CN219237408U - Inertial navigation mounting structure for intelligent unmanned aerial vehicle - Google Patents
Inertial navigation mounting structure for intelligent unmanned aerial vehicle Download PDFInfo
- Publication number
- CN219237408U CN219237408U CN202223594429.7U CN202223594429U CN219237408U CN 219237408 U CN219237408 U CN 219237408U CN 202223594429 U CN202223594429 U CN 202223594429U CN 219237408 U CN219237408 U CN 219237408U
- Authority
- CN
- China
- Prior art keywords
- hole
- positioning
- aerial vehicle
- unmanned aerial
- rod
- 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.)
- Active
Links
Images
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses an inertial navigation mounting structure for an intelligent unmanned aerial vehicle, which relates to the technical field of unmanned aerial vehicle equipment and comprises a navigator body, wherein a fixing box is arranged at the rear part of the navigator body, a fixing mechanism for quickly connecting the fixing box with the navigator body is arranged in the fixing box, a connecting component for vertically mounting the navigator body in the fixing mechanism is arranged at the back of the navigator body, a pull rod can drive a clamping block to move through the fixing mechanism, the clamping block can squeeze a spring when moving, the stability of the pull rod can be ensured, the bottom of the positioning rod penetrates through a first through hole and extends into the fixing box, the bottom of the positioning rod penetrates through a second through hole and the inside of the positioning hole in sequence, the fixing of the positioning rod can be realized, the quick mounting and dismounting of the navigator is convenient, the time for the overhaul of workers is avoided, the labor intensity of the workers is reduced, the working efficiency of the workers is improved, and the use of the workers is facilitated.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle equipment, in particular to an inertial navigation installation structure for an intelligent unmanned aerial vehicle.
Background
The inertial navigation device is an autonomous navigation device which does not depend on external information and radiates energy to the outside, and the basic working principle is that information such as speed, yaw angle and position in a navigation coordinate system can be obtained by measuring acceleration of a carrier in an inertial reference system, integrating the acceleration with time and transforming the acceleration into the navigation coordinate system based on Newton's law of mechanics. Currently, inertial navigation devices are widely used in transportation means such as airplanes, submarines, space planes and the like and in missiles.
The existing inertial navigation equipment is installed and fixed by adopting bolts in the using process, is complex in operation, is inconvenient for personnel to disassemble and maintain in the later period, and further needs a large amount of time when the navigation equipment is installed, when the navigation equipment is maintained and replaced, the time for overhauling the personnel is wasted, the labor intensity of the personnel is enhanced, the working efficiency of the personnel is reduced, and the use of the personnel is inconvenient.
Aiming at the problems, the utility model provides an inertial navigation installation structure for an intelligent unmanned aerial vehicle.
Disclosure of Invention
The utility model aims to provide an inertial navigation installation structure for an intelligent unmanned aerial vehicle, which is characterized in that a fixing mechanism is arranged, when the inertial navigation installation structure is installed, a pull rod is firstly held by a pull handle to pull the pull rod to the outside, the pull rod can drive a clamping block to move, the clamping block can squeeze a spring when moving, the stability of the movement of the pull rod can be ensured, the bottom of a positioning rod penetrates through a first through hole to extend into a fixing box, the bottom of the positioning rod penetrates through a second through hole and the inside of a positioning hole in sequence, the fixing of the positioning rod can be realized, the rapid installation and the disassembly of navigation equipment are convenient, the time for overhauling workers is avoided, the labor intensity of the workers is reduced, the working efficiency of the workers is improved, and the use of the workers is facilitated, thereby solving the problem in the background technology.
In order to achieve the above purpose, the present utility model provides the following technical solutions: an inertial navigation mounting structure for an intelligent unmanned aerial vehicle; the device comprises a navigator body, wherein a fixing box is arranged at the rear part of the navigator body, a fixing mechanism for quickly connecting the fixing box with the navigator body is arranged in the fixing box, and the fixing mechanism comprises two clamping blocks symmetrically arranged in the fixing box;
the navigator body back is equipped with and is used for vertically installing the inside coupling assembling of fixed establishment with the navigator body.
Further, fixed establishment still includes pull rod, the spring, the locating piece, first through-hole, locating hole and second through-hole, the pull rod transversely runs through fixed box lateral wall, and pull rod and fixed box sliding connection, the pull rod is located the inside one end fixedly connected with fixture block of fixed box, the second through-hole has vertically been seted up to the fixture block, cup jointed the spring on the pull rod between fixture block and the fixed box lateral wall, fixed box top is equipped with first through-hole, bottom surface fixedly connected with locating piece in the fixed box, the locating hole has been seted up on the locating piece, the one end fixedly connected with pull handle of fixture block is kept away from to the pull rod.
Further, the connecting assembly comprises a positioning rod and a connecting rod, one end of the connecting rod is fixedly connected with the back of the navigator body, and the other end of the connecting rod is fixedly connected with the top of the positioning rod.
Further, the bottom of the positioning rod extends to the inside of the fixing box to sequentially penetrate through the first through hole, the second through hole and the positioning hole, and the positioning rod is mutually matched with the first through hole, the second through hole and the positioning hole.
Further, the diameters of the first through hole, the second through hole and the positioning hole are consistent, and the first through hole and the positioning hole are located on the same axis.
Further, the back of the fixed box is fixedly connected with a mounting plate, and a plurality of mounting holes are formed in the mounting plate.
Compared with the prior art, the utility model has the following beneficial effects:
1. according to the inertial navigation installation structure for the intelligent unmanned aerial vehicle, the fixing mechanism is arranged, when the inertial navigation installation structure is installed, the pull rod is firstly held by the pull handle to pull the pull rod to the outside, the pull rod can drive the clamping block to move, the spring can be extruded while the clamping block moves, the stability of the movement of the pull rod can be ensured, the bottom of the positioning rod penetrates through the first through hole to extend into the fixing box, the bottom of the positioning rod penetrates through the second through hole and the inside of the positioning hole in sequence, the fixing of the positioning rod can be realized, the rapid installation and the disassembly of navigation equipment are convenient, the time for overhauling of workers is avoided, the labor intensity of the workers is reduced, the working efficiency of the workers is improved, and the use of the workers is facilitated.
2. According to the inertial navigation installation structure for the intelligent unmanned aerial vehicle, the connecting assembly is arranged, and the navigator body is connected with the fixed box through the connecting rod, so that the navigator body can be conveniently separated from the fixed box, and the problem that the existing unmanned aerial vehicle navigator is troublesome to install and detach is solved.
Drawings
FIG. 1 is a perspective view of the present utility model;
FIG. 2 is a perspective view of a fixing case of the present utility model;
FIG. 3 is a perspective view of the securing mechanism of the present utility model;
FIG. 4 is a cross-sectional view of a mounting box of the present utility model;
fig. 5 is a perspective view of the connection assembly of the present utility model.
In the figure: 1. a mounting plate; 2. a mounting hole; 3. a fixed box; 4. a fixing mechanism; 41. a clamping block; 42. a pull rod; 43. a spring; 44. a positioning block; 45. a first through hole; 46. positioning holes; 47. a second through hole; 5. a pull handle; 6. a connection assembly; 61. a positioning rod; 62. a connecting rod; 7. a navigator body.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
In order to solve the technical problem of how to quickly detach or install the navigation device, as shown in fig. 1-5, the following preferred technical scheme is provided:
the utility model provides an inertial navigation mounting structure for intelligent unmanned aerial vehicle, includes navigator body 7, and navigator body 7 rear portion is equipped with fixed box 3, is equipped with the fixed mechanism 4 that is used for quick connection fixed box 3 and navigator body 7 in the fixed box 3, and fixed mechanism 4 includes two fixture blocks 41 that set up in fixed box 3 symmetry;
the back of the navigator body 7 is provided with a connecting assembly 6 for vertically mounting the navigator body 7 inside the fixing mechanism 4.
In order to solve the technical problem of how to quickly detach or install the navigation device, as shown in fig. 1-5, the following preferred technical scheme is provided:
the fixing mechanism 4 further comprises a pull rod 42, a spring 43, a positioning block 44, a first through hole 45, a positioning hole 46 and a second through hole 47, the pull rod 42 transversely penetrates through the side wall of the fixing box 3, the pull rod 42 is in sliding connection with the fixing box 3, one end of the pull rod 42, located inside the fixing box 3, is fixedly connected with a clamping block 41, the clamping block 41 is vertically provided with the second through hole 47, the spring 43 is sleeved on the pull rod 42 between the clamping block 41 and the side wall of the fixing box 3, the first through hole 45 is formed in the top of the fixing box 3, the positioning block 44 is fixedly connected with the inner bottom surface of the fixing box 3, the positioning hole 46 is formed in the positioning block 44, and one end, away from the clamping block 41, of the pull rod 42 is fixedly connected with a pull handle 5. Specifically, holding the pull handle 5 pulls the pull rod 42 to the outside, and the pull rod 42 can drive the fixture block 41 to move, and the fixture block 41 can squeeze the spring 43 when moving, can guarantee the stationarity of pull rod 42 motion, runs through first through hole 45 with the locating lever 61 bottom and extends to inside the fixed box 3, runs through second through hole 47 and locating hole 46 inside in proper order with the locating lever 61 bottom, can realize the fixed to the locating lever 61.
In order to solve the technical problem of how to quickly detach or install the navigation device, as shown in fig. 1-5, the following preferred technical scheme is provided:
the connecting component 6 comprises a positioning rod 61 and a connecting rod 62, one end of the connecting rod 62 is fixedly connected with the back surface of the navigator body 7, and the other end of the connecting rod 62 is fixedly connected with the top of the positioning rod 61. Specifically, the positioning rod 61 is inserted into the fixing case 3 to connect the navigator body 7 with the fixing case 3, thereby fixing the navigator body 7.
Further, as shown in fig. 1-5, the following preferred technical scheme is provided:
the bottom of the positioning rod 61 extends to the inside of the fixed box 3 to sequentially penetrate through the first through hole 45, the second through hole 47 and the positioning hole 46, and the positioning rod 61 is mutually matched with the first through hole 45, the second through hole 47 and the positioning hole 46. Specifically, the bottom of the positioning rod 61 penetrates through the first through hole 45 to extend into the fixed box 3, and the bottom of the positioning rod 61 penetrates through the second through hole 47 and the positioning hole 46 in sequence, so that the positioning rod 61 can be fixed, and the navigator can be quickly installed and detached.
Further, as shown in fig. 1-5, the following preferred technical scheme is provided:
the first through hole 45, the second through hole 47 and the positioning hole 46 have the same diameter, and the first through hole 45 and the positioning hole 46 are located on the same axis. Specifically, this arrangement ensures that the positioning rod 61 can pass through the first through hole 45, the second through hole 47, and the positioning hole 46 in this order.
In order to solve the technical problem of how to quickly detach or install the navigation device, as shown in fig. 1-5, the following preferred technical scheme is provided:
the back of the fixed box 3 is fixedly connected with a mounting plate 1, and a plurality of mounting holes 2 are formed in the mounting plate 1. Specifically, staff accessible fixing bolt and mounting hole 2 are fixed mounting panel 1 on unmanned aerial vehicle, easy operation, convenient to use, and the practicality is stronger.
Working principle: when the navigation device is required to be installed on an unmanned aerial vehicle, a worker can fix the mounting plate 1 on the unmanned aerial vehicle through the fixing bolts and the mounting holes 2, firstly, the pull handle 5 is held to pull the pull rod 42 outwards, the pull rod 42 can drive the clamping block 41 to move, the clamping block 41 can squeeze the spring 43 when moving, the stability of the movement of the pull rod 42 can be ensured, the bottom of the positioning rod 61 penetrates through the first through hole 45 to extend into the fixing box 3, the bottom of the positioning rod 61 penetrates through the second through hole 47 and the inside of the positioning hole 46 in sequence, the fixing of the positioning rod 61 can be realized, the navigator body 7 is vertically pushed upwards when the navigator body 7 is dismounted, the positioning rod 61 is driven to break away from the fixing box 3, the navigator body 7 can be dismounted, the time of wasting of the worker maintenance is avoided, the labor intensity of the worker is reduced, and the working efficiency of the worker is improved.
It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. An inertial navigation mounting structure for intelligent unmanned aerial vehicle, includes navigator body (7), its characterized in that: the rear part of the navigator body (7) is provided with a fixed box (3), a fixed mechanism (4) for quickly connecting the fixed box (3) with the navigator body (7) is arranged in the fixed box (3), and the fixed mechanism (4) comprises two clamping blocks (41) symmetrically arranged in the fixed box (3);
the back of the navigator body (7) is provided with a connecting component (6) for vertically installing the navigator body (7) into the fixing mechanism (4).
2. The inertial navigation mounting structure for an intelligent unmanned aerial vehicle of claim 1, wherein: the fixing mechanism (4) further comprises a pull rod (42), a spring (43), a positioning block (44), a first through hole (45), a positioning hole (46) and a second through hole (47), wherein the pull rod (42) transversely penetrates through the side wall of the fixing box (3), the pull rod (42) is in sliding connection with the fixing box (3), one end of the pull rod (42) located inside the fixing box (3) is fixedly connected with a clamping block (41), the clamping block (41) is vertically provided with the second through hole (47), the spring (43) is sleeved on the pull rod (42) between the clamping block (41) and the side wall of the fixing box (3), the first through hole (45) is formed in the top of the fixing box (3), the positioning block (44) is fixedly connected with the positioning block (44), and the positioning hole (46) is formed in the positioning block (44), and one end, away from the clamping block (41), of the pull rod (42), of the clamping block (41) is fixedly connected with a pull handle (5).
3. The inertial navigation mounting structure for an intelligent unmanned aerial vehicle of claim 1, wherein: the connecting assembly (6) comprises a positioning rod (61) and a connecting rod (62), one end of the connecting rod (62) is fixedly connected with the back of the navigator body (7), and the other end of the connecting rod (62) is fixedly connected with the top of the positioning rod (61).
4. An inertial navigation mounting structure for an intelligent unmanned aerial vehicle according to claim 3, wherein: the bottom of the locating rod (61) extends to the inside of the fixed box (3) to sequentially penetrate through the first through hole (45), the second through hole (47) and the locating hole (46), and the locating rod (61) is mutually matched with the first through hole (45), the second through hole (47) and the locating hole (46).
5. The inertial navigation mounting structure for an intelligent unmanned aerial vehicle of claim 2, wherein: the diameters of the first through hole (45), the second through hole (47) and the positioning hole (46) are consistent, and the first through hole (45) and the positioning hole (46) are positioned on the same axis.
6. The inertial navigation mounting structure for an intelligent unmanned aerial vehicle of claim 1, wherein: the back of the fixed box (3) is fixedly connected with a mounting plate (1), and a plurality of mounting holes (2) are formed in the mounting plate (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223594429.7U CN219237408U (en) | 2022-12-30 | 2022-12-30 | Inertial navigation mounting structure for intelligent unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223594429.7U CN219237408U (en) | 2022-12-30 | 2022-12-30 | Inertial navigation mounting structure for intelligent unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219237408U true CN219237408U (en) | 2023-06-23 |
Family
ID=86844649
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223594429.7U Active CN219237408U (en) | 2022-12-30 | 2022-12-30 | Inertial navigation mounting structure for intelligent unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219237408U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117508688A (en) * | 2023-11-23 | 2024-02-06 | 山东中宇航空科技发展有限公司 | Unmanned aerial vehicle instruction signaling device |
-
2022
- 2022-12-30 CN CN202223594429.7U patent/CN219237408U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117508688A (en) * | 2023-11-23 | 2024-02-06 | 山东中宇航空科技发展有限公司 | Unmanned aerial vehicle instruction signaling device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN219237408U (en) | Inertial navigation mounting structure for intelligent unmanned aerial vehicle | |
| CN208897306U (en) | Unmanned aerial vehicle body and wing fast assembling-disassembling connection structure | |
| CN103101759B (en) | Adjustable flexible side wall clamp | |
| CN218384392U (en) | Backlight driving board convenient to mount | |
| CN203946287U (en) | A kind of novel momentum wheel mounting bracket | |
| CN211266705U (en) | Split type motor assembly fixture of range extender | |
| CN212332975U (en) | Releasable towing pipe hanger | |
| CN211317465U (en) | Radar level meter convenient to dismantle | |
| CN203482690U (en) | Artificial influence weather onboard dispenser | |
| CN218041526U (en) | Vehicle-mounted camera structure easy to disassemble and assemble | |
| CN217878020U (en) | Transformer infrared temperature measurement mounting module suitable for unmanned aerial vehicle | |
| CN213354865U (en) | Push type mount quick assembly disassembly mechanism | |
| CN206537465U (en) | It is easy to the local component installation structure dismounted for autonomous underwater vehicle | |
| CN220404498U (en) | Multifunctional decontamination car | |
| CN219775292U (en) | Mounting bracket for laser range finder | |
| CN218658800U (en) | Balanced elbow quick assembly disassembly instrument of tracked vehicle | |
| CN216269957U (en) | Utilize unmanned aerial vehicle survey and drawing instrument fixing device for survey and drawing | |
| CN220198967U (en) | Universal wheel locking and positioning structure at bottom of dismounting bracket of aircraft engine | |
| CN216577686U (en) | Cantilever assembly fixture | |
| CN108645652B (en) | Convenient long column-shaped sampler winding and unwinding auxiliary device | |
| CN213354864U (en) | Spiral mounting and fast dismounting mechanism | |
| CN219194257U (en) | Mobile control box for single-beam crane | |
| CN204728229U (en) | Pavement reflecting board | |
| CN216545585U (en) | Vehicle spring hook | |
| CN218003734U (en) | GPS monitoring system of coal mine engineering vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |