Preferably, be formed in one structure between the push rod and sprue.
Compared with prior art, the beneficial effects of the utility model are：The unmanned plane high-pressure air source launches separator, enters
Inflator and gas outlet are equipped with blowing mouth, and blowing mouth is in circular platform type, are inside plugged with the sprue of circular platform type, like this internally gas
Extruded in the presence of body tighter, it is not easy to which gas leakage, the spring top clamping that passes behind of sprue seals, relatively simple for structure, also allows for
Safeguard, cost is also than relatively low, and fixture block and neck are in order to easy to connect, and sealing ring and seal groove are then to play sealing function.
Brief description of the drawings
Fig. 1 is the utility model structure diagram.
In figure：1 inlet cylinder, 2 gas outlets, 3 blowing mouths, 4 sprues, 5 springs, 6 support frames, 7 first sealing rings, 8 push rods, 9
Fixture block, 10 necks, 11 sealing rings, 12 seal grooves, 13 second sealing rings.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
Referring to Fig. 1, the utility model provides a kind of technical scheme：A kind of unmanned plane high-pressure air source launches separator,
Including inlet cylinder 1, inlet cylinder 1 is fixed on the rear end of unmanned plane, and unmanned plane is located on guide rail, and the rear end of inlet cylinder 1 is connected with
Gas outlet 2, and gas outlet 2 is fixed on guide rail, the upper end of inlet cylinder 1 is connected with the engine of unmanned plane, and under gas outlet 2
End is connected with high-pressure air source, and this is prior art, therefore is no longer described in detail, and is opened on inlet cylinder 1 and the relative end face of gas outlet 2
Blowing mouth 3 provided with circular platform type, and the small head end of two blowing mouths 3 is relative, the circular platform type that is engaged is plugged with blowing mouth 3
Sprue 4, the inside of sprue 4 is in hollow structure, mitigates and bears a heavy burden, and motion is more flexible, and the rear side of sprue 4 is connected with by spring 5
Support frame 6.
Two support frames 6 are separately fixed on inlet cylinder 1 and gas outlet 2, and the circumference of sprue 4 is connected with the first sealing ring 7,
Two sprues 4 are equipped with push rod 8 in the middle part of relative end face, and be formed in one structure between push rod 8 and sprue 4, more solid,
It is easy to manufacture, and blowing mouth 3 is stretched out in the end of push rod 8, when mutually contradicting, will be recovered in blowing mouth 3, two phases of push rod 8
Connected between opposite end by fixture block 9 and neck 10, and fixture block 9 is in truncated cone-shaped, the upper end of gas outlet 2 is circumferentially with the sealing of annular
Ring 11, and inlet cylinder 1 is provided with annular seal groove 12 corresponding with sealing ring 11, the openend of seal groove 12 is provided with chamfering,
Facilitate insertion into, the second sealing ring 13 is equipped with the interior outer face that seal groove 12 contacts with sealing ring 11.
The unmanned plane high-pressure air source launches separator, and inlet cylinder 1 and gas outlet 2 are equipped with blowing mouth 3, and blowing mouth 3 is in
Circular platform type, the sprue 4 of circular platform type is inside plugged with, is like this internally extruded in the presence of gas tighter, it is not easy to gas leakage, block up
Block 4 passes behind the top tight sealing of spring 5, relatively simple for structure, also allows for safeguarding, cost is also than relatively low, fixture block 9 and neck 10
It is in order to easy to connect, sealing ring 11 and seal groove 12 are then to play sealing function.
While there has been shown and described that embodiment of the present utility model, for the ordinary skill in the art,
It is appreciated that these embodiments can be carried out with a variety of changes in the case where not departing from principle of the present utility model and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (4)
1. a kind of unmanned plane high-pressure air source launches separator, including inlet cylinder（1）, it is characterised in that：The inlet cylinder（1）Gu
The rear end of unmanned plane is scheduled on, and unmanned plane is located on guide rail, the inlet cylinder（1）Rear end be connected with gas outlet（2）, and outlet
Cylinder（2）It is fixed on guide rail, the inlet cylinder（1）Upper end be connected with the engine of unmanned plane, and gas outlet（2）Lower end with
High-pressure air source is connected, the inlet cylinder（1）And gas outlet（2）The blowing mouth of circular platform type is offered on relative end face（3）, and
Two blowing mouths（3）Small head end it is relative, the blowing mouth（3）Place is plugged with the sprue for the circular platform type being engaged（4）, and sprue
（4）Rear side pass through spring（5）It is connected with support frame（6）, two support frames（6）It is separately fixed at inlet cylinder（1）And gas outlet
（2）On, the sprue（4）Circumference be connected with the first sealing ring（7）, two sprues（4）It is equipped with the middle part of relative end face
Push rod（8）, and push rod（8）End stretch out blowing mouth（3）, two push rods（8）Pass through fixture block between opposite end（9）And neck
（10）Connection, and fixture block（9）In truncated cone-shaped, the gas outlet（2）Upper end be circumferentially with annular sealing ring（11）, and air inlet
Cylinder（1）It is provided with and sealing ring（11）Corresponding annular seal groove（12）, the seal groove（12）With sealing ring（11）Contact
Interior outer face on be equipped with the second sealing ring（13）.
A kind of 2. unmanned plane high-pressure air source transmitting separator according to claim 1, it is characterised in that：The sprue
（4）Inside be in hollow structure.
A kind of 3. unmanned plane high-pressure air source transmitting separator according to claim 1, it is characterised in that：The seal groove
（12）Openend be provided with chamfering.
A kind of 4. unmanned plane high-pressure air source transmitting separator according to claim 1, it is characterised in that：The push rod
（8）With sprue（4）Between be formed in one structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720342915.XU CN206766370U (en) | 2017-04-02 | 2017-04-02 | A kind of unmanned plane high-pressure air source launches separator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720342915.XU CN206766370U (en) | 2017-04-02 | 2017-04-02 | A kind of unmanned plane high-pressure air source launches separator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206766370U true CN206766370U (en) | 2017-12-19 |
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ID=60630952
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720342915.XU Active CN206766370U (en) | 2017-04-02 | 2017-04-02 | A kind of unmanned plane high-pressure air source launches separator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206766370U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112124611A (en) * | 2020-08-22 | 2020-12-25 | 西安科为实业发展有限责任公司 | Shelling and separating system and method for cylindrical jet type folding wing aircraft |
-
2017
- 2017-04-02 CN CN201720342915.XU patent/CN206766370U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112124611A (en) * | 2020-08-22 | 2020-12-25 | 西安科为实业发展有限责任公司 | Shelling and separating system and method for cylindrical jet type folding wing aircraft |
| CN112124611B (en) * | 2020-08-22 | 2023-11-28 | 西安科为实业发展有限责任公司 | Shelling separation system and method for cylindrical jet type folding wing aircraft |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: No. 0109, unit 109, No. 62, Chengyi North Street, phase III, software park, Xiamen City, Fujian Province Patentee after: Xiamen Leading Tianxun Technology Co., Ltd. Address before: 361000 Fujian city of Xiamen Province torch torch high tech Zone Park torch torch Road Plaza South Building No. 56-58 203-75 (the residence only as legal instruments of commercial subject address for service) Patentee before: Xiamen Jiuxing Tianxiang Aviation Technology Co. Ltd. |