CN209938929U - Helicopter belly convenient to carry on multiple equipment simultaneously - Google Patents
Helicopter belly convenient to carry on multiple equipment simultaneously Download PDFInfo
- Publication number
- CN209938929U CN209938929U CN201920237678.XU CN201920237678U CN209938929U CN 209938929 U CN209938929 U CN 209938929U CN 201920237678 U CN201920237678 U CN 201920237678U CN 209938929 U CN209938929 U CN 209938929U
- Authority
- CN
- China
- Prior art keywords
- fixedly connected
- supporting
- plate
- belly
- helicopter
- 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.)
- Expired - Fee Related
Links
Images
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a helicopter ventral convenient to carry on multiple equipment simultaneously, including the ventral body, the top of ventral body is provided with the flight paddle leaf, the bottom fixedly connected with landing leg of ventral body, the bottom symmetry of ventral body is provided with two backup pads, the bottom fixedly connected with link block of backup pad, link block's surface sliding connection has the supporting seat. The utility model discloses a machine abdomen body, link block, a supporting seat, first buffer spring, support slide bar, support sliding sleeve, fixed plate, first mounting panel, electric putter, driving motor, threaded rod, movable plate, bracing piece and the mutually supporting of second mounting panel for can install different equipment on first mounting panel and the second mounting panel, be convenient for carry on multiple equipment simultaneously, need not to return to the journey and change equipment, avoid because change equipment causes the damage of organism and equipment, reduce the waste to human cost and time.
Description
Technical Field
The utility model relates to a helicopter technical field specifically is a helicopter ventral convenient to carry on multiple equipment simultaneously.
Background
Helicopter flight power is primarily derived from the rotation of the blades of the rotor system. During helicopter flight, the blades of the rotor system rotate about a rotor shaft.
The ventral of helicopter often needs to carry on equipment, but the current helicopter ventral can't carry on multiple equipment simultaneously, all needs to return to the air as required at every turn and changes equipment, causes the damage of organism and equipment easily on the one hand, and another conveniently changes equipment repeatedly and causes the waste of human cost and time.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a helicopter ventral convenient to carry on multiple equipment simultaneously has the advantage of carrying on multiple equipment simultaneously, has solved the problem that current helicopter ventral can't carry on multiple equipment simultaneously.
In order to achieve the above object, the utility model provides a following technical scheme: a helicopter belly convenient for simultaneously carrying various devices comprises a belly body, wherein the top of the belly body is provided with a flight blade, the bottom of the belly body is fixedly connected with landing legs, the bottom of the belly body is symmetrically provided with two supporting plates, the bottoms of the supporting plates are fixedly connected with a connecting slide block, the surface of the connecting slide block is slidably connected with a supporting seat, the surface of the supporting plate is sleeved with a first buffer spring positioned inside the supporting seat, the connecting slide block is fixedly connected with the top of the inner wall of the supporting seat through the first buffer spring, the two supporting seats are fixedly connected through a supporting slide rod, the surface of the supporting slide rod is slidably connected with two supporting slide sleeves, the bottoms of the supporting slide sleeves are fixedly connected with a fixing plate, the bottoms of the two supporting seats are fixedly connected through a first mounting plate, and the bottom of the first mounting plate is provided with a, the bottom of the fixed plate is fixedly connected with electric push rods which are positioned on the left side and the right side of the through groove, the bottom of the fixed plate penetrates through the through groove and extends to the lower side of the through groove, a limiting plate is fixedly connected with the bottom of the fixed plate, one side of the electric push rods, which is close to the fixed plate, is fixedly connected with the fixed plate positioned on the same side, two storage shells are symmetrically arranged at the bottom of the belly body, one sides of the storage shells, which are far away from the supporting seat, are provided with through holes, a partition plate is fixedly connected onto the inner wall of each storage shell, one side of the inner wall of each storage shell, which is close to the supporting seat, is fixedly connected with a driving motor, a threaded rod is fixedly connected onto the output shaft of the driving motor, the surface of the, the left side fixedly connected with second mounting panel of bracing piece, the left side symmetry of second mounting panel begins to have two mounting holes.
Preferably, the left side and the right side of the landing leg are both fixedly connected with cushions.
Preferably, a second buffer spring is sleeved on the surface of the support sliding rod and located between the two support sliding sleeves, and the two support sliding sleeves are fixedly connected through the second buffer spring.
Preferably, one side of the electric push rod, which is far away from the fixed plate, is fixedly connected with a reinforcing plate, and the top of the reinforcing plate is fixedly connected with the mounting plate.
Preferably, the bearing is fixedly connected in the groove on one side of the partition plate close to the threaded rod, and the inner wall of the inner ring of the bearing is fixedly connected with the threaded rod.
Preferably, the bottom of the inner wall of the storage shell is provided with a supporting sliding groove corresponding to the position of the moving plate, the inner wall of the supporting sliding groove is fixedly connected with a supporting sliding block corresponding to the fixed position of the moving plate, and the top of the supporting sliding block penetrates through the supporting sliding groove and extends to the outside of the supporting sliding block to be fixedly connected with the bottom of the moving plate.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses a machine abdomen body, link block, a supporting seat, first buffer spring, support slide bar, support sliding sleeve, fixed plate, first mounting panel, electric putter, driving motor, threaded rod, movable plate, bracing piece and the mutually supporting of second mounting panel for can install different equipment on first mounting panel and the second mounting panel, be convenient for carry on multiple equipment simultaneously, need not to return to the journey and change equipment, avoid because change equipment causes the damage of organism and equipment, reduce the waste to human cost and time.
2. The utility model discloses a set up the blotter, played the effect of the clash power of descending landing leg when buffering descending, through setting up second buffer spring, played two support sliding sleeve of buffering and removed and the effect of the vibrations that produce, through setting up the gusset plate, played the effect of being connected between reinforcement electric putter and the first mounting panel, through setting up the bearing, played the effect of supporting threaded rod, through setting up support spout and support slider, played the effect of supporting the movable plate.
Drawings
FIG. 1 is a structural section view in elevation of the present invention;
fig. 2 is a partial enlarged view of a-a in fig. 1 according to the present invention.
In the figure: the aircraft comprises a web body 1, flight blades 2, landing legs 3, supporting plates 4, connecting sliders 5, supporting seats 6, first buffer springs 7, supporting slide rods 8, supporting sliding sleeves 9, fixing plates 10, first mounting plates 11, through grooves 12, electric push rods 13, limiting plates 14, storage shells 15, through holes 16, partition plates 17, driving motors 18, threaded rods 19, moving plates 20, supporting rods 21, second mounting plates 22, mounting holes 23, cushion pads 24, second buffer springs 25, reinforcing plates 26, bearings 27, supporting chutes 28 and supporting sliders 29.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-2, a helicopter belly convenient for carrying various devices simultaneously comprises a belly body 1, a flight blade 2 is arranged at the top of the belly body 1, landing legs 3 are fixedly connected to the bottom of the belly body 1, cushions 24 are fixedly connected to the left and right sides of the bottom of the landing legs 3, the cushions 24 are arranged to play a role in buffering the impact force of the landing legs 3 during landing, two support plates 4 are symmetrically arranged at the bottom of the belly body 1, a connecting slide block 5 is fixedly connected to the bottom of each support plate 4, a support seat 6 is slidably connected to the surface of each connecting slide block 5, the connecting relationship between each support plate 4 and each support seat 6 is movable, a first buffer spring 7 is sleeved on the surface of each support plate 4 and positioned inside each support seat 6, and the connecting slide block 5 is fixedly connected to the top of the inner wall of each support seat 6 through the first buffer spring, the first buffer spring 7 is arranged to play a role of buffering the shaking of the supporting seat 6, the two supporting seats 6 are fixedly connected through the supporting slide rod 8, the surface of the supporting slide rod 8 is slidably connected with two supporting slide sleeves 9, the surface of the supporting slide rod 8 is sleeved with the second buffer spring 25 at a position between the two supporting slide sleeves 9, the two supporting slide sleeves 9 are fixedly connected through the second buffer spring 25, the second buffer spring 25 is arranged to play a role of buffering the vibration generated by the movement of the two supporting slide sleeves 9, the bottom of the supporting slide sleeve 9 is fixedly connected with the fixing plate 10, the bottoms of the two supporting seats 6 are fixedly connected through the first mounting plate 11, the bottom of the first mounting plate 11 is provided with the through groove 12, the bottom of the fixing plate 10 is fixedly connected with the electric push rod 13 at the left side and the right side of the through groove 12, and the reinforcing plate 26 is fixedly connected to one side, the top of the reinforcing plate 26 is fixedly connected with the first mounting plate 11, the reinforcing plate 26 is arranged to play a role of reinforcing the connection between the electric push rod 13 and the first mounting plate 11, the bottom of the fixing plate 10 penetrates through the through groove 12 and extends to the lower part of the through groove 12, the fixing plate 10 is connected to the inner wall of the through groove 12 in a sliding manner, the bottom of the fixing plate 10 is fixedly connected with the limiting plate 14, one side of the electric push rod 13 close to the fixing plate 10 is fixedly connected with the fixing plate 10 positioned at the same side, the bottom of the belly body 1 is symmetrically provided with two storage shells 15, one side of the storage shells 15 far away from the supporting seat 6 is provided with a through hole 16, the inner wall of the storage shells 15 is fixedly connected with a partition plate 17, one side of the inner wall of the storage shells 15 close to the supporting seat 6 is fixedly connected with a driving motor, the inner wall of the inner ring of the bearing 27 is fixedly connected with the threaded rod 19, the bearing 27 is arranged to play a role of supporting the threaded rod 19, the surface of the threaded rod 19 is in threaded connection with the movable plate 20, the bottom of the inner wall of the storage shell 15 is provided with a supporting sliding groove 28 corresponding to the position of the movable plate 20, the inner wall of the supporting sliding groove 28 is fixedly connected with a supporting sliding block 29 corresponding to the position of the movable plate 20, the top of the supporting sliding block 29 penetrates through the supporting sliding groove 28 and extends to the outside of the supporting sliding block and is fixedly connected with the bottom of the movable plate 20, the supporting sliding groove 28 and the supporting sliding block 29 are arranged to play a role of supporting the movable plate 20, one side of the movable plate 20, which is far away from the supporting seat 6, is fixedly connected with the supporting rod 21, one side of the supporting rod 21, which is far away from, the left side symmetry of second mounting panel 22 begins to have two mounting holes 23, through machine abdomen body 1, link block 5, supporting seat 6, first buffer spring 7, support slide bar 8, support sliding sleeve 9, fixed plate 10, first mounting panel 11, electric putter 13, driving motor 18, threaded rod 19, movable plate 20, mutually supporting of bracing piece 21 and second mounting panel 22, make and to install different equipment on first mounting panel 11 and the second mounting panel 22, be convenient for carry on multiple equipment simultaneously, need not to return to the journey and change equipment, avoid causing the damage of organism and equipment because change equipment, reduce the waste to human cost and time.
During the use, in installing camera or other check out test set to second mounting panel 22, mounting hole 23 has been seted up on the second mounting panel 22, easy to assemble, when need moving out storage casing 15 with camera or check out test set, start driving motor 18, driving motor 18 drives threaded rod 19 and rotates, the external screw thread of threaded rod 19 orders about movable plate 20 and moves to opening 16 play, movable plate 20 passes through bracing piece 21 and drives camera on the second mounting panel 22 and pass and move out storage casing 15 behind opening 16, alright use, fix great equipment through two fixed plates 10, limiting plate 14 supports the bottom of equipment, start electric putter 13, electric putter 13 promotes fixed plate 10, two fixed plates 10 press from both sides tight equipment, it is fixed to accomplish.
In summary, the following steps: this helicopter machine belly convenient to carry on multiple equipment simultaneously has solved the unable problem of carrying on multiple equipment simultaneously of current helicopter machine belly through mutually supporting of machine belly body 1, link block 5, supporting seat 6, first buffer spring 7, support slide bar 8, support sliding sleeve 9, fixed plate 10, first mounting panel 11, electric putter 13, driving motor 18, threaded rod 19, movable plate 20, bracing piece 21 and second mounting panel 22.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a helicopter ventral convenient to carry on multiple equipment simultaneously, includes ventral body (1), its characterized in that: the aircraft wing is characterized in that a flight blade (2) is arranged at the top of the aircraft belly body (1), landing legs (3) are fixedly connected to the bottom of the aircraft belly body (1), two supporting plates (4) are symmetrically arranged at the bottom of the aircraft belly body (1), a connecting slide block (5) is fixedly connected to the bottom of each supporting plate (4), a supporting seat (6) is connected to the surface of each connecting slide block (5) in a sliding manner, a first buffer spring (7) is sleeved on the surface of each supporting plate (4) and located inside each supporting seat (6), the connecting slide block (5) is fixedly connected with the top of the inner wall of each supporting seat (6) through the first buffer spring (7), the two supporting seats (6) are fixedly connected through supporting slide rods (8), the surface of each supporting slide rod (8) is connected with two supporting slide sleeves (9), and a fixing plate (10) is fixedly connected to the bottom of each, the bottom of two supporting seats (6) is fixedly connected through a first mounting plate (11), the bottom of the first mounting plate (11) is provided with a through groove (12), the bottom of a fixing plate (10) is positioned at the left side and the right side of the through groove (12) and is fixedly connected with an electric push rod (13), the bottom of the fixing plate (10) penetrates through the through groove (12) and extends to the lower side of the through groove, the bottom of the fixing plate (10) is fixedly connected with a limiting plate (14), one side of the electric push rod (13) close to the fixing plate (10) is fixedly connected with the fixing plate (10) positioned at the same side, the bottom of the belly body (1) is symmetrically provided with two storage shells (15), one side of the storage shells (15) far away from the supporting seats (6) is provided with a through opening (16), the inner wall of the storage shells (15) is fixedly connected with a partition plate (17), one side of the inner wall of the storage, fixedly connected with threaded rod (19) on the output shaft of driving motor (18), the surperficial threaded connection of threaded rod (19) has movable plate (20), one side fixedly connected with bracing piece (21) of supporting seat (6) are kept away from in movable plate (20), one side that movable plate (20) were kept away from in bracing piece (21) runs through baffle (17) and extends to its left side, the left side fixedly connected with second mounting panel (22) of bracing piece (21), the left side symmetry of second mounting panel (22) begins to have two mounting holes (23).
2. A helicopter belly for facilitating the simultaneous carrying of multiple devices according to claim 1, wherein: the left side and the right side of the bottom of the landing leg (3) are fixedly connected with cushion pads (24).
3. A helicopter belly for facilitating the simultaneous carrying of multiple devices according to claim 1, wherein: the surface of the support sliding rod (8) is sleeved with a second buffer spring (25) at a position between the two support sliding sleeves (9), and the two support sliding sleeves (9) are fixedly connected through the second buffer spring (25).
4. A helicopter belly for facilitating the simultaneous carrying of multiple devices according to claim 1, wherein: one side of the electric push rod (13) far away from the fixing plate (10) is fixedly connected with a reinforcing plate (26), and the top of the reinforcing plate (26) is fixedly connected with the first mounting plate (11).
5. A helicopter belly for facilitating the simultaneous carrying of multiple devices according to claim 1, wherein: the baffle (17) are close to the recess of threaded rod (19) one side in fixedly connected with bearing (27), the inner wall and the threaded rod (19) fixed connection of bearing (27) inner ring.
6. A helicopter belly for facilitating the simultaneous carrying of multiple devices according to claim 1, wherein: support spout (28) have been seted up to the position that the bottom of storage casing (15) inner wall corresponds movable plate (20), correspond the fixed position that movable plate (20) decided on the inner wall of support spout (28) and support slider (29), the top of supporting slider (29) runs through support spout (28) and extends to the bottom fixed connection of its outside and movable plate (20).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920237678.XU CN209938929U (en) | 2019-02-25 | 2019-02-25 | Helicopter belly convenient to carry on multiple equipment simultaneously |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920237678.XU CN209938929U (en) | 2019-02-25 | 2019-02-25 | Helicopter belly convenient to carry on multiple equipment simultaneously |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209938929U true CN209938929U (en) | 2020-01-14 |
Family
ID=69122863
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920237678.XU Expired - Fee Related CN209938929U (en) | 2019-02-25 | 2019-02-25 | Helicopter belly convenient to carry on multiple equipment simultaneously |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209938929U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112278279A (en) * | 2020-12-30 | 2021-01-29 | 江西云本数字科技有限公司 | Remote sensing monitored control system based on unmanned aerial vehicle |
-
2019
- 2019-02-25 CN CN201920237678.XU patent/CN209938929U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112278279A (en) * | 2020-12-30 | 2021-01-29 | 江西云本数字科技有限公司 | Remote sensing monitored control system based on unmanned aerial vehicle |
| CN112278279B (en) * | 2020-12-30 | 2021-03-26 | 荷塘智能科技(固安)有限公司 | Remote sensing monitored control system based on unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN209938929U (en) | Helicopter belly convenient to carry on multiple equipment simultaneously | |
| CN104707297B (en) | Low noise type straightly-drive type treadmill | |
| CN208707449U (en) | A kind of permanent-magnet brushless DC electric machine cushion socket of new and effective printing winding | |
| CN103705160B (en) | A kind of bathroom accessories being provided with buffer unit | |
| CN104759061A (en) | Road condition simulation running machine | |
| CN104707296B (en) | Low energy consumption high-efficiency treadmill | |
| CN106655609B (en) | A kind of Moving adjusting electromechanical actuator | |
| CN211512529U (en) | Swing mechanism of fat losing machine | |
| CN110427080B (en) | Computer cabinet | |
| ITGE20110131A1 (en) | REFINABLE FLAT BENCH | |
| CN208313548U (en) | A kind of rotary transformer vibration test machine | |
| CN213043500U (en) | Three-phase asynchronous motor with shell quick-disassembling structure | |
| CN105947177B (en) | A kind of swing-wing manned vehicle | |
| CN215767685U (en) | Automobile detection equipment protection device | |
| CN205770208U (en) | A kind of test fixture of big back amount formula motion | |
| CN101458146B (en) | Device for testing dynamic balance of fan rotor for horizontal type balancing machine | |
| CN114079347A (en) | Three-phase asynchronous motor with safe locking structure for escalator | |
| CN208061559U (en) | A kind of travelling guider | |
| CN210783603U (en) | Balanced rotation formula integral type mechanism | |
| CN207603904U (en) | A kind of runway type voice coil convenient for quick disassembling function | |
| CN208647133U (en) | Portable unmanned machine | |
| CN207589335U (en) | A kind of Novel cloud cabinet | |
| CN208164828U (en) | A kind of automotive seat spring shock absorption mechanism | |
| CN217049033U (en) | Unmanned helicopter of bispin wing organism that excels in | |
| CN109674236A (en) | A kind of bookshelf with Telescopic |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200114 Termination date: 20210225 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |