CN110143287A - Booster separation device - Google Patents
Booster separation device Download PDFInfo
- Publication number
- CN110143287A CN110143287A CN201910599271.6A CN201910599271A CN110143287A CN 110143287 A CN110143287 A CN 110143287A CN 201910599271 A CN201910599271 A CN 201910599271A CN 110143287 A CN110143287 A CN 110143287A
- Authority
- CN
- China
- Prior art keywords
- driving portion
- separation device
- fixed mechanism
- clamping
- strut
- 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.)
- Pending
Links
- 238000000926 separation method Methods 0.000 title claims abstract description 33
- 230000007246 mechanism Effects 0.000 claims abstract description 78
- 238000000034 method Methods 0.000 description 8
- 238000010276 construction Methods 0.000 description 4
- 238000009434 installation Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000008859 change Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Classifications
-
- B64D27/40—
Abstract
The present invention provides a kind of Booster separation device, Booster separation device includes: strut, and the first end of strut is connected to the body of aircraft or the bottom of wing upwards, and the second end of strut is connected to the front end of boost motor；Fixed mechanism, fixed mechanism are connected to downwards body, and boost motor is mounted on fixed mechanism；Driving portion and link mechanism, driving portion is mounted on body, and the first end of link mechanism is provided with clamping protrusion, the second end connection of driving portion and link mechanism, driving portion, which has, makes clamping protrusion connect and fix the first position of mechanism, and the second position for making clamping protrusion leave fixed mechanism；In the case where driving portion is in the second position, the first end and fixed mechanism of strut are separated from body.Wherein fixed mechanism carries multiple boost motors, avoids the nonsynchronous problem of separation caused by using independent automatically controlled disengaging boost motor, and overall mechanism is simply easy to install, light-weight convenient for carrying.
Description
Technical field
The present invention relates to Booster separation equipment technical fields, in particular to a kind of Booster separation device.
Background technique
An important mode of taking off of unmanned plane is by solid-rocket booster (hereinafter referred to as " boosting at this stage
Engine ") zero length lauuch, this just needs the thrust line of booster and the axis of unmanned plane, and there are certain angles, i.e., simultaneously
Connection installation booster.Sometimes for solution booster and unmanned plane protrusion (such as air intake duct, propeller) interference
The problem of, need more boosters used in parallel, the installation and separated in synchronization of such booster become unmanned plane
The critical issue of section of taking off.
Summary of the invention
The main purpose of the present invention is to provide a kind of Booster separation devices, to solve boost motor in the prior art point
From the nonsynchronous problem of device separation process.
To achieve the goals above, the present invention provides a kind of Booster separation device, Booster separation device includes: branch
Bar, the first end of strut are connected to the body of aircraft or the bottom of wing upwards, and the second end of strut is connected to boost motor
Front end；Fixed mechanism, fixed mechanism are connected to downwards body, and boost motor is mounted on fixed mechanism；Driving portion and link mechanism,
Driving portion is mounted on body, and the first end of link mechanism is provided with clamping protrusion, the second end company of driving portion and link mechanism
It connects, driving portion, which has, makes clamping protrusion connect and fix the first position of mechanism, and clamping protrusion is made to leave the of fixed mechanism
Two positions；In the case where driving portion is in the second position, the first end and fixed mechanism of strut are separated from body.
Further, link mechanism includes first body of rod and second body of rod, and the first end and driving portion of first body of rod drive
Connection, the first end of second body of rod is articulated on body, and clamping protrusion is set to the second end of second body of rod, and the of first body of rod
Two ends are articulated in the interlude of second body of rod.
Further, driving portion includes driving motor and the rocker arm with driving motor output end drive connection, first body of rod
First end be articulated on rocker arm.
Further, fixed mechanism includes fixed frame, in the case where driving portion is in first position, is clamped protrusion clamping
On fixed frame.
Further, multiple fixing sleeves are provided on fixed frame, boost motor is mounted in fixing sleeve correspondingly.
Further, setting clamping protrusion on fixed frame, is clamped on protrusion and is provided with fixture block, be in second in driving portion
In the case where setting, fixture block and clamping protrusion are engaged by clamping.
Further, for clamping protrusion for clamping pin, the axis for being clamped pin is parallel with the drive-connecting shaft of link mechanism.
Further, it is provided with bayonet on the side wall of separate clamping protrusion one end of fixed frame, is provided with card column on body,
In the case where driving portion is in first position, card column is connected in bayonet.
Further, card column is cylinder, and bayonet is semicircle bayonet.
Further, Booster separation device further includes spring, in the case where driving portion is in first position, spring
First end is connected to the top of fixed frame, and the second end of spring is connected to the bottom of body.
It applies the technical scheme of the present invention, after boost motor completion pushes the work forward, driving portion switches to the second operating position,
At this point, clamping protrusion is moved to the direction far from fixed mechanism, and separated with fixed mechanism, the first end of strut 40 and fixed machine
Structure is separated from body 10, and fixed mechanism and boost motor are detached from, and passes through the mechanical structures such as strut, driving portion, driving motor
Cooperating realizes the disengaging to fixed mechanism, and wherein fixed mechanism carries multiple boost motors, avoids using individually automatically controlled de-
From the nonsynchronous problem of separation caused by boost motor, and overall mechanism is simply easy to install, light-weight convenient for carrying.
Other than objects, features and advantages described above, there are also other objects, features and advantages by the present invention.
Below with reference to figure, the present invention is described in further detail.
Detailed description of the invention
The Figure of description for constituting a part of the invention is used to provide further understanding of the present invention, and of the invention shows
Examples and descriptions thereof are used to explain the present invention for meaning property, does not constitute improper limitations of the present invention.In the accompanying drawings:
Fig. 1 diagrammatically illustrates the partial sectional view that Booster separation device of the invention is mounted on carry-on embodiment；
Fig. 2 diagrammatically illustrates the enlarged drawing of B area in Fig. 1；
Fig. 3 diagrammatically illustrates the office that Booster separation device of the invention is mounted on another section of carry-on embodiment
Portion's cross-sectional view；
Fig. 4 diagrammatically illustrates the enlarged drawing of a-quadrant in Fig. 3；
Fig. 5 diagrammatically illustrates the top view of aircraft of the invention.
Wherein, the above drawings include the following reference numerals:
10, body；20, wing；30, boost motor；40, strut；41, hemisphere jut；42, recess portion；50, driving portion；51, driving electricity
Machine；52, rocker arm；60, link mechanism；61, clamping protrusion；62, first body of rod；63, second body of rod；70, fixed frame；71, fixture block；
80, card column.
Specific embodiment
It should be noted that in the absence of conflict, the feature in embodiment and embodiment in the present invention can phase
Mutually combination.The present invention will be described in detail below with reference to the accompanying drawings and embodiments.
In order to enable those skilled in the art to better understand the solution of the present invention, below in conjunction in the embodiment of the present invention
Attached drawing, technical scheme in the embodiment of the invention is clearly and completely described, it is clear that described embodiment is only
The embodiment of a part of the invention, instead of all the embodiments.Based on the embodiments of the present invention, ordinary skill people
The model that the present invention protects all should belong in member's every other embodiment obtained without making creative work
It encloses.
It should be noted that description and claims of this specification and term " first " in above-mentioned attached drawing, "
Two " etc. be to be used to distinguish similar objects, without being used to describe a particular order or precedence order.It should be understood that using in this way
Term be interchangeable under appropriate circumstances, so as to the embodiment of the present invention described herein.In addition, term " includes " and " tool
Have " and their any deformation, it is intended that cover it is non-exclusive include, for example, containing a series of steps or units
Process, method, system, product or equipment those of are not necessarily limited to be clearly listed step or unit, but may include without clear
Other step or units listing to Chu or intrinsic for these process, methods, product or equipment.
It should be noted that term used herein above is merely to describe specific embodiment, and be not intended to restricted root
According to the illustrative embodiments of the application.As used herein, unless the context clearly indicates otherwise, otherwise singular
Also it is intended to include plural form, additionally, it should be understood that, when in the present specification using term "comprising" and/or " packet
Include " when, indicate existing characteristics, step, operation, device, component and/or their combination.
As documented by background technique, an important mode of taking off of unmanned plane is helped by solid-rocket at this stage
Engine hereinafter referred to as " booster " zero length lauuch is pushed away, this just needs the thrust line of booster and the axis of unmanned plane
There are certain angles, that is, are installed in parallel booster.Sometimes for solve booster and unmanned plane protrusion such as into
The problem of air flue, propeller etc. are interfered, need more boosters used in parallel, the installation and synchronization of such booster
Separation, becomes the critical issue of unmanned plane section of taking off.
To solve the above-mentioned problems, referring to Fig. 1 to Fig. 5, the embodiment provides a kind of Booster separation device,
The Booster separation device of the present embodiment includes strut 40, fixed mechanism, driving portion 50 and link mechanism 60, wherein strut 40
First end be connected to the body 10 of aircraft upwards or the bottom of wing 20, the second end of strut 40 are connected to boost motor 30
Front end；Fixed mechanism is connected to downwards body 10, and boost motor 30 is mounted on fixed mechanism；Driving portion 50 is mounted on body 10
On, the first end of link mechanism 60 is provided with clamping protrusion 61, and driving portion 50 is connect with the second end of link mechanism 60, driving portion
50 have clamping protrusion are made 61 to connect and fix the first position of mechanism, and the seconds for making clamping protrusion 61 leave fixed mechanism
It sets；In the case where driving portion 50 is in the second position, the first end and fixed mechanism of strut 40 are separated from body 10.Its
In, the first end of strut is arranged hemisphere jut 41, and the bottom of body or wing is provided with recess portion 42, and hemisphere jut 41 is connected to recessed
In portion 42, the end of recess portion 42 is provided with spherical concave surface, and hemisphere jut 41 and spherical concave surface cooperate, and when installation, driving portion 50 is cut
First position is changed to, by clamping protrusion and strut to the active force of boost motor and fixed mechanism, boost motor is made to be maintained at body
On；After boost motor completion pushes the work forward, driving portion switches to the second operating position, at this point, clamping protrusion is to far from fixed machine
The direction of structure moves, and separates with fixed mechanism, and the first end and fixed mechanism of strut 40 are separated from body 10, fixed machine
Structure and boost motor are detached from, and by the cooperating of the mechanical structures such as strut 40, driving portion, driving motor, are realized to fixed mechanism
Disengaging, wherein fixed mechanism carries multiple boost motors, avoids using separation difference caused by independent automatically controlled disengagings boost motor
The problem of step, and overall mechanism is simply easy to install, it is light-weight convenient for carrying.
Shown in Figure 2, specifically, the link mechanism 60 in the present embodiment includes first body of rod 62 and second body of rod
63, the first end and driving portion 50 of first body of rod 62 are drivingly connected, and the first end of second body of rod 63 is articulated on body 10, are clamped
Protrusion 61 is set to the second end of second body of rod 63, and the second end of first body of rod 62 is articulated in the interlude of second body of rod 63,
In, interlude refers to the region between the first end and second end of second body of rod.
Wherein, the driving portion 50 in the present embodiment includes driving motor 51 and is drivingly connected with 51 output end of driving motor
The first end of Rocker arm 52, first body of rod 62 is articulated on Rocker arm 52, and after boost motor completion pushes the work forward, driving motor band shakes
Arm rotation, clamping protrusion is moved to the direction far from fixed mechanism, and is separated with fixed mechanism, certainly, the drive in the present embodiment
Dynamic portion can also be other driving structures, such as pneumatic mechanism.
Fixed mechanism in the present embodiment includes fixed frame 70, in the case where driving portion 50 is in first position, clamping
Protrusion 61 is connected on fixed frame 70.Multiple fixing sleeves are provided on fixed frame 70 in the present embodiment, boost motor 30 1 is a pair of
It is mounted in fixing sleeve with answering, after boost motor completion pushes the work forward, driving portion switches to the second operating position, at this point, clamping
Protrusion is moved to the direction far from fixed mechanism, and is separated with fixed mechanism, the equal slave of first end and fixed mechanism of strut 40
It being separated on body 10, fixed mechanism and boost motor are detached from, by the cooperating of the mechanical structures such as strut, driving portion, driving motor,
Realize the separated in synchronization of multiple boost motors.
Setting clamping protrusion on fixed frame 70 in the present embodiment, is clamped on protrusion and is provided with fixture block 71, in driving portion 50
In the case where the second position, fixture block 71 and clamping protrusion 61 are engaged by clamping, and specially fixture block 71 rides in clamping protrusion 61.
In order to keep the clamping of clamping protrusion more stable, the clamping protrusion 61 in the present embodiment is clamping pin, is clamped pin
Axis is parallel with the drive-connecting shaft of link mechanism 60.
It is shown in Figure 2, card is provided on the side wall of raised 61 one end of the separate clamping of the fixed frame 70 in the present embodiment
Mouthful, it is provided with card column 80 on body 10, in the case where driving portion 50 is in first position, card column 80 is connected in bayonet.?
In the case that driving portion 50 is in the second position, clamping protrusion is moved to the direction far from fixed mechanism, and is divided with fixed mechanism
From fixed frame is overturn by self gravity, is clamped bayonet no longer with card column, realizes the disengaging to fixed mechanism.
In order to keep the separation process of fixed mechanism more smooth, the card column 80 in the present embodiment is cylinder, and bayonet is semicircle
Shape bayonet.
In order to enable fixed mechanism to be quickly detached from fuselage, being rapidly separated for boost motor is realized, helping in the present embodiment
Thruster separator further includes spring, and in the case where driving portion 50 is in first position, the first end of spring is connected to fixation
The top of frame 70, the second end of spring are connected to the bottom of body 10.
It can be seen from the above description that the above embodiments of the present invention realized the following chievements:.
After boost motor completion pushes the work forward, driving portion switches to the second operating position, at this point, clamping protrusion is to far from solid
Determine the direction movement of mechanism, and separated with fixed mechanism, the first end and fixed mechanism of strut are separated from body, fixed machine
Structure and boost motor are detached from, and by the cooperating of the mechanical structures such as strut, driving portion, driving motor, are realized to fixed mechanism
It is detached from, wherein fixed mechanism carries multiple boost motors, avoids asynchronous using separation caused by independent automatically controlled disengaging boost motor
The problem of, and overall mechanism is simply easy to install, it is light-weight convenient for carrying.
Unless specifically stated otherwise, positioned opposite, the digital table of the component and step that otherwise illustrate in these embodiments
It is not limited the scope of the invention up to formula and numerical value.Simultaneously, it should be appreciated that for ease of description, each portion shown in attached drawing
The size divided not is to draw according to actual proportionate relationship.For technology, side known to person of ordinary skill in the relevant
Method and equipment may be not discussed in detail, but in the appropriate case, and the technology, method and apparatus should be considered as authorizing explanation
A part of book.In shown here and discussion all examples, any occurrence should be construed as merely illustratively, and
Not by way of limitation.Therefore, the other examples of exemplary embodiment can have different values.It should also be noted that similar label
Similar terms are indicated in following attached drawing with letter, therefore, once it is defined in a certain Xiang Yi attached drawing, then subsequent attached
It does not need that it is further discussed in figure.
For ease of description, spatially relative term can be used herein, as " ... on ", " ... top ",
" ... upper surface ", " above " etc., for describing such as a device shown in the figure or feature and other devices or spy
The spatial relation of sign.It should be understood that spatially relative term is intended to comprising the orientation in addition to device described in figure
Except different direction in use or operation.For example, being described as if the device in attached drawing is squeezed " in other devices
It will be positioned as " under other devices or construction after part or construction top " or the device of " on other devices or construction "
Side " or " under other devices or construction ".Thus, exemplary term " ... top " may include " ... top " and
" in ... lower section " two kinds of orientation.The device can also be positioned with other different modes and (is rotated by 90 ° or in other orientation), and
And respective explanations are made to the opposite description in space used herein above.
In the description of the present invention, it is to be understood that, the noun of locality such as " front, rear, top, and bottom, left and right ", " it is laterally, vertical,
Vertically, orientation or positional relationship indicated by level " and " top, bottom " etc. is normally based on orientation or position shown in the drawings and closes
System, is merely for convenience of description of the present invention and simplification of the description, in the absence of explanation to the contrary, these nouns of locality do not indicate that
It must have a particular orientation or be constructed and operated in a specific orientation with the device or element for implying signified, therefore cannot manage
Solution is limiting the scope of the invention；The noun of locality " inside and outside " refers to inside and outside the profile relative to each component itself.
The foregoing is only a preferred embodiment of the present invention, is not intended to restrict the invention, for the skill of this field
For art personnel, the invention may be variously modified and varied.All within the spirits and principles of the present invention, made any to repair
Change, equivalent replacement, improvement etc., should all be included in the protection scope of the present invention.
Claims (10)
1. a kind of Booster separation device, which is characterized in that the Booster separation device includes:
Strut (40), the first end of the strut (40) are connected to the body (10) of aircraft or the bottom of wing (20) upwards,
The second end of the strut (40) is connected to the front end of boost motor (30)；
Fixed mechanism, the fixed mechanism are connected to downwards the body (10), and the boost motor (30) is mounted on the fixation
In mechanism；
Driving portion (50) and link mechanism (60), the driving portion (50) are mounted on the body (10), the link mechanism
(60) first end is provided with clamping protrusion (61), and the driving portion (50) connect with the second end of the link mechanism (60),
The driving portion (50), which has, makes the clamping raised (61) be clamped the first position of the fixed mechanism, and makes the clamping
Raised (61) leave the second position of the fixed mechanism；In the case where the driving portion (50) is in the second position,
The first end of the strut (40) and the fixed mechanism are separated from the body (10).
2. Booster separation device according to claim 1, which is characterized in that the link mechanism (60) includes the first bar
Body (62) and second body of rod (63), the first end of first body of rod (62) and the driving portion (50) are drivingly connected, and described the
The first end of bipole body (63) is articulated on the body (10), and the clamping raised (61) is set to second body of rod (63)
Second end, the second end of first body of rod (62) is articulated in the interlude of second body of rod (63).
3. Booster separation device according to claim 2, which is characterized in that the driving portion (50) includes driving motor
(51) and with the driving motor (51) output end the rocker arm (52) being drivingly connected, the first end pivot joint of first body of rod (62)
On the rocker arm (52).
4. Booster separation device according to claim 1, which is characterized in that the fixed mechanism includes fixed frame
(70), in the case where the driving portion (50) is in the first position, the clamping raised (61) is connected to the fixation
On frame (70).
5. Booster separation device according to claim 4, which is characterized in that be provided on the fixed frame (70) multiple
Fixing sleeve, the boost motor (30) are mounted on correspondingly in the fixing sleeve.
6. Booster separation device according to claim 4, which is characterized in that setting clamping is convex on the fixed frame (70)
Portion is provided with fixture block (71) on the clamping protrusion, described in the case where the driving portion (50) is in the second position
Fixture block (71) and the clamping raised (61) are engaged by clamping.
7. Booster separation device according to claim 2, which is characterized in that the clamping raised (61) is clamping pin,
The axis of the clamping pin is parallel with the drive-connecting shaft of the link mechanism (60).
8. Booster separation device according to claim 4, which is characterized in that the separate card of the fixed frame (70)
It connects and is provided with bayonet on the side wall of raised (61) one end, card column (80) are provided on the body (10), in the driving portion
(50) in the case where being in the first position, the card column (80) is connected in the bayonet.
9. Booster separation device according to claim 8, which is characterized in that the card column (80) is cylinder, the card
Mouth is semicircle bayonet.
10. Booster separation device according to claim 4, which is characterized in that the Booster separation device further includes
Spring, in the case where the driving portion (50) is in the first position, the first end of the spring is connected to the fixation
The top of frame (70), the second end of the spring are connected to the bottom of the body (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910599271.6A CN110143287A (en) | 2019-07-04 | 2019-07-04 | Booster separation device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910599271.6A CN110143287A (en) | 2019-07-04 | 2019-07-04 | Booster separation device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110143287A true CN110143287A (en) | 2019-08-20 |
Family
ID=67596943
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910599271.6A Pending CN110143287A (en) | 2019-07-04 | 2019-07-04 | Booster separation device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110143287A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113460320A (en) * | 2020-03-31 | 2021-10-01 | 海鹰航空通用装备有限责任公司 | Booster separating mechanism for unmanned aerial vehicle and method for using booster separating mechanism |
| CN114248946A (en) * | 2020-09-22 | 2022-03-29 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle helps and separating mechanism |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106688325B (en) * | 2005-12-28 | 2011-03-30 | 中国航天科技集团公司第十一研究院 | Unmanned plane booster drop-off device |
| CN204279987U (en) * | 2014-11-27 | 2015-04-22 | 江西洪都航空工业集团有限责任公司 | A kind of aircraft Booster separation mechanism |
| CN204452941U (en) * | 2014-12-30 | 2015-07-08 | 王洪洋 | A kind of simple and fast delivery device for model plane load-carrying air-drop |
| CN205918517U (en) * | 2016-05-12 | 2017-02-01 | 西安航天动力技术研究所 | Big airborne solid rocket engine aircraft climb assisting unit |
| CN107933946A (en) * | 2017-12-11 | 2018-04-20 | 浙江大学 | Unmanned plane two point form rocket assist emitter and its method |
| CN207292430U (en) * | 2017-06-28 | 2018-05-01 | 中国航天空气动力技术研究院 | A kind of throwing mechanism of the big quality weight/HP ratio of binary machine |
| CN108408076A (en) * | 2018-01-30 | 2018-08-17 | 南京航天猎鹰飞行器技术有限公司 | A kind of unmanned plane is fixed with booster rocket and is oriented to separating mechanism |
| CN109703772A (en) * | 2018-12-28 | 2019-05-03 | 西北工业大学 | A kind of unmanned plane rocket dropping mechanism of rear-mounted power arrangement |
| CN210284626U (en) * | 2019-07-04 | 2020-04-10 | 哈工大机器人（岳阳）军民融合研究院 | Booster separator |
-
2019
- 2019-07-04 CN CN201910599271.6A patent/CN110143287A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106688325B (en) * | 2005-12-28 | 2011-03-30 | 中国航天科技集团公司第十一研究院 | Unmanned plane booster drop-off device |
| CN204279987U (en) * | 2014-11-27 | 2015-04-22 | 江西洪都航空工业集团有限责任公司 | A kind of aircraft Booster separation mechanism |
| CN204452941U (en) * | 2014-12-30 | 2015-07-08 | 王洪洋 | A kind of simple and fast delivery device for model plane load-carrying air-drop |
| CN205918517U (en) * | 2016-05-12 | 2017-02-01 | 西安航天动力技术研究所 | Big airborne solid rocket engine aircraft climb assisting unit |
| CN207292430U (en) * | 2017-06-28 | 2018-05-01 | 中国航天空气动力技术研究院 | A kind of throwing mechanism of the big quality weight/HP ratio of binary machine |
| CN107933946A (en) * | 2017-12-11 | 2018-04-20 | 浙江大学 | Unmanned plane two point form rocket assist emitter and its method |
| CN108408076A (en) * | 2018-01-30 | 2018-08-17 | 南京航天猎鹰飞行器技术有限公司 | A kind of unmanned plane is fixed with booster rocket and is oriented to separating mechanism |
| CN109703772A (en) * | 2018-12-28 | 2019-05-03 | 西北工业大学 | A kind of unmanned plane rocket dropping mechanism of rear-mounted power arrangement |
| CN210284626U (en) * | 2019-07-04 | 2020-04-10 | 哈工大机器人（岳阳）军民融合研究院 | Booster separator |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113460320A (en) * | 2020-03-31 | 2021-10-01 | 海鹰航空通用装备有限责任公司 | Booster separating mechanism for unmanned aerial vehicle and method for using booster separating mechanism |
| CN114248946A (en) * | 2020-09-22 | 2022-03-29 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle helps and separating mechanism |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN110143287A (en) | Booster separation device | |
| CN104656203B (en) | Optical communication connector | |
| CN207997972U (en) | A kind of foldable unmanned plane | |
| CN105857571A (en) | Unmanned aerial vehicle with multi-vehicle-arm synchronous folding mechanism | |
| CN109592025A (en) | More rotor unmanned aircrafts, external member and its foldable rotor assemblies | |
| CN105539827A (en) | Arm folding device of multi-axial air vehicle | |
| CN110466750A (en) | A kind of Portable vertical landing scouting monitoring unmanned plane | |
| CN109016343A (en) | Manipulator, robot and mold insert equipment | |
| CN104691736A (en) | Fixed-wing unmanned aerial vehicle | |
| CN112896497A (en) | Unmanned helicopter | |
| CN210284626U (en) | Booster separator | |
| WO2019132285A1 (en) | Tilting blade assembly for drone | |
| CN107542704B (en) | Fan subassembly and have its air conditioner | |
| CN105945910A (en) | Clamping mechanical arm of unmanned aerial vehicle | |
| CN210191814U (en) | Unmanned aerial vehicle | |
| CN112408179A (en) | Foldable telescopic combined hoisting device | |
| CN210101967U (en) | Automatic folding device of unmanned aerial vehicle horn | |
| CN109895987B (en) | Rudder folding device for ocean robot | |
| CN205971816U (en) | Scaffold fixing structure | |
| CN205673830U (en) | A kind of SC adapter automatic assembling device | |
| CN209192224U (en) | A kind of easy-to-dismount propeller of unmanned plane | |
| CN109941450A (en) | A kind of multi-functional unmanned flight's device | |
| CN208963327U (en) | Unmanned plane | |
| CN210083545U (en) | Aerodynamic test glider | |
| CN112977813A (en) | Tiltable wing and unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20220128 Address after: 414000 Harbin Institute of technology robot (Yueyang) military civilian integration innovation center (Dongfeng Village, Yunxin Avenue), Chenglingji new port area, Yueyang City, Hunan Province Applicant after: Hunan Hagong Lanhang Technology Co.,Ltd. Address before: 3 / F, Xindeng incubator office building, civil military integration industrial park, Chenglingji new port area, Yueyang City, Hunan Province, 414000 Applicant before: HARBIN INSTITUTE OF TECHNOLOGY ROBOT (YUEYANG) MILITARY AND CIVILIAN INTEGRATION Research Institute |