CN206971969U - A kind of unmanned plane umbrella hatchcover automatic-opening mechanism - Google Patents

A kind of unmanned plane umbrella hatchcover automatic-opening mechanism Download PDF

Info

Publication number
CN206971969U
CN206971969U CN201720820915.6U CN201720820915U CN206971969U CN 206971969 U CN206971969 U CN 206971969U CN 201720820915 U CN201720820915 U CN 201720820915U CN 206971969 U CN206971969 U CN 206971969U
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.)
Active
Application number
CN201720820915.6U
Other languages
Chinese (zh)
Inventor
李春
曹春艳
马斌
任春鹤
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Northwestern Polytechnical University
Xian Aisheng Technology Group Co Ltd
Original Assignee
Northwestern Polytechnical University
Xian Aisheng Technology Group Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Northwestern Polytechnical University, Xian Aisheng Technology Group Co Ltd filed Critical Northwestern Polytechnical University
Priority to CN201720820915.6U priority Critical patent/CN206971969U/en
Application granted granted Critical
Publication of CN206971969U publication Critical patent/CN206971969U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Holders For Apparel And Elements Relating To Apparel (AREA)

Abstract

It the utility model is related 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 utility model 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

A kind of unmanned plane umbrella hatchcover automatic-opening mechanism
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.
CN201720820915.6U 2017-07-08 2017-07-08 A kind of unmanned plane umbrella hatchcover automatic-opening mechanism Active CN206971969U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720820915.6U CN206971969U (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
CN201720820915.6U CN206971969U (en) 2017-07-08 2017-07-08 A kind of unmanned plane umbrella hatchcover automatic-opening mechanism

Publications (1)

Publication Number Publication Date
CN206971969U true CN206971969U (en) 2018-02-06

Family

ID=61406468

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720820915.6U Active CN206971969U (en) 2017-07-08 2017-07-08 A kind of unmanned plane umbrella hatchcover automatic-opening mechanism

Country Status (1)

Country Link
CN (1) CN206971969U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107514185A (en) * 2017-07-08 2017-12-26 西北工业大学 A kind of unmanned plane umbrella hatchcover automatic-opening mechanism

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107514185A (en) * 2017-07-08 2017-12-26 西北工业大学 A kind of unmanned plane umbrella hatchcover automatic-opening mechanism

Similar Documents

Publication Publication Date Title
CN107514185A (en) A kind of unmanned plane umbrella hatchcover automatic-opening mechanism
CN207889993U (en) A kind of multi-rotor unmanned aerial vehicle including parachute construction
CN106394882B (en) A kind of chute-type unmanned plane skid jack
CN104527984A (en) Automatic parachute falling mechanism of unmanned aerial vehicle
US20090321559A1 (en) Aircraft noise reduction apparatus
CN108116668A (en) The land and air double-used more rotor manned aircraft of full electricity
CN209506075U (en) A kind of unmanned plane undercarriage
CN105109694B (en) A kind of anti-fall aircraft and anti-fall control method
CN206971969U (en) A kind of unmanned plane umbrella hatchcover automatic-opening mechanism
CN108482685A (en) Unmanned plane recovery system, unmanned plane and recovery method
CN109455302A (en) A kind of Emergency recovery umbrella system suitable for medium-and-large-sized unmanned plane
CN105539849B (en) A kind of electronic gondola of external hanging type aviation and application method
CN108674669A (en) A kind of unmanned plane that fail-safe is crashed
CN106184701A (en) Unmanned plane parachute automatic open device
CN110017065A (en) A kind of stealthy unmanned engine room cover locking mechanism of flying wing type layout
CN107826264A (en) A kind of vehicle-mounted unmanned aerial vehicle landing control system and its control method
CN108016616A (en) A kind of unmanned plane protection system based on modularized design
CN106314802A (en) Parachute bay device for unmanned aerial vehicle and unmanned aerial vehicle
CN206068176U (en) A kind of nacelle arrangement of fixed-wing aerial survey unmanned plane
CN106275391B (en) The disengaged land undercarriage of aircraft
CN206766338U (en) One kind stops stable unmanned plane
CN110963048B (en) System and method for verifying unlimited-quality parachute opening strength of parachute
CN205273879U (en) Safe seat above aircraft
CN108058833A (en) A kind of list rotor unmanned helicopter parachute landing system
CN107444632A (en) It is a kind of can VTOL dalta wing unmanned plane

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant