CN111409843A - Task equipment connecting mechanism - Google Patents
Task equipment connecting mechanism Download PDFInfo
- Publication number
- CN111409843A CN111409843A CN202010401940.7A CN202010401940A CN111409843A CN 111409843 A CN111409843 A CN 111409843A CN 202010401940 A CN202010401940 A CN 202010401940A CN 111409843 A CN111409843 A CN 111409843A
- Authority
- CN
- China
- Prior art keywords
- equipment
- task
- connecting mechanism
- mechanism according
- equipment end
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 230000007246 mechanism Effects 0.000 title claims abstract description 53
- 238000003780 insertion Methods 0.000 claims description 10
- 230000037431 insertion Effects 0.000 claims description 10
- 230000008878 coupling Effects 0.000 claims description 2
- 238000010168 coupling process Methods 0.000 claims description 2
- 238000005859 coupling reaction Methods 0.000 claims description 2
- 238000009434 installation Methods 0.000 abstract description 4
- 238000005381 potential energy Methods 0.000 description 3
- 238000000926 separation method Methods 0.000 description 3
- 230000006978 adaptation Effects 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 210000001503 joint Anatomy 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Details Of Connecting Devices For Male And Female Coupling (AREA)
Abstract
The invention discloses a task equipment connecting mechanism which comprises an airborne end and an equipment end, wherein the airborne end is arranged on an aircraft, the equipment end is arranged on task equipment, an electric connecting port is arranged on the airborne end, an electric connector matched with the electric connecting port is arranged on the equipment end, a sliding groove for inserting the equipment end is arranged on the airborne end, and an anti-falling locking mechanism for preventing the equipment end from retreating from the sliding groove is arranged between the airborne end and the equipment end. The task equipment connecting mechanism can realize quick installation and disassembly of task equipment, is convenient for replacing different task equipment to realize different functions, enlarges the application range, realizes mechanical connection and electrical connection integrally, is simple and quick to operate, high in connection reliability and high in safety, has an automatic locking function, and can effectively avoid the situation that the task equipment is accidentally separated and falls off.
Description
Technical Field
The invention relates to the technical field of aircrafts, in particular to a task equipment connecting mechanism.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing a radio remote control device or a self-contained program control device, and the existing task equipment connecting mechanism is widely applied and is well applied in 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, electric power inspection, disaster relief, movie and television shooting, romantic manufacturing and the like. Unmanned aerial vehicle can carry on task equipment usually and carry out a certain practical application task, current unmanned aerial vehicle adopts the mode of task equipment snap-on the fuselage usually, can't change, and nimble suitability is poor, is difficult to use unmanned aerial vehicle in the different scenes, and traditional task equipment is usually that mechanical connection part is independent with electric connection part when being connected to on the fuselage, need connect respectively and dismantle, installs and removes inconveniently, it is inefficient to maintain the change.
Disclosure of Invention
The invention aims to solve the technical problems and provides a task equipment connecting mechanism which is an improvement on the prior art and solves the problems that the connecting mode of the task equipment of an unmanned aerial vehicle in the prior art is flexible and poor in applicability, inconvenient to assemble and disassemble and low in maintenance and replacement efficiency.
In order to solve the technical problems, the technical scheme of the invention is as follows:
the utility model provides a task equipment coupling mechanism, is including installing the machine on the aircraft and holding and installing the equipment end on the task equipment, the machine carry and serve and be provided with the electric connector, the equipment serve be provided with the electric connector that the electric connector matches, and the machine carry and serve and be provided with the equipment end male spout that supplies to the machine carries and still be provided with the anticreep locking mechanical system that prevents the equipment end and withdraw from the spout between end and the equipment end. The invention integrates the mechanical connection and the electrical connection of the task equipment, namely, the mechanical connection and the fixation of the task equipment on the unmanned aerial vehicle and the electrical connection of the task equipment and an electrical system of the unmanned aerial vehicle are simultaneously realized through the connection of the airborne end and the equipment end, the operation is simple and rapid, the connection reliability is good, the separation of the equipment end and the airborne end under the condition of no operation is avoided by using the anti-falling locking mechanism, the condition that the task equipment is accidentally separated and falls off can be avoided, and the use safety and the reliability of the unmanned aerial vehicle are improved.
Furthermore, the electric connector and the electric connector are in butt joint and separation when the onboard end moves along the sliding groove, namely, the electric connection and the mechanical connection are completed synchronously, the assembly and disassembly efficiency is improved, the mechanical plugging operation and the electrical interface plugging operation are avoided, and the complex operation degree is reduced.
Furthermore, the electric connection port is arranged at the tail end of the sliding direction of the sliding groove, the electric connector is arranged at the front end of the inserting direction of the equipment end, the assembling and disassembling are convenient and efficient, the equipment end does not withdraw from the sliding groove, the electric connector and the electric connector cannot be separated, the electric connection reliability can be effectively guaranteed, and the poor contact condition is avoided.
Furthermore, the lateral wall of spout on be provided with along the guided way of slip direction, the lateral wall of equipment end on be provided with the guide way that matches with the guided way, improve equipment end along the gliding degree of accuracy of spout to ensure that electrical connector and electric connector can accurate butt joint.
Further, anticreep locking mechanism supply the elastic pin male jack including the elastic pin that sets up on the lateral wall of equipment end and set up on the lateral wall of spout, simple structure, implementation convenience, easy operation, locking reliability is high, equipment end inserts and carries automatic realization locking behind the end, effectively prevents unexpected the deviating from, need not the manual work and carries out the operation of locking again after the plug-in operation, avoids appearing forgetting to carry out the produced potential safety hazard of locking operation.
Furthermore, anticreep locking mechanical system respectively be provided with one in the both sides of spout slip direction, improve the reliability of locking, to preventing that equipment end and machine from carrying the end accident separately increasing the guarantee.
Furthermore, the anti-falling locking mechanism further comprises a key which is movably inserted into the jack and used for unlocking, the elastic pin is driven to return to the end of the equipment to realize unlocking by pressing the key, and the convenience of operation is improved.
Furthermore, an elastic pushing mechanism for pushing the equipment end out of the sliding chute is further arranged in the sliding chute, after the anti-falling locking mechanism is operated to unlock, the equipment end withdraws along the sliding chute under the action of the elastic pushing mechanism, so that the equipment end can be more conveniently and completely pulled out of the sliding chute, the operation convenience is improved, in addition, a certain fit clearance exists due to the adoption of the connecting mode of the sliding chute plug-in connection between the airborne end and the equipment end, the fit clearance can generate larger vibration in the flight process, the working reliability of task equipment is seriously influenced, therefore, the elastic pushing mechanism can also play a role of generating pre-tightening force when the equipment end is inserted into the airborne end, the acting force of the elastic pushing mechanism faces the direction of the sliding chute withdrawal, the fit clearance between the airborne end and the equipment end can be filled and eliminated, the anti-falling locking mechanism is more tightly matched and locked, and the vibration problem is, the working stability and reliability of the task equipment are guaranteed.
Furthermore, the elastic pushing mechanism is arranged at the tail end of the sliding direction of the sliding groove, the structure is compact, the external space is not occupied, and the equipment end can be reliably pushed along the sliding groove.
Furthermore, the elastic pushing mechanism is composed of a pushing block and a pushing spring, and is simple in structure, convenient to implement and good in pushing reliability.
Compared with the prior art, the invention has the advantages that:
the task equipment connecting mechanism can realize quick installation and disassembly of task equipment, is convenient for replacing different task equipment to realize different functions, enlarges the application range, realizes mechanical connection and electrical connection integrally, is simple and quick to operate, high in connection reliability and high in safety, has an automatic locking function, and can effectively avoid the situation that the task equipment is accidentally separated and falls off.
Drawings
FIG. 1 is a schematic diagram of a configuration of a machine-mounted end and an equipment end;
FIG. 2 is a schematic structural view of an onboard end;
FIG. 3 is an exploded view of the vehicle-mounted end;
FIG. 4 is a schematic diagram of the structure of the device side;
FIG. 5 is an exploded view of the device side
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
The task equipment connecting mechanism disclosed by the embodiment of the invention has a simple and compact structure, integrates mechanical connection and electrical connection into a whole, is convenient to assemble, disassemble and maintain, has high efficiency, can flexibly replace task equipment applied to different scenes, and increases the application range of the unmanned aerial vehicle.
As shown in fig. 1 to 5, the task device connecting mechanism mainly includes an onboard end 41 installed on the aircraft and a device end 42 installed on the task device, the onboard end 41 is provided with an electrical connector 43, the device end 42 is provided with an electrical connector 44 matching with the electrical connector 43, the onboard end 41 is provided with a chute 45 into which the device end 42 is inserted, and an anti-drop locking mechanism for preventing the device end 42 from dropping out of the chute 45 is further provided between the onboard end 41 and the device end 42, the task device connecting mechanism of the present embodiment can be used to conveniently and rapidly connect the task device to the aircraft body, and integrate the mechanical connection and the electrical connection of the task device into a whole, so that the installation operation is simpler and faster, and different types of task devices can be conveniently replaced, so that the aircraft can be applied to different requirements, the application range is enlarged.
Specifically, the electrical connector 43 and the electrical connector 44 are 40pin electrical connectors, which can meet the use requirements of most task devices;
in order to improve the efficiency of assembly and disassembly, when the task equipment is mechanically fixed on the body of the aircraft and the electric connecting port 43 and the electric connector 44 are connected, the direction of insertion and extraction of the electric connecting port 43 and the electric connector 44 is set to the direction of movement of the machine-carrying end 41 along the sliding chute 45, specifically, the electric connecting port 43 is arranged at the tail end of the sliding chute 45, the electric connector 44 is arranged at the front end of the insertion direction of the equipment end 42, so that the electric connecting port 43 and the electric connector 44 are inserted while the equipment end 42 is inserted along the sliding chute 45, and the electric connecting port 43 and the electric connector 44 are separated while the equipment end 42 is extracted along the sliding chute 45, thereby simplifying the operation of assembly and disassembly of the task equipment and improving the efficiency of assembly and disassembly, the electric connecting port 43 is arranged at the tail end of the sliding chute 45, and the electric connector 44 is arranged at the front end of the equipment end 42, after the installation is finished, the electric connection port 43 and the electric connector 44 are blocked by the equipment end 42, and due to the existence of the anti-falling locking mechanism, the equipment end 42 cannot withdraw from the sliding groove 45, so that the electric connection stability of the electric connection port 43 and the electric connector 44 can be ensured, the condition of poor electric connection contact can be avoided, and when the equipment end 42 is inserted into the sliding groove 45 in place, the electric connection port 43 and the electric connector 44 are wrapped inside the equipment end 42 and the task end, the electric connection port 43 and the electric connector 44 can be effectively protected, the electric connection can be prevented from being damaged due to exposure outside, the reliability of electric connection can be further ensured, and the task equipment can stably work;
in this embodiment, the left and right side walls of the sliding slot 45 in the sliding direction are provided with the guide rails 451 along the sliding direction, the side wall of the equipment end 42 is provided with the guide grooves 452 matched with the guide rails 451, so that the accuracy of inserting and pulling the equipment end 42 into and out of the sliding slot is improved, the electrical connection port 43 and the electrical connector 44 can be accurately butted, and the situation that the electrical connector 44 is difficult to be inserted into the electrical connection port 43 is avoided;
the anti-falling locking mechanism mainly comprises an elastic pin 46 arranged on the side wall of the side where the guide groove 452 of the equipment end 42 is arranged and a jack 47 arranged on the side wall of the side where the guide rail 451 of the sliding groove 45 is arranged for inserting the elastic pin 46, the elastic pin 46 is similar to a latch structure, the front end side facing the inserting direction of the equipment end 42 is a guide inclined surface, the rear end side facing the inserting direction of the equipment end 42 is a right-angled surface, the elastic pin 46 comprises a pin and a spring for pushing the pin to protrude out of the equipment end 42, when the equipment end 42 is inserted into the vehicle-mounted end 41 along the sliding groove 45, the elastic pin 46 is pressed and retracted into the equipment end 42 by the side wall of the sliding groove 45 when the elastic pin 46 does not reach the jack 47 position, and when the equipment end 42 is inserted into the place, the elastic pin 46 just reaches the jack 47 position, so that the elastic pin 46 is reset to pop out of the jack 47 to achieve the, the equipment end 42 is prevented from reversely exiting the chute 45, so that the task equipment is reliably connected to the aircraft, and the dangerous condition that the task equipment is separated from the aircraft is avoided;
furthermore, the anti-disengaging locking mechanism further comprises a key 48 movably inserted into the insertion hole 47 for unlocking, and the elastic pin 46 is pushed by pushing the key 48, so that the elastic pin 46 retracts towards the inside of the equipment end 42, and the locking state of the equipment end 42 and the airborne end 41 is released, and the operation is simple and rapid; in this embodiment, the anti-falling locking mechanism is provided one on each of the left and right sides of the sliding direction of the sliding chute 45, the insertion hole 47 penetrates through the side wall of the sliding chute 45 in the left and right directions of the sliding chute 45, the button 48 is provided on the left and right sides of the sliding chute 45, and unlocking can be achieved by pressing the button 48 toward the center of the sliding chute 45;
in order to facilitate the separation of the equipment end 42 and the onboard end 41, an elastic pushing mechanism 49 for pushing the equipment end 42 out of the chute 45 is further arranged in the chute 45, that is, when the button 48 is pressed to press the elastic pin 46 back into the equipment end 42 so that the locking state of the insertion hole 47 of the elastic pin 46 is released, the elastic pushing mechanism 49 pushes the equipment end 42 to move out of the chute 45, specifically, the elastic pushing mechanism 49 is arranged at the end of the sliding direction of the chute 45, the elastic pushing mechanism 49 is composed of a pushing block and a pushing spring, when the equipment end 42 is inserted along the chute 45, the equipment end 42 will push the elastic pushing mechanism 49 so that the pushing spring of the elastic pushing mechanism 49 is compressed to store elastic potential energy, and when the elastic pin 46 is inserted into the locking state of the insertion hole 47, the elastic pushing mechanism 49 is always in the state of storing elastic potential energy, when the elastic pin 46 exits the insertion hole 47 to become an unlocked state, the elastic pushing mechanism 49 releases elastic potential energy to push the equipment end 42 outwards along the sliding groove 45, so that the convenience of disassembly is improved.
The above is only a preferred embodiment of the present invention, and it should be noted that the above preferred embodiment should not be considered as limiting the present invention, and the protection scope of the present invention should be subject to the scope defined by the claims. It will be apparent to those skilled in the art that various modifications and adaptations can be made without departing from the spirit and scope of the invention, and these modifications and adaptations should be considered within the scope of the invention.
Claims (10)
1. The utility model provides a task equipment coupling mechanism, characterized in that, is including installing airborne end (41) on the aircraft and installing equipment end (42) on the task equipment, airborne end (41) on be provided with electric connector (43), equipment end (42) on be provided with electric connector (44) that match with electric connector (43), and airborne end (41) on be provided with and supply equipment end (42) male spout (45) to still be provided with the anticreep locking mechanical system that prevents equipment end (42) to withdraw from spout (45) between airborne end (41) and equipment end (42).
2. The mission device connection mechanism according to claim 1, wherein the electrical connection port (43) and the electrical connector (44) are engaged and disengaged when the vehicle-mounted end (41) moves along the slide groove (45).
3. The task equipment connecting mechanism according to claim 1, wherein the electrical connection port (43) is provided at an end in a sliding direction of the slide groove (45), and the electrical connector (44) is provided at a front end in an insertion direction of the equipment terminal (42).
4. The task equipment connecting mechanism according to claim 1, characterized in that the side wall of the chute (45) is provided with a guide rail (451) along the sliding direction, and the side wall of the equipment end (42) is provided with a guide groove (452) matched with the guide rail (451).
5. The task equipment connecting mechanism according to claim 1, characterized in that the anti-disengagement locking mechanism comprises an elastic pin (46) provided on a side wall of the equipment end (42) and an insertion hole (47) provided on a side wall of the slide groove (45) for inserting the elastic pin (46).
6. The task equipment connecting mechanism according to claim 5, characterized in that the anti-drop locking mechanism is provided one on each side of the sliding direction of the slide groove (45).
7. The task device connecting mechanism according to claim 5, characterized in that the anti-disengagement locking mechanism further comprises a button (48) movably inserted in the insertion hole (47) for unlocking.
8. The mission equipment connecting mechanism according to claim 1, wherein an elastic pushing mechanism (49) for pushing the equipment end (42) out of the chute (45) is further provided in the chute (45).
9. The mission equipment connecting mechanism according to claim 8, wherein the elastic thrusting mechanism (49) is provided at the end of the sliding direction of the chute (45).
10. The mission equipment connecting mechanism according to claim 8, wherein the elastic urging mechanism (49) is composed of an urging block and an urging spring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010401940.7A CN111409843A (en) | 2020-05-13 | 2020-05-13 | Task equipment connecting mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010401940.7A CN111409843A (en) | 2020-05-13 | 2020-05-13 | Task equipment connecting mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111409843A true CN111409843A (en) | 2020-07-14 |
Family
ID=71490465
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010401940.7A Pending CN111409843A (en) | 2020-05-13 | 2020-05-13 | Task equipment connecting mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111409843A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113471738A (en) * | 2021-07-16 | 2021-10-01 | 北京晶品特装科技股份有限公司 | Quick-change device and assembling method thereof |
| CN113581477A (en) * | 2021-06-29 | 2021-11-02 | 成都纵横大鹏无人机科技有限公司 | Functional module mounting structure and aircraft adopting same |
| CN114572409A (en) * | 2022-05-07 | 2022-06-03 | 北京卓翼智能科技有限公司 | A installation device and unmanned aerial vehicle for unmanned aerial vehicle load |
-
2020
- 2020-05-13 CN CN202010401940.7A patent/CN111409843A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113581477A (en) * | 2021-06-29 | 2021-11-02 | 成都纵横大鹏无人机科技有限公司 | Functional module mounting structure and aircraft adopting same |
| CN113581477B (en) * | 2021-06-29 | 2024-04-26 | 成都纵横大鹏无人机科技有限公司 | Function module mounting structure and adopt its aircraft |
| CN113471738A (en) * | 2021-07-16 | 2021-10-01 | 北京晶品特装科技股份有限公司 | Quick-change device and assembling method thereof |
| CN113471738B (en) * | 2021-07-16 | 2023-11-03 | 北京晶品特装科技股份有限公司 | Quick-change device and assembly method thereof |
| CN114572409A (en) * | 2022-05-07 | 2022-06-03 | 北京卓翼智能科技有限公司 | A installation device and unmanned aerial vehicle for unmanned aerial vehicle load |
| CN114572409B (en) * | 2022-05-07 | 2022-07-29 | 北京卓翼智能科技有限公司 | A installation device and unmanned aerial vehicle for unmanned aerial vehicle load |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN111409843A (en) | Task equipment connecting mechanism | |
| EP3067724B1 (en) | Optical connector plug | |
| CN105633716B (en) | High-tension connector | |
| CN101572363B (en) | Electrical connector having pull tether for latch release | |
| CN110383524B (en) | Battery module and unmanned aerial vehicle | |
| KR102205924B1 (en) | Connection system with bayonet-type locking device configured to allow quick disconnect operation | |
| CN108521051B (en) | Secondary locking and time-delay unlocking structure | |
| CN105846242A (en) | Handle-type high-voltage connector | |
| CN217182547U (en) | Connector with CPA structure | |
| US20190221970A1 (en) | Anti-off socket | |
| US10985500B2 (en) | Connector assembly | |
| CN113933943B (en) | Connector assembly and plug and adapter thereof | |
| CN217740931U (en) | Electric connecting device and plug connector | |
| CN113189713B (en) | Locking mechanism, connector and connector assembly | |
| CN212099372U (en) | Task equipment connecting mechanism | |
| CN103688421B (en) | Electric coupler component | |
| CN212158327U (en) | A release and insert mechanism that is used for between rocket bomb and launching tube | |
| CN219917772U (en) | Lockable connector | |
| CN218958151U (en) | Charging gun head and charging system | |
| CN113253394B (en) | Miniaturized hierarchical transmission mechanism, connector and connector assembly | |
| US11855380B2 (en) | Adapter, plug connector assembly and connector assembly | |
| DE102010061185B4 (en) | Locking actuator for an electrical connector | |
| CN209963386U (en) | Subminiature high-speed high-density communication connector | |
| CN117199915A (en) | Push-type secondary locking structure and electric connector | |
| CN218055648U (en) | Unmanned aerial vehicle rapid disassembly structure |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |