CN209834035U - Novel launcher structure - Google Patents
Novel launcher structure Download PDFInfo
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- CN209834035U CN209834035U CN201920369849.4U CN201920369849U CN209834035U CN 209834035 U CN209834035 U CN 209834035U CN 201920369849 U CN201920369849 U CN 201920369849U CN 209834035 U CN209834035 U CN 209834035U
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Abstract
The utility model discloses a novel launcher structure, which comprises a mounting plate and a T-shaped support, wherein the T-shaped support comprises a cross rod and a long rod vertical to the middle point of the cross rod, one end of the long rod is connected to the cross rod, the other end of the long rod is also provided with a supporting device, the T-shaped support also comprises two supporting rods vertical to the plane of the cross rod and the long rod, the connecting points of the two supporting rods and the cross rod are symmetrical about the connecting point of the long rod and the cross rod, one end of the supporting rod, which is far away from the cross rod, is hinged with the mounting plate, the T-shaped support also comprises a push rod, the two ends of which are respectively hinged with the mounting plate and the supporting device, the push rod is extended or shortened under the driving of a driving device, the mounting plate comprises a rectangular frame, a reinforcing frame parallel to the, the support frame also comprises a front support frame perpendicular to the plane of the support frame.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle launches field, in particular to novel launcher structure.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
Fixed wing drones are a subclass of drones, and the wings of drones of this class have adopted a fixed design and are therefore called fixed wing drones. The fixed-wing unmanned aerial vehicle has the advantages of long endurance time, high flight efficiency, stable flight attitude, strong wind resistance, high operation efficiency and large load. The application is mainly applied to the fields of forestry and grassland monitoring, mine resource monitoring, marine environment monitoring, urban and rural junction and land utilization monitoring, water conservancy, electric power and the like. Although the unmanned aerial vehicle has the characteristics of long endurance, high efficiency and the like, the fixed-wing unmanned aerial vehicle has obvious defects in the past. Fixed wing drones primarily rely on the wind flowing over the wings to provide lift. However, the take-off and recovery problems of the fixed-wing unmanned aerial vehicle are two major difficulties which plague the fixed-wing unmanned aerial vehicle. The take-off mode of the fixed-wing unmanned aerial vehicle mainly comprises the following three modes: rocket boosters, wheeled taxis, hand-thrown versions, and the like. The rocket booster is difficult to launch and guarantee, the rocket projectile is safe to store, store and use, the launcher is needed, the preparation time is long, and the guarantee work is complex.
The existing launcher for fixed-wing unmanned aerial vehicles is simple in structure, poor in supporting effect on unmanned aerial vehicles, low in stability during launching and not beneficial to high-precision launching.
Disclosure of Invention
The utility model aims to provide a: the utility model provides a novel launcher structure, it is comparatively simple to have solved current fixed wing unmanned aerial vehicle launcher structure, and is not good to unmanned aerial vehicle's supporting effect, and stability is lower when the transmission, is unfavorable for the transmission of high accuracy.
The utility model adopts the technical scheme as follows:
a novel launcher structure comprises a mounting plate and a T-shaped support, wherein the T-shaped support comprises a cross rod and a long rod perpendicular to the middle point of the cross rod, one end of the long rod is connected to the cross rod, a supporting device is further arranged at the other end of the long rod, the T-shaped support further comprises two supporting rods perpendicular to the plane of the cross rod and the plane of the long rod, the connecting points of the two supporting rods and the cross rod are symmetrical about the connecting point of the long rod and the cross rod, one end, away from the cross rod, of each supporting rod is hinged with the mounting plate, the T-shaped support further comprises a push rod, the two ends of the push rod are respectively hinged with the mounting plate and the supporting device, the push rod extends or shortens under the driving of a driving device, the mounting plate comprises a rectangular supporting frame, a reinforcing frame parallel to a rectangular short edge is further arranged in the supporting frame, a, the tail support frame is connected to the reinforcing frame and perpendicular to the reinforcing frame on the short edge close to the reinforcing frame, the front support frame is also perpendicular to the long edge of the support frame, and the short edge of the support frame, which is not connected with the tail support frame, is located on the front support frame.
The support device is characterized by further comprising a pull rod, wherein one end of the pull rod is hinged to the support device, and the other end of the pull rod is hinged to a connecting point of the support rod and the mounting plate.
The tail support frame comprises a rectangular metal base plate, two identical trapezoidal plates, a rectangular metal plate, a long-strip-shaped metal baffle, a rectangular metal baffle and a spiral regulator, wherein the two identical trapezoidal plates are oppositely symmetrical, the long bottom edge is vertically connected to the rectangular metal base plate under the long bottom edge and is parallel to one side of the rectangular metal base plate, the short bottom edges of the two identical trapezoidal plates are connected with the rectangular metal plate, the length of the edge of the rectangular metal plate connected with the two identical trapezoidal plates is larger than that of the upper bottom edges of the two identical trapezoidal plates, the length of the other two edges of the rectangular metal plate is equal to the distance of a far point between the two identical trapezoidal plates, one edge of the rectangular metal plate is superposed with the front point connecting lines of the upper bottom edges of the two identical trapezoidal plates, the long-strip-shaped metal baffle is connected to the rectangular metal plate and the two connecting edges of the two identical trapezoidal plates, the distance between the long edge of the strip-shaped metal baffle plate and the two same trapezoidal plates is equal and is parallel to the connecting line of the front points of the upper bottom edges of the two same trapezoidal plates, the distance between the long edge of the rectangular metal baffle plate and the two same trapezoidal plates is equal, the coincidence of base back point connecting wire on one of them long limit and two the same trapezoidal boards, the waist coincidence of two minor faces and two the same trapezoidal boards, there is a screw hole at rectangle metal baffle face mid point, the screw regulator front end is the crooked rectangle metal plate of connecting from rectangle metal plate lower extreme of a rigid connecting rod front end, rigid connecting rod is by a stub bar of pivot structural connection, the stub bar passes through a pivot structural connection screw, the screw passes the screw hole at rectangular metal baffle face mid point, the screw end has a carousel of helping the rotatory regulation of screw, rectangle metal soleplate connects on the short edge of strengthening frame and braced frame.
Preceding support frame includes two cuboid metal strips, the metal sheet, the tail end horizontal pole, middle horizontal pole, two metals extend piece and two metal backing sheets, two cuboid metal strips are placed to standing upright, it is terminal by the connection of tail end horizontal pole, two cuboid metal strips of tail end horizontal pole perpendicular to, a bit is connected with middle horizontal pole in the middle section half department of this end to cuboid metal strip, the U type opening internal connection that two cuboid metal strips and middle horizontal pole formed has the metal sheet, the metal sheet inwards hollows out the part along U type opening, and hollows out the part and dwindle gradually in to U type opening, the head end outside of two cuboid metal strips is connected with two metals respectively and extends the piece, two metals extend the piece and be connected with two metal backing sheets respectively, middle horizontal pole is braced frame's minor face not connected with the tail support frame.
The two ends of the cross rod are also provided with supporting seats, and second reinforcing rods are further arranged between the supporting seats and the supporting rods close to one side of the supporting seats.
And a third reinforcing rod perpendicular to the supporting rods is also arranged between the two supporting rods.
The long rod is hinged to the supporting device through a pin shaft and fixed to the cross rod through a bolt.
Still include that one end is connected on the stock, two first stiffeners on the horizontal pole are connected to the other end.
To sum up, owing to adopted above-mentioned technical scheme, the beneficial effects of the utility model are that:
1. the utility model relates to a novel launcher structure, which solves the problems that the existing launcher is easy to deform due to the fact that the existing launcher cannot bear the impact because the fixed-wing unmanned aerial vehicle generally needs to be pushed when being launched, and the impact on the launcher is large when being launched, so that the unmanned aerial vehicle is launched;
2. the utility model relates to a novel launcher structure, because the fixed wing unmanned aerial vehicle is driven by the rocket when launching, the impact force and the vibration of launching are larger, and a plurality of groups of reinforcing rods are adopted, the novel launcher structure can deal with the vibration generated when the unmanned aerial vehicle launches, and has stable structure and high reliability;
3. the utility model relates to a novel launcher structure can make whole launcher adapt to different unmanned aerial vehicle's specification through adjusting.
Drawings
The invention will now be described, by way of example, with reference to the accompanying drawings, in which:
fig. 1 is a schematic structural diagram of the present invention;
fig. 2 is a schematic structural diagram of the present invention;
fig. 3 is a schematic structural diagram of the present invention;
fig. 4 is a schematic structural diagram of the present invention;
fig. 5 is a schematic structural diagram of the present invention;
in the figure, 1-long rod, 2-cross rod, 3-supporting device, 4-supporting seat, 5-push rod, 6-first reinforcing rod, 7-supporting rod, 8-second reinforcing rod, 10-mounting plate, 101-supporting frame, 102-tail supporting frame, 10201-rectangular metal bottom plate, 10202-two same trapezoidal plates, 10203-rectangular metal plate, 10204-long strip-shaped metal baffle, 10205-rectangular metal baffle, 10206-spiral regulator, 103-front supporting frame, 10301-rectangular metal strip, 10302-metal plate, 10303-tail end cross rod, 10304-middle cross rod, 10305-two metal extending sheets, 10306-two metal supporting sheets and 104-reinforcing frame.
Detailed Description
All of the features disclosed in this specification, or all of the steps in any method or process so disclosed, may be combined in any combination, except combinations of features and/or steps that are mutually exclusive.
The present invention will be described in detail with reference to fig. 1 to 5.
Example 1
As shown in fig. 1-5, a novel launcher structure comprises a mounting plate 10, a T-shaped support, wherein the T-shaped support comprises a cross bar 2 and a long bar 1 perpendicular to the midpoint of the cross bar 2, one end of the long bar 1 is connected to the cross bar 2, a support device 3 is further arranged at the other end of the long bar 1, two support bars 7 perpendicular to the plane of the cross bar 2 and the long bar 1 are further included, the connection points of the two support bars 7 and the cross bar 2 are symmetrical about the connection point of the long bar 1 and the cross bar 2, one end of the support bar 7 far away from the cross bar 2 is hinged to the mounting plate 10, the novel launcher structure further comprises a push rod 5, the two ends of the push rod 5 are respectively hinged to the mounting plate 10 and the support device 3, the push rod 5 is extended or shortened under the driving of a driving device 501, the mounting plate 10 comprises a rectangular support frame 101, the supporting frame structure further comprises a tail supporting frame 102 perpendicular to the plane of the supporting frame 101 and located on the supporting frame, and a front supporting frame 103 perpendicular to the plane of the supporting frame 101, wherein the tail supporting frame 102 is connected to the reinforcing frame 104 and is perpendicular to the reinforcing frame 104 on the short side close to the reinforcing frame 104, the front supporting frame 103 is also perpendicular to the long side of the supporting frame 101, and the short side, which is not connected with the tail supporting frame 102, of the supporting frame 101 is located on the front supporting frame 103.
The support device further comprises a pull rod 11, wherein one end of the pull rod 11 is hinged to the support device 3, and the other end of the pull rod 11 is hinged to a connecting point of the support rod 7 and the mounting plate 10.
The tail support frame 102 comprises a rectangular metal base plate 10201, two identical trapezoidal plates 10202, a rectangular metal plate 10203, a long strip-shaped metal baffle 10204, a rectangular metal baffle 10205 and a spiral regulator 10206, wherein the two identical trapezoidal plates 10202 are oppositely symmetrical, the long bottom edge is vertically connected to the rectangular metal base plate 10201 at the lower part, the long bottom edge is parallel to one edge of the rectangular metal base plate 10201, the short bottom edge of the two identical trapezoidal plates 10202 is connected with the rectangular metal plate 10203, the length of the edge of the rectangular metal plate 10203 connected with the two identical trapezoidal plates 10202 is more than or equal to the length of the bottom edge of the two identical trapezoidal plates 10202, the length of the other two edges of the rectangular metal plate 10203 is equal to the distance between the far points of the two identical trapezoidal plates 10202, one edge of the rectangular metal plate 10203 is superposed with the front point connecting line of the two identical trapezoidal plates 10202, the long strip-shaped metal baffle 10204 is connected to the rectangular metal, two short sides of a long strip-shaped metal baffle 10204 are connected with a rectangular metal plate 10203 and two connecting sides of two same trapezoidal plates 10202, the distance between the long side of the long strip-shaped metal baffle 10204 and the two same trapezoidal plates 10202 is equal, the short side is parallel to a front point connecting line of the upper bottom sides of the two same trapezoidal plates, the distance between the long side of the rectangular metal baffle 10205 and the two same trapezoidal plates 10202 is equal, one long side is superposed with a rear point connecting line of the upper bottom sides of the two same trapezoidal plates 10202, the two short sides are superposed with the waists of the two same trapezoidal plates 10202, a screw hole is arranged in the middle point of the plate surface of the rectangular metal baffle 10205, the front end of a screw regulator 10206 is a rigid connecting rod, the front end of the rigid connecting rod is bent and is connected with the rectangular metal plate 10203 from the lower end of the rectangular metal plate 10203, the rigid connecting rod is connected with a short rod through a pivot structure, the screw is terminated with a turn plate that assists in the rotational adjustment of the screw, and the rectangular metal base plate 10201 is attached to the reinforcing frame 104 and the short side of the support frame 101.
The front support frame 103 comprises two cuboid metal strips 10301, a metal plate 10302, a tail end cross bar 10303, a middle cross bar 10304, two metal extending sheets 10305 and two metal supporting sheets 10306, the two cuboid metal strips 10301 are arranged oppositely, the tail ends are connected by the tail end cross bar 10303, the tail end cross bar 10303 is perpendicular to the two cuboid metal strips 10301, the middle cross bar 10304 is connected from the tail ends to one point in the half part of the middle section of the cuboid metal strip 10301, the metal plate 10302 is connected inside a U-shaped opening formed by the two cuboid metal strips 10301 and the middle cross bar 10304, the metal plate 10302 is hollowed inwards along the U-shaped opening, and the hollowed part is gradually reduced towards the inside of the U-shaped opening, the outer parts of the head ends of the two cuboid metal strips 10301 are respectively connected with two metal extending sheets 10305, the two metal extending sheets 10305 are respectively connected with two metal supporting sheets 10306, the middle crossbar 10304 is a short side of the support frame 10301 that is not connected to the tail support frame 10302.
The two ends of the cross rod 2 are also provided with supporting seats 4, and second reinforcing rods 8 are further arranged between the supporting seats 4 and the supporting rods 7 close to one side of the supporting seats.
A third reinforcing rod 9 vertical to the supporting rod 7 is also arranged between the two supporting rods 7.
The long rod 1 is hinged to the supporting device 3 through a pin shaft, and the long rod 1 is fixed to the cross rod 2 through a bolt.
And the device also comprises two first reinforcing rods 6, one end of each first reinforcing rod is connected to the long rod 1, and the other end of each first reinforcing rod is connected to the cross rod 2. The utility model discloses a theory of operation/working process do:
the above description is only for the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art can be covered within the protection scope of the present invention without the changes or substitutions conceived by the inventive work within the technical scope disclosed by the present invention. Therefore, the protection scope of the present invention should be subject to the protection scope defined by the claims.
Claims (8)
1. A novel launcher structure, comprising a mounting plate (10), characterized in that: still include a T type support, T type support includes stock (1) of a horizontal pole (2) and perpendicular to horizontal pole (2) mid point, stock (1) one end is connected on horizontal pole (2), still is provided with strutting arrangement (3) on the other end of stock (1), still includes two perpendicular to horizontal pole (2) and the planar bracing piece (7) in stock (1) place, the tie point of two bracing pieces (7) and horizontal pole (2) is symmetrical about stock (1) and horizontal pole (2) tie point, the one end that horizontal pole (2) were kept away from to bracing piece (7) is articulated with mounting panel (10), still includes both ends respectively with mounting panel (10) and strutting arrangement (3) articulated push rod (5), push rod (5) are extended or shortened under drive arrangement (501), mounting panel (10) include rectangular braced frame (101), the supporting frame (101) is internally provided with a reinforcing frame (104) parallel to the rectangular short side, and further comprises a tail supporting frame (102) perpendicular to the plane of the supporting frame (101) and positioned on the supporting frame, and a front supporting frame (103) perpendicular to the plane of the supporting frame (101), wherein the tail supporting frame (102) is connected to the reinforcing frame (104) and is perpendicular to the reinforcing frame (104) on the short side close to the reinforcing frame (104), the front supporting frame (103) is also perpendicular to the long side of the supporting frame (101), and the short side of the supporting frame (101) which is not connected with the tail supporting frame (102) is positioned on the front supporting frame (103).
2. The novel launcher structure according to claim 1, wherein: the device is characterized by further comprising a pull rod (11), wherein one end of the pull rod (11) is hinged to the supporting device (3), and the other end of the pull rod (11) is hinged to a connecting point of the supporting rod (7) and the mounting plate (10).
3. The novel launcher structure according to claim 1, wherein: the tail support frame (102) comprises a rectangular metal base plate (10201), two identical trapezoidal plates (10202), a rectangular metal plate (10203), a long strip-shaped metal baffle plate (10204), a rectangular metal baffle plate (10205) and a spiral regulator (10206), the two identical trapezoidal plates (10202) are oppositely symmetrical, the long bottom edge is vertically connected to the rectangular metal base plate (10201) at the lower part, the long bottom edge is parallel to one side of the rectangular metal base plate (10201), the short bottom edges of the two identical trapezoidal plates (10202) are connected with the rectangular metal plate (10203), the length of the edge connected with the two identical trapezoidal plates (10202) of the rectangular metal plate (10203) is greater than or equal to that of the bottom edges of the two identical trapezoidal plates (10202), the length of the other two sides of the rectangular metal plate (10203) is equal to the distance of a far point between the identical trapezoidal plates (10202), and the front connecting line of one side of the rectangular metal plate coincides with the bottom edge of the two identical trapezoidal plates (10202), the rectangular metal plate (10203) is connected with a long strip-shaped metal baffle plate (10204), two short edges of the long strip-shaped metal baffle plate (10204) are connected with the rectangular metal plate (10203) and two connecting edges of two same trapezoidal plates (10202), the distance between the long edge of the long strip-shaped metal baffle plate (10204) and the two same trapezoidal plates (10202) is equal, the long edge of the long strip-shaped metal baffle plate is parallel to a front point connecting line of the bottom edges of the two same trapezoidal plates, the distance between the long edge of the rectangular metal baffle plate (10205) and the two same trapezoidal plates (10202) is equal, one long edge of the long strip-shaped metal baffle plate is superposed with a rear point connecting line of the bottom edges of the two same trapezoidal plates (10202), the two short edges of the long strip-shaped metal baffle plate and the two same trapezoidal plates (10202) are superposed, the plate surface of the rectangular metal baffle plate (10205) is provided with a screw hole, the front end of a rigid connecting rod, the hard connecting rod is connected a quarter butt by pivot structure, and the quarter butt passes through pivot structure and connects a screw, and the screw passes the screw hole of rectangle metal baffle (10205) face midpoint, and the screw end has a carousel of helping the screw rotation regulation, rectangle metal bottom plate (10201) is connected on the minor face of reinforcement frame (104) and braced frame (101).
4. The novel launcher structure according to claim 1, wherein: the front support frame (103) comprises two cuboid metal strips (10301), a metal plate (10302), a tail end cross bar (10303), a middle cross bar (10304), two metal extension sheets (10305) and two metal support sheets (10306), the two cuboid metal strips (10301) are arranged oppositely, the tail ends are connected by the tail end cross bar (10303), the tail end cross bar (10303) is perpendicular to the two cuboid metal strips (10301), the middle cross bar (10304) is connected from the tail end to one point in the middle section half part of the cuboid metal strip (10301), the metal plate (10302) is connected inside a U-shaped opening formed by the two cuboid metal strips (10301) and the middle cross bar (10304), the metal plate (10302) draws a hollow part inwards along the U-shaped opening, the hollow part is gradually reduced towards the U-shaped opening, two metal extension sheets (10305) are respectively connected outside the two cuboid metal strips (10301), the two metal extending pieces (10305) are respectively connected with two metal supporting pieces (10306), and the middle cross bar (10304) is a short side of the supporting frame (101) which is not connected with the tail supporting frame (102).
5. The novel launcher structure according to claim 1, wherein: the two ends of the cross rod (2) are also provided with supporting seats (4), and second reinforcing rods (8) are further arranged between the supporting seats (4) and the supporting rods (7) close to one side of the supporting seats.
6. The novel launcher structure according to claim 1, wherein: a third reinforcing rod (9) which is vertical to the supporting rods (7) is also arranged between the two supporting rods (7).
7. The novel launcher structure according to claim 1, wherein: the long rod (1) is hinged to the supporting device (3) through a pin shaft, and the long rod (1) is fixed to the cross rod (2) through a bolt.
8. The novel launcher structure according to claim 1, wherein: the device also comprises two first reinforcing rods (6) with one end connected to the long rod (1) and the other end connected to the cross rod (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920369849.4U CN209834035U (en) | 2019-03-22 | 2019-03-22 | Novel launcher structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920369849.4U CN209834035U (en) | 2019-03-22 | 2019-03-22 | Novel launcher structure |
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| Publication Number | Publication Date |
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| CN209834035U true CN209834035U (en) | 2019-12-24 |
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| CN201920369849.4U Active CN209834035U (en) | 2019-03-22 | 2019-03-22 | Novel launcher structure |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109850175A (en) * | 2019-03-22 | 2019-06-07 | 绵阳富莱特航空科技有限公司 | A kind of novel emission frame structure |
-
2019
- 2019-03-22 CN CN201920369849.4U patent/CN209834035U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109850175A (en) * | 2019-03-22 | 2019-06-07 | 绵阳富莱特航空科技有限公司 | A kind of novel emission frame structure |
| CN109850175B (en) * | 2019-03-22 | 2024-03-12 | 绵阳富莱特航空科技有限公司 | Novel transmitting frame structure |
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