CN110877750B - Adjustable high-adaptability field launching support for unmanned aerial vehicle - Google Patents
Adjustable high-adaptability field launching support for unmanned aerial vehicle Download PDFInfo
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- CN110877750B CN110877750B CN201911238958.3A CN201911238958A CN110877750B CN 110877750 B CN110877750 B CN 110877750B CN 201911238958 A CN201911238958 A CN 201911238958A CN 110877750 B CN110877750 B CN 110877750B
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- 230000005540 biological transmission Effects 0.000 description 3
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- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/04—Ground or aircraft-carrier-deck installations for launching aircraft
- B64F1/06—Ground or aircraft-carrier-deck installations for launching aircraft using catapults
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Abstract
The invention discloses an adjustable high-adaptability field launching support for an unmanned aerial vehicle, which comprises a launching support, wherein the launching support consists of a first folding frame and a second folding frame, the first folding frame and the second folding frame are movably connected through a folding connecting piece, a tail supporting leg is installed at the bottom end of the tail of the first folding frame, an elastic abutting piece is arranged on the tail supporting leg, and a pair of middle fixing legs are respectively installed on two sides of the bottom end of the head of the first folding frame. According to the adjustable high-adaptability field launching bracket for the unmanned aerial vehicle, the elastic abutting piece is arranged on the tail supporting leg of the launching bracket, so that the influence of the vibration of the unmanned aerial vehicle at the moment of catapult take-off on the stability of the launching bracket is effectively prevented; the universal adjusting structure and the convenient fixing structure are arranged on the middle fixing leg and the head fixing leg of the launching bracket, so that the supporting rod is fixed more simply, conveniently and firmly.
Description
Technical Field
The invention relates to the field of unmanned aerial vehicle equipment, in particular to an adjustable high-adaptability field launching bracket for an unmanned aerial vehicle.
Background
Unmanned aerial vehicle is unmanned aircraft promptly, it is the unmanned aircraft that one kind utilizes radio remote control equipment and self-contained program control device to control, unmanned aircraft can divide into many rotors and fixed wing two kinds according to the structure, wherein fixed wing unmanned aerial vehicle is owing to have flight distance long, the area of cruising is big, flight speed is fast, flight height advantage such as high, it is multi-purpose in field work, for example, forest fire tours, topography survey etc. fixed wing unmanned aerial vehicle's transmission generally all needs fixed emission support, present emission support is only ejection angle, ejection force is adjustable, can also fold the transportation, but terrain environment in the field is complicated, ordinary emission support adjusts the adaptability not enough, fixing that can not be fine, thereby influence unmanned aircraft's transmission.
Disclosure of Invention
The invention mainly aims to provide an adjustable high-adaptability field launching bracket for an unmanned aerial vehicle, which can effectively solve the problems in the background technology.
In order to achieve the purpose, the invention adopts the technical scheme that:
the utility model provides a high adaptability unmanned aerial vehicle field emission support with adjustable, is including launching the support, launch the support and constitute by folding leg and No. two folding legs, through a folding joint spare swing joint between folding leg and No. two folding legs, an afterbody supporting leg is installed to the afterbody bottom of folding leg, be equipped with an elasticity on the afterbody supporting leg and support the piece, a pair of middle fixed leg is installed respectively to the head bottom both sides of folding leg, a pair of fixed leg of head is installed respectively to the head bottom both sides of No. two folding legs, all be equipped with an universal regulation structure and a convenient fixed knot structure on middle fixed leg and the fixed leg of head.
Preferably, the main structure of the tail supporting leg is two supporting inclined rods, a pedal is fixedly connected to the bottom between the supporting inclined rods, a fixed inserting nail is vertically arranged at the bottom of each supporting inclined rod, the top ends of the supporting inclined rods are movably connected with a mounting seat through connecting pins respectively, and the mounting seats are fixedly mounted at the bottom of the first folding frame through two hexagon socket head bolts.
Preferably, elasticity supports the bottom both sides of piece and is equipped with one respectively and rotates the head to rotate head movable mounting through two and support between the down tube, support the lateral surface of down tube and install a locking knob respectively at the mounted position that corresponds the rotation head, the head of locking knob is equipped with a bolt and connects through threaded connection and stretches into in the centre bore that the rotation head tip was seted up.
Preferably, elasticity supports the piece and mainly supports tight board by telescope tube, flexible head and activity and constitutes, the rotation head sets up the bottom both sides position at the telescope tube promptly, the inside flexible chamber that is provided with of telescope tube, the inside in flexible chamber is equipped with a plurality of expanding spring, expanding spring's bottom fixed mounting is on the bottom surface in flexible chamber, and other end then fixed connection stretches into the bottom of the flexible head of flexible intracavity portion, flexible head portion stretches out flexible chamber and is provided with a mounting groove on the top, the activity supports the bottom fixed mounting of tight board and has a rotary joint, rotary joint is through an axis of rotation movable mounting in the mounting groove on flexible head top.
Preferably, the middle fixing leg and the head fixing leg are consistent in structure and are composed of a universal seat forming a universal adjusting structure and a supporting rod forming a convenient fixing structure, and the length of the head fixing leg is larger than that of the middle fixing leg.
Preferably, the universal seat mainly comprises a connecting seat, a ball sleeve, an opening sleeve and a universal ball, the connecting seat is fixedly installed at the bottom of the ball sleeve, the whole universal seat is installed on the ejection support through the connecting seat, the ball sleeve and the opening sleeve are integrally formed components, the universal ball is arranged inside the ball sleeve and the opening sleeve, and a layer of fastening lining is wrapped between the universal ball and the ball sleeve as well as between the universal ball and the opening sleeve.
Preferably, the surface of the universal ball is provided with an installation screw hole, and the top end of the support rod is fixedly installed in the installation screw hole in a threaded connection mode.
Preferably, the opening cover is equipped with a connector and No. two connectors respectively in opening part both sides, the inside fixed mounting of a connector has a connecting bolt, connecting bolt's head passes No. two connectors and connects a convenient locking handle in the outside of No. two connectors.
Preferably, a telescopic hole is formed in the bottom end of the supporting rod, a pin screw is connected to the inside of the telescopic hole in a threaded connection mode, a pointed end of an integrally formed structure is arranged at the bottom of the pin screw, a resisting spring is fixedly mounted at the top end of the telescopic hole, and the bottom end of the resisting spring is fixedly connected to the top end of the pin screw.
Preferably, the bottom outside of bracing piece is equipped with the spacing snap ring of round to the position outside cover at spacing snap ring has a rotation regulating part, rotate and to correspond on the inner wall of regulating part and seted up the spacing draw-in groove of round and block on spacing snap ring, the bottom of rotating the regulating part is fixed mounting in addition has a conical regulation head, be carved with on the inner wall of regulation head with participate in screw rod assorted internal thread.
Compared with the prior art, the invention has the following beneficial effects:
according to the adjustable high-adaptability field launching bracket for the unmanned aerial vehicle, the elastic abutting piece is arranged on the tail supporting leg of the launching bracket, and the elastic abutting piece abuts against the tail end of the launching bracket after the tail supporting leg is fixed, so that the launching bracket is effectively prevented from being driven to vibrate by vibration at the moment of launching and launching the unmanned aerial vehicle, and further the launching and launching quality is influenced; meanwhile, the universal adjusting structure consisting of the universal seat and the convenient fixing structure with the rotating adjusting piece are arranged on the middle fixing leg and the head fixing leg of the launching bracket, the angle of the bottom supporting rod can be adjusted at will by the universal seat, the optimal supporting point is convenient to find, the rotating adjusting piece can drive the pin inserting screw to insert downwards through threaded connection, the fixing mode that a transmission hand is knocked by feet is replaced, and the supporting rod is fixed more conveniently.
Drawings
Fig. 1 is a schematic diagram of the overall structure of an adjustable high-adaptability field launch bracket of an unmanned aerial vehicle;
FIG. 2 is a schematic structural diagram of a tail support leg of an adjustable high-adaptability unmanned aerial vehicle field launching bracket;
FIG. 3 is a schematic view of an installation of an elastic fastening member of an adjustable high-adaptability field launching bracket of an unmanned aerial vehicle according to the invention;
FIG. 4 is a schematic view of an internal structure of an elastic abutting member of an adjustable high-adaptability field launching bracket of an unmanned aerial vehicle according to the invention;
FIG. 5 is a schematic structural view of a universal base of an adjustable high-adaptability field launch bracket of an unmanned aerial vehicle according to the invention;
FIG. 6 is a schematic view of a pin screw mounting adjustment structure of an adjustable high-adaptability field launch bracket of an unmanned aerial vehicle according to the present invention;
fig. 7 is an enlarged view of a portion a in fig. 6.
In the figure: 1. ejecting the bracket; 2. a first folding frame; 3. a second folding frame; 4. folding the connecting piece; 5. a tail supporting leg; 6. a middle fixing leg; 7. a head fixing leg; 8. supporting the diagonal rods; 9. a foot pedal; 10. fixing the inserted nails; 11. an elastic abutting piece; 12. a movable abutting plate; 13. locking the knob; 14. a mounting seat; 15. connecting pins; 16. rotating the head; 17. a telescopic sleeve; 18. a telescopic head; 19. a rotating joint; 20. a telescoping chamber; 21. a tension spring; 22. a universal base; 23. a support bar; 24. a connecting seat; 25. a ball sleeve; 26. opening the sleeve; 27. fastening the bushing; 28. a universal ball; 29. a first connector; 30. a second connector; 31. a connecting bolt; 32. the handle is conveniently locked; 33. a telescopic hole; 34. a pin screw; 35. a tip; 36. the spring is tightly propped; 37. rotating the adjusting member; 38. an adjustment head; 39. a limit snap ring; 40. limiting clamping grooves.
Detailed Description
In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the invention easy to understand, the invention is further described with the specific embodiments.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, such as "connected," which may be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
As shown in fig. 1-7, an adjustable high-adaptability field launch support for an unmanned aerial vehicle comprises a launch support 1, wherein the launch support 1 is composed of a first folding leg 2 and a second folding leg 3, the first folding leg 2 and the second folding leg 3 are movably connected through a folding connecting piece 4, a tail supporting leg 5 is installed at the bottom end of the tail part of the first folding leg 2, an elastic abutting piece 11 is arranged on the tail supporting leg 5, a pair of middle fixing legs 6 are respectively installed on two sides of the bottom end of the head part of the first folding leg 2, a pair of head fixing legs 7 are respectively installed on two sides of the bottom end of the head part of the second folding leg 3, and a universal adjusting structure and a convenient fixing structure are respectively arranged on each of the middle fixing legs 6 and the head fixing legs 7;
the main structure of the tail supporting leg 5 is two supporting inclined rods 8, a pedal plate 9 is fixedly connected to the bottom between the supporting inclined rods 8, a fixed inserting nail 10 is vertically arranged at the bottom of each supporting inclined rod 8, the top ends of the supporting inclined rods 8 are movably connected with an installation seat 14 through connecting pins 15 respectively, and the installation seats 14 are fixedly installed at the bottom of the first folding frame 2 through two hexagon socket head bolts; two sides of the bottom of the elastic abutting piece 11 are respectively provided with a rotating head 16, the elastic abutting piece is movably arranged between the two supporting inclined rods 8 through the two rotating heads 16, the outer side surfaces of the supporting inclined rods 8 are respectively provided with a locking knob 13 at the installation position corresponding to the rotating heads 16, and the head of each locking knob 13 is provided with a bolt and is connected and extended into a central hole formed in the end part of each rotating head 16 in a threaded connection mode; the elastic abutting piece 11 mainly comprises a telescopic sleeve 17, a telescopic head 18 and a movable abutting plate 12, a rotating head 16 is arranged at two sides of the bottom of the telescopic sleeve 17, a telescopic cavity 20 is arranged inside the telescopic sleeve 17, a plurality of telescopic springs 21 are arranged inside the telescopic cavity 20, the bottoms of the telescopic springs 21 are fixedly arranged on the bottom surface of the telescopic cavity 20, the other ends of the telescopic springs are fixedly connected to the bottom of the telescopic head 18 extending into the telescopic cavity 20, the head of the telescopic head 18 extends out of the telescopic cavity 20 and is provided with a mounting groove at the top end, the bottom of the movable abutting plate 12 is fixedly provided with a rotating joint 19, and the rotating joint 19 is movably arranged in the mounting groove at the top end of the telescopic head 18 through a rotating shaft; the middle fixing leg 6 and the head fixing leg 7 have the same structure and are both composed of a universal seat 22 forming a universal adjusting structure and a supporting rod 23 forming a convenient fixing structure, but the length of the head fixing leg 7 is larger than that of the middle fixing leg 6; the universal seat 22 mainly comprises a connecting seat 24, a ball sleeve 25, an opening sleeve 26 and a universal ball 28, wherein the connecting seat 24 is fixedly arranged at the bottom of the ball sleeve 25, the whole universal seat 22 is arranged on the ejection bracket 1 through the connecting seat 24, the ball sleeve 25 and the opening sleeve 26 are integrally formed members, the universal ball 28 is arranged inside the ball sleeve 25 and the opening sleeve 26, and a layer of fastening bush 27 is further wrapped between the universal ball 28 and the ball sleeve 25 and between the universal ball 28 and the opening sleeve 26; the surface of the universal ball 28 is provided with an installation screw hole, and the top end of the support rod 23 is fixedly installed in the installation screw hole in a threaded connection mode; the two sides of the opening sleeve 26 are respectively provided with a first connector 29 and a second connector 30, a connecting bolt 31 is fixedly arranged inside the first connector 29, the head of the connecting bolt 31 penetrates through the second connector 30, and the outer side of the second connector 30 is connected with a convenient locking handle 32; a telescopic hole 33 is formed in the bottom end of the supporting rod 23, a pin screw 34 is connected to the inside of the telescopic hole 33 in a threaded connection mode, a pointed end 35 of an integrally formed structure is arranged at the bottom of the pin screw 34, a resisting spring 36 is fixedly mounted at the top end of the telescopic hole 33, and the bottom end of the resisting spring 36 is fixedly connected to the top end of the pin screw 34; the bottom outside of bracing piece 23 is equipped with spacing snap ring 39 of round to the position outside cover at spacing snap ring 39 has one to rotate regulating part 37, rotates and has seted up spacing draw-in groove 40 of round and block on spacing snap ring 39 on the inner wall of regulating part 37 correspondingly, rotates the bottom of regulating part 37 and fixed mounting has a conical regulation head 38 in addition, is carved with on the inner wall of regulation head 38 and participates in screw rod 34 assorted internal thread.
The invention relates to an adjustable high-adaptability field launching bracket of an unmanned aerial vehicle, which is characterized in that an elastic abutting piece 11 is arranged on a tail supporting leg 5 of a launching bracket 1 and is used for ensuring the stability of the launching bracket 1 at the moment of launching and taking off, and a universal adjusting structure and a convenient fixing structure are arranged on a middle fixing leg 6 and a head fixing leg 7 of the launching bracket 1 and are used for ensuring that the launching bracket 1 can be more portable and firmer when being installed and fixed; when the folding leg is actually installed and used, the tail supporting leg 5 is firstly turned out, the fixed inserting nail 10 is vertically inserted into the bottom surface by the foot pedal 9 at a preset place, the foot pedal 9 is parallel to the ground surface, then the middle fixed leg 6 is well installed to support the first folding frame 2, the connecting bolt 31 is loosened by the convenient locking handle 32, the opening sleeve 26 is loosened from the tightly wrapped universal ball 28, then the angle of the supporting rod 23 is adjusted by the universal ball 28, the most proper fixed inserting point is found, after the fixed inserting points of the two supporting rods 23 are found, the rotating adjusting piece 37 at the bottom of the supporting rod 23 is rotated by hand, the adjusting head 38 rotates along with the universal ball 28, and due to the fixation of the limited snap ring 39 between the rotating adjusting piece 37 and the supporting rod 23, the adjusting head 38 can only rotate in place, so that the inserting pin screw 34 is screwed out under the effect of threaded connection, the pointed end 35 of the head of the adjusting piece is inserted into the ground, the supporting rods 23 on the two sides are synchronously adjusted, the ejection support 1 is adjusted to be horizontal by matching with a horizontal display device at the upper end of the ejection support 1, after the two supporting rods 23 are fixed, the top end of the pin screw 34 is in a tensioned state due to the pulling of the abutting spring 36, the threaded connection between the pin screw and the adjusting head 38 is avoided from being twisted back due to the gravity above, and further the horizontal of the ejection support 1 is influenced, then the first folding frame 2 and the second folding frame 3 are opened, the head fixing leg 7 is fixed in the same way, the insertion amount of each supporting rod 23 is adjusted according to the angle of the airplane ejection, after the angle is adjusted, the elastic abutting piece 11 on the tail supporting leg 5 is turned over, the movable abutting plate 12 at the top end of the elastic abutting piece is tightly attached to the bottom surface of the first folding frame 2, and finally the elastic abutting piece 11 is fixed by using the locking knob 13, so that the installation of the ejection support 1 is completed, and then the plane can be arranged on the ejection bracket 1 by using the ejection trolley to perform ejection take-off.
The foregoing shows and describes the general principles and broad features of the present invention and advantages thereof. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the invention as claimed. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (8)
1. The utility model provides a high adaptability unmanned aerial vehicle field emission support with adjustable, its characterized in that: including launching support (1), launch support (1) and constitute by folding leg (2) and No. two folding legs (3), through a folding joint spare (4) swing joint between folding leg (2) and No. two folding legs (3), a afterbody supporting leg (5) is installed to the afterbody bottom of folding leg (2), be equipped with an elasticity on afterbody supporting leg (5) and support tight piece (11), elasticity supports the bottom both sides of tight piece (11) and is equipped with one and rotates head (16) respectively to through two rotation head (16) swing joint between two support down tube (8), the lateral surface that supports down tube (8) is corresponding the mounted position that rotates head (16) and is installed one locking knob (13) respectively, the head of locking knob (13) is equipped with a bolt and is connected through the threaded connection mode and is stretched into the centre bore that the tip of rotating head (16) was seted up, elasticity supports the tight piece (11) and mainly supports tight board (12) by telescope tube (17), flexible head (18) and activity and constitutes, rotate head (16) and set up the bottom both sides position at telescope tube (17) promptly, telescope tube (17) inside is provided with one flexible chamber (20), the inside in flexible chamber (20) is equipped with a plurality of expanding spring (21), the bottom fixed mounting of expanding spring (21) is on the bottom surface in flexible chamber (20), the other end then fixed connection stretches into the bottom of the inside flexible head (18) in flexible chamber (20), flexible head (18) head stretches out flexible chamber (20) and is provided with a mounting groove on the top, the activity supports the bottom fixed mounting of tight board (12) and has a rotary joint (19), rotary joint (19) are through a axis of rotation movable mounting in the mounting groove on flexible head (18) top, a pair of middle fixed legs (6) are installed respectively to the head bottom both sides of a folding leg (2), a pair of head fixed legs (7) are installed respectively to the head bottom both sides of No. two folding legs (3), all be equipped with an universal regulation structure and a convenient fixed knot construct on middle fixed leg (6) and head fixed leg (7).
2. The adjustable high-adaptability field launch bracket for unmanned aerial vehicles according to claim 1, wherein: the tail supporting leg (5) is characterized in that the main structure of the tail supporting leg is composed of two supporting inclined rods (8), a pedal plate (9) is fixedly connected to the bottom between the supporting inclined rods (8), a fixed inserting nail (10) is vertically arranged at the bottom of each supporting inclined rod (8), the top end of each supporting inclined rod (8) is movably connected with a mounting seat (14) through a connecting pin (15), and each mounting seat (14) is fixedly mounted at the bottom of a folding frame (2) through two hexagon socket head bolts.
3. The adjustable high-adaptability field launch bracket for unmanned aerial vehicles according to claim 1, wherein: the middle fixing leg (6) and the head fixing leg (7) are consistent in structure and composed of a universal seat (22) forming a universal adjusting structure and a supporting rod (23) forming a convenient fixing structure, and the length of the head fixing leg (7) is larger than that of the middle fixing leg (6).
4. The adjustable high-adaptability field launch bracket for unmanned aerial vehicles according to claim 3, wherein: the universal seat (22) mainly comprises a connecting seat (24), a ball sleeve (25), an opening sleeve (26) and a universal ball (28), wherein the connecting seat (24) is fixedly installed at the bottom of the ball sleeve (25), the whole universal seat (22) is installed on the ejection support (1) through the connecting seat (24), the ball sleeve (25) and the opening sleeve (26) are integrally formed, the universal ball (28) is arranged inside the ball sleeve (25) and the opening sleeve (26), and a layer of fastening bush (27) wraps the universal ball (28), the ball sleeve (25) and the opening sleeve (26) in addition.
5. The adjustable high-adaptability field launch bracket for unmanned aerial vehicles according to claim 4, wherein: the surface of the universal ball (28) is provided with an installation screw hole, and the top end of the support rod (23) is fixedly installed in the installation screw hole in a threaded connection mode.
6. The adjustable high-adaptability field launch bracket for unmanned aerial vehicles according to claim 5, wherein: opening cover (26) are equipped with a connector (29) and No. two connectors (30) respectively in opening part both sides, the inside fixed mounting of a connector (29) has a connecting bolt (31), the head of connecting bolt (31) passes No. two connectors (30) and connects a convenient locking handle (32) in the outside of No. two connectors (30).
7. The adjustable high-adaptability field launch bracket for unmanned aerial vehicles according to claim 6, wherein: the bottom end of the supporting rod (23) is internally provided with a telescopic hole (33), the inside of the telescopic hole (33) is connected with a pin screw (34) in a threaded connection mode, the bottom of the pin screw (34) is provided with a pointed end (35) of an integrally formed structure, the top end of the telescopic hole (33) is fixedly provided with a resisting spring (36), and the bottom end of the resisting spring (36) is fixedly connected to the top end of the pin screw (34).
8. The adjustable high-adaptability field launch bracket for unmanned aerial vehicles according to claim 7, wherein: the utility model discloses a bracing piece, including bracing piece (23), rotation regulating part (37), the bottom outside of bracing piece (23) is equipped with round spacing snap ring (39) to the position outside cover of spacing snap ring (39) has one, rotate and to have seted up round spacing draw-in groove (40) and block on spacing snap ring (39) on the inner wall of regulating part (37) correspondingly, the bottom of rotating regulating part (37) fixed mounting has a conical regulation head (38) in addition, be carved with on the inner wall of regulation head (38) and participate in screw rod (34) assorted internal thread.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911238958.3A CN110877750B (en) | 2019-12-06 | 2019-12-06 | Adjustable high-adaptability field launching support for unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911238958.3A CN110877750B (en) | 2019-12-06 | 2019-12-06 | Adjustable high-adaptability field launching support for unmanned aerial vehicle |
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| CN110877750A CN110877750A (en) | 2020-03-13 |
| CN110877750B true CN110877750B (en) | 2022-04-05 |
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| CN201911238958.3A Active CN110877750B (en) | 2019-12-06 | 2019-12-06 | Adjustable high-adaptability field launching support for unmanned aerial vehicle |
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| CN114476111A (en) * | 2021-04-29 | 2022-05-13 | 曾磊 | Be used for fixed wing unmanned aerial vehicle to launch with electromagnetic emission slide rail device |
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| GB2132577A (en) * | 1982-12-17 | 1984-07-11 | Nash Frazer Ltd | Launching aircraft |
| CN101654151A (en) * | 2009-09-02 | 2010-02-24 | 中兵光电科技股份有限公司 | Supporting mechanism applied unmanned aerial vehicle launching system |
| CN202449219U (en) * | 2011-12-31 | 2012-09-26 | 沈阳航天新光集团有限公司 | Unmanned aerial vehicle catapult |
| CN105711851A (en) * | 2016-01-25 | 2016-06-29 | 中国人民解放军国防科学技术大学 | Electric and light-weight catapult with multiple strands of rubber strings for small unmanned aerial vehicle |
| CN109878755A (en) * | 2019-03-29 | 2019-06-14 | 芜湖市极星航空科技有限公司 | A kind of novel unmanned plane launcher |
| CN209130438U (en) * | 2018-11-25 | 2019-07-19 | 深圳市宏润泰科技有限公司 | A kind of Flat computer support frame convenient for folding |
-
2019
- 2019-12-06 CN CN201911238958.3A patent/CN110877750B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2132577A (en) * | 1982-12-17 | 1984-07-11 | Nash Frazer Ltd | Launching aircraft |
| CN101654151A (en) * | 2009-09-02 | 2010-02-24 | 中兵光电科技股份有限公司 | Supporting mechanism applied unmanned aerial vehicle launching system |
| CN202449219U (en) * | 2011-12-31 | 2012-09-26 | 沈阳航天新光集团有限公司 | Unmanned aerial vehicle catapult |
| CN105711851A (en) * | 2016-01-25 | 2016-06-29 | 中国人民解放军国防科学技术大学 | Electric and light-weight catapult with multiple strands of rubber strings for small unmanned aerial vehicle |
| CN209130438U (en) * | 2018-11-25 | 2019-07-19 | 深圳市宏润泰科技有限公司 | A kind of Flat computer support frame convenient for folding |
| CN109878755A (en) * | 2019-03-29 | 2019-06-14 | 芜湖市极星航空科技有限公司 | A kind of novel unmanned plane launcher |
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| CN110877750A (en) | 2020-03-13 |
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