CN107514185A - A kind of unmanned plane umbrella hatchcover automatic-opening mechanism - Google Patents
A kind of unmanned plane umbrella hatchcover automatic-opening mechanism Download PDFInfo
- Publication number
- CN107514185A CN107514185A CN201710553335.XA CN201710553335A CN107514185A CN 107514185 A CN107514185 A CN 107514185A CN 201710553335 A CN201710553335 A CN 201710553335A CN 107514185 A CN107514185 A CN 107514185A
- Authority
- CN
- China
- Prior art keywords
- umbrella hatchcover
- parachute
- mounting bracket
- umbrella
- hatchcover
- 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
Classifications
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B47/00—Operating or controlling locks or other fastening devices by electric or magnetic means
- E05B47/0001—Operating or controlling locks or other fastening devices by electric or magnetic means with electric actuators; Constructional features thereof
- E05B47/0002—Operating or controlling locks or other fastening devices by electric or magnetic means with electric actuators; Constructional features thereof with electromagnets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/80—Vertical take-off or landing, e.g. using rockets
- B64U70/83—Vertical take-off or landing, e.g. using rockets using parachutes, balloons or the like
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B17/00—Accessories in connection with locks
- E05B17/0025—Devices for forcing the wing firmly against its seat or to initiate the opening of the wing
- E05B17/0033—Devices for forcing the wing firmly against its seat or to initiate the opening of the wing for opening only
- E05B17/0037—Spring-operated
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B47/00—Operating or controlling locks or other fastening devices by electric or magnetic means
- E05B2047/0048—Circuits, feeding, monitoring
- E05B2047/005—Opening, closing of the circuit
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Mechanical Engineering (AREA)
- Holders For Apparel And Elements Relating To Apparel (AREA)
Abstract
The present invention relates to a kind of unmanned plane umbrella hatchcover automatic-opening mechanism, including mounting bracket, umbrella hatchcover, stage clip, catch, extractor parachute, parachute, suction iron iron plate and Electromagnetic lock component；The Electromagnetic lock component includes housing, control board, silicon steel sheet and coil；Electromagnetic lock component is located in the space that mounting bracket and umbrella hatchcover are formed, and is connected by housing and mounting bracket；Control board, silicon steel sheet and coil are fixed in housing；Iron iron plate is inhaled to be fixed on umbrella hatchcover；Stud is connected on mounting bracket by screw thread, and stage clip is cased with stud, and stage clip original state is compressive state.The present invention has been effectively saved fuselage space；Umbrella hatchcover is tightly pinned using magnetic adhesion caused by electromagnet, it is necessary to during parachute-opening, and flight control computer sends signal, cuts off the electricity supply, and magnetic adhesion disappears, and stage clip plays a role, while under airflow function, can fast and accurately open umbrella hatchcover.
Description
Technical field
The present invention relates to unmanned plane technical field of aerospace, and in particular to a kind of new unmanned plane umbrella hatchcover automatic opener
Structure.
Background technology
Unmanned plane recovery is broadly divided into running landing and parachuting landing two ways.Running landing is higher to site requirements,
For small and medium size unmanned aerial vehicles, in order to reclaim simplicity, landed and reclaimed using parachuting more.
When being reclaimed using parachuting landing, parachute is generally placed upon in the fuselage deckle board of unmanned plane, is covered with umbrella hatchcover.Work as nothing
Man-machine completion task is, it is necessary to when landing, it is necessary to opens umbrella hatchcover at once and discharges parachute, completes parachute-opening action.Work as unmanned plane
In the task of execution, it is not necessary to during parachute-opening, if umbrella hatchcover is opened, parachute can be caused to open, unmanned plane is crashed；Equally work as nothing
It is man-machine need landing when, if umbrella hatchcover accurately, can not be opened quickly, also result in unmanned plane crash.
Simultaneously because unmanned aerial vehicle body space is limited, the requirement to weight is higher, therefore umbrella hatchcover opener structure is not
Preferably complicated, occupancy volume is small, and functional reliability will height.
Chinese Patent Application No. CN 106184701A disclose a kind of unmanned plane parachute automatic-opening mechanism, by fixing
Bulkhead skeleton in internal body, the umbrella hatchcover that can be upspring automatically, the umbrella cabin for matching with umbrella hatchcover connection, steering wheel, drive shaft,
Steering wheel rocking arm, steering wheel fixed platform composition；Characterized in that, bulkhead skeleton is fixed on internal body, set at the top of bulkhead skeleton
There is steering wheel fixed platform；The side of bulkhead skeleton is provided with umbrella cabin, and the one end in umbrella cabin is flexibly connected one end of umbrella hatchcover, umbrella hatchcover
The other end and the sidepiece joint match of steering wheel fixed platform；Steering wheel is fixed with the inside of steering wheel fixed platform, is set on steering wheel
Drive shaft is connected by steering wheel fixed platform and steering wheel rocking arm.Its good effect is：Make full use of unmanned plane body
Unmanned plane parachute is loaded in inner space, facilitates the filling and unlatching of parachute；Umbrella hatchcover is reduced to greatest extent opens driving machine
Air drag produced by structure.
Unmanned plane parachute automatic-opening mechanism disclosed in document, automatically upspring using having of being matched on unmanned plane umbrella cabin
The umbrella hatchcover of function, to facilitate the filling of parachute and unlatching；When before unmanned plane takes off and flight course in, one end of umbrella hatchcover
(as shown in Figure 1) is suppressed by steering wheel rocking arm, to ensure flight safety；When unmanned plane drops to ground, in steering wheel fixed platform
The steering wheel of installation drives steering wheel rocking arm to stir to the left or in the range of 90 ° of right side by drive shaft, umbrella hatchcover is upspring automatically,
And parachute is opened, help unmanned plane to slow down with realization, the purpose of safe falling.The drive mechanism opened as umbrella hatchcover
Steering wheel, in unmanned plane body, only steering wheel rocking arm is exposed, and air produced by can reducing the part to greatest extent hinders
Power.
It is not difficult to find out, unmanned plane parachute automatic-opening mechanism has the following disadvantages disclosed in document：
First, need that a steering wheel is installed, add the unstability of mechanism operation；
2nd, the rocking arm at the top of steering wheel is during unmanned plane during flying, it is possible to occurs trembling due to caused in aircraft flight
It is dynamic to wait other situations, cause rocking arm to loosen, self falling so that umbrella hatchcover opens voluntarily, to add risk；
3rd, steering wheel rocking arm is only used only and pins umbrella hatchcover, and the matching for opening mechanism and the locking device certainly of umbrella hatchcover
Do not illustrate, matching is still to be tested.
The content of the invention
Present invention solves the technical problem that it is：In view of the shortcomings of the prior art, the present invention provides a kind of unmanned plane umbrella hatchcover
Automatic-opening mechanism, the mechanism utilize the principle of electric magnetisation, and when electric current passes through coil, electromagnetic lock can produce powerful magnetic attraction
Tightly hold iron iron plate and reach the effect for pinning umbrella hatchcover.After cutting off the electricity supply, electromagnetic lock loses magnetic attraction and made in stage clip
With lower opening umbrella hatchcover.
The technical scheme is that：A kind of unmanned plane umbrella hatchcover automatic-opening mechanism, including mounting bracket 1, umbrella hatchcover 3,
Stage clip 4, catch 6, extractor parachute and parachute；Characterized in that, also include inhaling iron iron plate 8 and Electromagnetic lock component 13；The electricity
Magnetic padlock body component 13 includes housing 2, control board 7, silicon steel sheet 9 and coil 10；Electromagnetic lock component 13 is located at the He of mounting bracket 1
In the space that umbrella hatchcover 3 is formed, it is connected by housing 2 and mounting bracket 1；Control board 7, silicon steel sheet 9 and coil 10 are fixed on
In housing 2；Iron iron plate 8 is inhaled to be fixed on umbrella hatchcover 3；Stud 5 is connected on mounting bracket 1 by screw thread, and stage clip is cased with stud 5
4, the original state of stage clip 4 is compressive state；Control board 7 in the Electromagnetic lock component 13 receives outside cut-offing instruction
Powered off, the current vanishes of coil 10, magnetic field caused by electric current disappears simultaneously, and magnetic attraction caused by silicon steel sheet 9 disappears, silicon
Magnetic force is disappeared between steel disc 9 and suction iron iron plate 8, and umbrella hatchcover 3 is quickly opened in the presence of stage clip 4, discharges extractor parachute and drop
Fall umbrella, complete parachute-opening.
The present invention further technical scheme be：The umbrella hatchcover 3 and unmanned machine frame 12 are be hinged, when umbrella hatchcover 3 is beaten
When opening, under airflow function, umbrella hatchcover 3 is that circumferentially shape starts in axle center with hinge 14, and pulls out extractor parachute and parachute.
The present invention further technical scheme be：The top installation Electromagnetic lock component 13 of the mounting bracket 1, caused by it
Magnetic force tightly holds the suction iron iron plate 8 on umbrella hatchcover 3, reaches the purpose for pinning umbrella hatchcover.
Invention effect
The technical effects of the invention are that：Compact-sized, small volume of the invention, has been effectively saved fuselage space；Utilize
Magnetic adhesion caused by electromagnet tightly pins umbrella hatchcover, it is necessary to during parachute-opening, and flight control computer sends signal, cuts off the electricity supply,
Magnetic adhesion disappears, and stage clip plays a role, while under airflow function, can fast and accurately open umbrella hatchcover；The device is installed
Convenient, reliability height.
Brief description of the drawings
Fig. 1 is background technology unmanned plane parachute automatic-opening mechanism schematic diagram；
Fig. 2 is unmanned plane and unmanned plane umbrella hatchcover automatic-opening mechanism operation principle block diagram；
Fig. 3 is unmanned plane umbrella hatchcover automatic-opening mechanism structure chart；
Fig. 4 is unmanned plane umbrella hatchcover automatic-opening mechanism integral layout schematic diagram；
Description of reference numerals：1- mounting brackets, 2- housings, 3- umbrella hatchcovers, 4- stage clips, 5- screw rods, 6- catch, 7- control circuits
Plate, 8- inhale iron iron plate, 9- silicon steel sheets, 10- coils, 11- screws, the unmanned machine frames of 12-, 13- Electromagnetic lock components, 14- hinges.
15- bulkhead skeletons, 3- umbrella hatchcovers, 17- umbrellas cabin, 18- off line rocking arms, 19- steering wheels, 20- drive shafts, 21- steering wheels are consolidated
Fixed platform.
Embodiment
The technical solution adopted by the present invention is as follows：The unmanned plane umbrella hatchcover automatic-opening mechanism, by being fixed in body
The mounting bracket 1 of portion's framework, the umbrella hatchcover 3 that can be opened and close, suction iron iron plate 8, Electromagnetic lock installed in umbrella hatchcover one end
Component 13, stage clip 4, stud 5, catch 6 and screw 11 form.Characterized in that, mounting bracket 1 is fixed on unmanned plane with screw 11
On framework 12, the top of mounting bracket 1 is installed magnetic force lock body component 13, is engaged with the suction iron iron plate 8 on umbrella hatchcover 3；
Elastic structure is formed in the stud 5, stage clip 4, catch 6 of the installation of the right and left of Electromagnetic lock component 13, stage clip 4 can be along stud
5 are moved up and down；The other end of umbrella hatchcover uses hinge links with unmanned machine frame 12.
The present invention is a kind of unmanned plane umbrella hatchcover automatic-opening mechanism, including mounting bracket 1, housing 2, umbrella hatchcover 3, stage clip 4,
Screw rod 5, catch 6, control board 7, suction iron iron plate 8, silicon steel sheet 9, coil 10, screw 11, unmanned machine frame 12, Electromagnetic lock
Component 13, hinge 14.The mounting bracket 1 is fixed on the framework of internal body by screw 11, and Electromagnetic lock component 13 includes
Housing 2, coil 10, silicon steel sheet 9 and control board 7.Electromagnetic lock housing 2 is fixed on mounting bracket 1 by screw 11, by catch
6 and stage clip 4 penetrate on screw rod 5, screw rod 5 is threadedly secured on mounting bracket 1, is inhaled iron iron plate 8 and is fixed on umbrella hatchcover 3, inhales
Iron iron plate 8 is engaged with the Electromagnetic lock component 13 being fixed on mounting bracket 1.Add on umbrella hatchcover 3 with the opposite position of screw rod 5
Work through hole, making umbrella hatchcover 3, screw rod 5 is by the way that and stage clip 4 is compressed in closure.
Whole system includes height sensor, flight control computer and unmanned plane umbrella hatchcover automatic-opening mechanism；Highly sensing
Device is connected with flight control computer, and flight control computer is connected with unmanned plane umbrella hatchcover automatic-opening mechanism.Before unmanned plane takes off, beat
Parachute-opening hatchcover, parachute is folded by regulation and is put into parachute compartment, and extractor parachute is put into extractor parachute cabin, covers umbrella hatchcover 3
And switch on power, tightly pinned in electromagnetic force subumbrella hatchcover.Unmanned plane take off and execution task during, umbrella hatchcover is located always
In locking state.When unmanned plane, which completes task, to be prepared to land, flying height reduces, and height sensor detection unmanned plane during flying is high
Degree, and the real-time data transmission when the altitude value that flight control computer receives and is preset into height to flight control computer
When being worth consistent, flight control computer sends cut-offing instruction so that the control board 7 in Electromagnetic lock component 13 powers off；After power-off,
The current vanishes of coil 10, magnetic field also disappears simultaneously caused by electric current, and magnetic attraction caused by silicon steel sheet 9 disappears, the He of silicon steel sheet 9
Magnetic force disappears between inhaling iron iron plate 8, and at this moment by the stage clip 4 that umbrella hatchcover 3 compresses, quickly bounce-back jacks up upwards, promotes pad 6 and umbrella
Hatchcover 3 is moved upwards along screw rod 5, and the one end of umbrella hatchcover 3 is upspring, and opens an angle.Aircraft high-speed flight in the air simultaneously, meets
The powerful air-flow in face starts umbrella hatchcover 3 backward, and umbrella hatchcover 3 is that circumferentially shape starts in axle center with hinge 14, and pulls out extractor parachute
And parachute, so as to complete parachute-opening action.
Claims (3)
1. a kind of unmanned plane umbrella hatchcover automatic-opening mechanism, including mounting bracket (1), umbrella hatchcover (3), stage clip (4), catch (6), draw
Pilot chute and parachute；Characterized in that, also include inhaling iron iron plate (8) and Electromagnetic lock component (13)；The Electromagnetic lock component
(13) housing (2), control board (7), silicon steel sheet (9) and coil (10) are included；Electromagnetic lock component (13) is located at mounting bracket
(1) and in the space of umbrella hatchcover (3) formation, it is connected by housing (2) and mounting bracket (1)；Control board (7), silicon steel sheet (9)
It is fixed on coil (10) in housing (2)；Iron iron plate (8) is inhaled to be fixed on umbrella hatchcover (3)；Stud (5) is connected in by screw thread
On mounting bracket (1), stage clip (4) is cased with stud (5), stage clip (4) original state is compressive state；The Electromagnetic lock component
(13) control board (7) in receives outside cut-offing instruction and powered off, the current vanishes of coil (10), caused by electric current
Magnetic field disappears simultaneously, and magnetic attraction caused by silicon steel sheet (9) disappears, and magnetic force disappears between silicon steel sheet (9) and suction iron iron plate (8),
Umbrella hatchcover (3) is quickly opened in the presence of stage clip (4), discharges extractor parachute and parachute, completes parachute-opening.
A kind of 2. unmanned plane umbrella hatchcover automatic-opening mechanism as claimed in claim 1, it is characterised in that the umbrella hatchcover (3)
The other end is connected with unmanned machine frame (12) by hinge (14), when umbrella hatchcover (3) is opened, under airflow function, and umbrella hatchcover
(3) it is that circumferentially shape starts in axle center with hinge (14), and pulls out extractor parachute and parachute.
A kind of 3. unmanned plane umbrella hatchcover automatic-opening mechanism as claimed in claim 1, it is characterised in that the mounting bracket (1)
Top installation Electromagnetic lock component (13), its caused magnetic force tightly holds the suction iron iron plate on umbrella hatchcover (3)
(8) purpose for pinning umbrella hatchcover, is reached.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710553335.XA CN107514185A (en) | 2017-07-08 | 2017-07-08 | A kind of unmanned plane umbrella hatchcover automatic-opening mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710553335.XA CN107514185A (en) | 2017-07-08 | 2017-07-08 | A kind of unmanned plane umbrella hatchcover automatic-opening mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107514185A true CN107514185A (en) | 2017-12-26 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710553335.XA Pending CN107514185A (en) | 2017-07-08 | 2017-07-08 | A kind of unmanned plane umbrella hatchcover automatic-opening mechanism |
Country Status (1)
| Country | Link |
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| CN (1) | CN107514185A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108100265A (en) * | 2018-01-17 | 2018-06-01 | 安徽中骄智能科技有限公司 | A kind of band parachute-type unmanned plane |
| CN109050940A (en) * | 2018-07-20 | 2018-12-21 | 中国航空工业集团公司沈阳飞机设计研究所 | Plane umbrella cabin hood jettison gear and aircraft |
| CN109264002A (en) * | 2018-09-10 | 2019-01-25 | 西安爱生技术集团公司 | A kind of half active opener of unmanned plane recorery parachute of rear power |
| CN109353519A (en) * | 2018-12-06 | 2019-02-19 | 中国科学院工程热物理研究所 | Unmanned plane parachuting Emergency recovery system |
| CN113137138A (en) * | 2020-01-17 | 2021-07-20 | 茂旭资讯股份有限公司 | Magnetic lock with elastic pushing piece to eliminate residual magnetism |
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| EP2692973A1 (en) * | 2012-07-31 | 2014-02-05 | Airbus Operations GmbH | Door alignment and locking system |
| CN203946278U (en) * | 2014-06-11 | 2014-11-19 | 江苏数字鹰科技发展有限公司 | The parachuting umbrella cabin of unmanned plane |
| CN204489193U (en) * | 2014-12-25 | 2015-07-22 | 西安爱生技术集团公司 | Unmanned plane parachute automatic dropping mechanism |
| CN205396549U (en) * | 2016-03-11 | 2016-07-27 | 长春翱天宇智控科技有限公司 | Unmanned aerial vehicle retrieves parachute device |
| CN106184701A (en) * | 2016-08-31 | 2016-12-07 | 河南翱翔航空科技有限公司 | Unmanned plane parachute automatic open device |
| CN206971969U (en) * | 2017-07-08 | 2018-02-06 | 西北工业大学 | A kind of unmanned plane umbrella hatchcover automatic-opening mechanism |
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2017
- 2017-07-08 CN CN201710553335.XA patent/CN107514185A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2692973A1 (en) * | 2012-07-31 | 2014-02-05 | Airbus Operations GmbH | Door alignment and locking system |
| CN203946278U (en) * | 2014-06-11 | 2014-11-19 | 江苏数字鹰科技发展有限公司 | The parachuting umbrella cabin of unmanned plane |
| CN204489193U (en) * | 2014-12-25 | 2015-07-22 | 西安爱生技术集团公司 | Unmanned plane parachute automatic dropping mechanism |
| CN205396549U (en) * | 2016-03-11 | 2016-07-27 | 长春翱天宇智控科技有限公司 | Unmanned aerial vehicle retrieves parachute device |
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| CN206971969U (en) * | 2017-07-08 | 2018-02-06 | 西北工业大学 | A kind of unmanned plane umbrella hatchcover automatic-opening mechanism |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108100265A (en) * | 2018-01-17 | 2018-06-01 | 安徽中骄智能科技有限公司 | A kind of band parachute-type unmanned plane |
| CN109050940A (en) * | 2018-07-20 | 2018-12-21 | 中国航空工业集团公司沈阳飞机设计研究所 | Plane umbrella cabin hood jettison gear and aircraft |
| CN109050940B (en) * | 2018-07-20 | 2022-06-07 | 中国航空工业集团公司沈阳飞机设计研究所 | Aircraft parachute bay cover throwing device and aircraft |
| CN109264002A (en) * | 2018-09-10 | 2019-01-25 | 西安爱生技术集团公司 | A kind of half active opener of unmanned plane recorery parachute of rear power |
| CN109353519A (en) * | 2018-12-06 | 2019-02-19 | 中国科学院工程热物理研究所 | Unmanned plane parachuting Emergency recovery system |
| CN113137138A (en) * | 2020-01-17 | 2021-07-20 | 茂旭资讯股份有限公司 | Magnetic lock with elastic pushing piece to eliminate residual magnetism |
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| Date | Code | Title | Description |
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| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20171226 |
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| RJ01 | Rejection of invention patent application after publication |