CN110371099B - Hovercraft with magnetic suspension function - Google Patents

Hovercraft with magnetic suspension function Download PDF

Info

Publication number
CN110371099B
CN110371099B CN201910736603.0A CN201910736603A CN110371099B CN 110371099 B CN110371099 B CN 110371099B CN 201910736603 A CN201910736603 A CN 201910736603A CN 110371099 B CN110371099 B CN 110371099B
Authority
CN
China
Prior art keywords
hovercraft
motor
coil
pressure sensor
magnetic levitation
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
CN201910736603.0A
Other languages
Chinese (zh)
Other versions
CN110371099A (en
Inventor
叶翠容
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.)
Chang Li
Du Xin
Fu Qianshao
Song Xinzhi
Wang Yuejin
Original Assignee
Fuzhou Jianjinjian Intelligent Technology 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 Fuzhou Jianjinjian Intelligent Technology Co Ltd filed Critical Fuzhou Jianjinjian Intelligent Technology Co Ltd
Priority to CN202011087077.9A priority Critical patent/CN112224195A/en
Priority to CN202011067790.7A priority patent/CN112172777A/en
Priority to CN201910736603.0A priority patent/CN110371099B/en
Publication of CN110371099A publication Critical patent/CN110371099A/en
Application granted granted Critical
Publication of CN110371099B publication Critical patent/CN110371099B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60VAIR-CUSHION VEHICLES
    • B60V3/00Land vehicles, waterborne vessels, or aircraft, adapted or modified to travel on air cushions
    • B60V3/06Waterborne vessels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B43/00Improving safety of vessels, e.g. damage control, not otherwise provided for
    • B63B43/02Improving safety of vessels, e.g. damage control, not otherwise provided for reducing risk of capsizing or sinking
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B45/00Arrangements or adaptations of signalling or lighting devices
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B7/00Collapsible, foldable, inflatable or like vessels
    • B63B7/06Collapsible, foldable, inflatable or like vessels having parts of non-rigid material
    • B63B7/08Inflatable
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H25/00Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
    • B63H25/06Steering by rudders
    • B63H25/08Steering gear
    • B63H25/14Steering gear power assisted; power driven, i.e. using steering engine
    • B63H25/18Transmitting of movement of initiating means to steering engine
    • B63H25/20Transmitting of movement of initiating means to steering engine by mechanical means

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Ocean & Marine Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Vibration Prevention Devices (AREA)
  • Vehicle Body Suspensions (AREA)
  • Automatic Cycles, And Cycles In General (AREA)

Abstract

The invention provides a hovercraft with a magnetic suspension function, which comprises a hovercraft body, wherein the hovercraft body comprises a ship body and an intelligent system, the intelligent system comprises a pressure sensor, an air pressure sensor, a control box, an intelligent processor, a control switch, a power supply device, a first motor, a second motor, an alarm device, a first coil and a second coil, an inflatable cushion is arranged at the bottom of the ship body, a first suspension device is arranged between the inflatable cushion and the ship body, a second suspension device and a third suspension device are respectively arranged at two sides of the first suspension device, a bottom plate is arranged inside the ship body, a fixing frame is arranged between the bottom plate and the ship body, a fixing groove is arranged on the fixing frame, a fixing plate is arranged inside the fixing groove, a box body is arranged at one end of the ship body, a through hole is arranged on the, the hovercraft with the magnetic suspension function is reasonable in design and suitable for popularization.

Description

Hovercraft with magnetic suspension function
Technical Field
The invention relates to the field of hovercraft equipment of a motor boat, in particular to a hovercraft with a magnetic suspension function.
Background
The hovercraft uses high-pressure air to form an air cushion between the bottom of the hovercraft and the water surface or the ground to lift all or part of the hovercraft, thereby greatly reducing the resistance of the hovercraft during navigation, realizing high-speed navigation, and the hovercraft can also travel at very slow speed and hover on the water surface.
Disclosure of Invention
Aiming at the defects in the prior art, the invention aims to provide a hovercraft with a magnetic suspension function, which solves the problems in the background art.
In order to achieve the purpose, the invention is realized by the following technical scheme: a hovercraft with a magnetic suspension function comprises a hovercraft body, wherein the hovercraft body comprises a ship body and an intelligent system, the intelligent system comprises a pressure sensor, a control box, an intelligent processor, a control switch, a power supply device, a first motor, a second motor, an alarm device, a first coil and a second coil, an inflatable cushion is arranged at the bottom of the ship body, a first suspension device is arranged between the inflatable cushion and the ship body, a second suspension device and a third suspension device are respectively arranged on two sides of the first suspension device, a bottom plate is arranged inside the ship body, a fixing frame is arranged between the bottom plate and the ship body, a fixing groove is formed in the fixing frame, a fixing plate is arranged inside the fixing groove, a box body is arranged at one end of the ship body, a through hole is formed in the box body, a mounting plate is arranged inside the, the improved boat body structure is characterized in that a second output shaft is arranged on the first motor, fan blades are arranged on the second output shaft, an installation barrel is welded on one side of the box body, the second motor is arranged on the installation barrel, the first output shaft is arranged on the second motor, a first gear is arranged at the bottom of the first output shaft, a rotating rod is arranged inside the installation barrel, a second gear is arranged on the rotating rod, the first gear is matched with the second gear, a movable plate is welded on the rotating rod, and the control box is arranged inside the boat body.
As a preferred embodiment of the present invention, the control box includes an intelligent processor and a control switch, the intelligent processor includes a circuit board, and a microprocessor and a processing chip disposed on the circuit board, and the microprocessor and the processing chip are connected by a wire.
As a preferred embodiment of the present invention, the control box is electrically connected to the pressure sensor and the air pressure sensor through wires, the control box is electrically connected to the power supply device through wires, and the power supply device is electrically connected to the first motor, the second motor, the alarm device, the first coil and the second coil through wires.
In a preferred embodiment of the present invention, the pressure sensor is mounted on the bottom of the bottom plate, and the air pressure sensor is mounted inside the hull.
In a preferred embodiment of the invention, one end of the ship body is provided with an inflation connector, and the inflation connector is provided with a control valve.
As a preferred embodiment of the present invention, both ends of the rotation lever are fixed inside the installation tub by bearings.
In a preferred embodiment of the present invention, an outer cylinder is disposed at the bottom of the first coil, and an inner cylinder is disposed at the top of the second coil, and the inner cylinder is fixed inside the outer cylinder.
In a preferred embodiment of the present invention, the number of the second suspension devices and the third suspension devices is 2 columns, and the number of the first suspension devices is 1 column.
In a preferred embodiment of the present invention, the hull is provided with a support plate, and the support plate is provided with a fixing lug.
As a preferred embodiment of the present invention, the width of the movable plate matches with the diameter of the installation barrel.
The invention has the beneficial effects that: the invention discloses a hovercraft with a magnetic suspension function, which comprises a hovercraft body, an inflatable cushion, a bottom plate, a fixing frame, a fixing groove, a fixing plate, a box body, an installation barrel, a supporting plate, a fixing lug, an inflatable interface, an installation plate, a first motor, a second motor, a first output shaft, a first gear, a rotating rod, a second gear, a movable plate, a second output shaft, fan blades, a first suspension device, a second suspension device, a third suspension device, a first coil, a second coil, an outer cylinder, an inner cylinder, a pressure sensor, an air pressure sensor, a control box, an intelligent processor, a control switch, a power supply device and an alarm.
1. This hovercraft of magnetic suspension function passes through the suspending device and drives shape change between inflatable packer and the hull, uses under the different situation, when inclining about going on the bottom plate through the user, pressure sensor through to data transmission to intelligent processor on, drive the fly leaf through control switch control motor and carry out rotary motion to change the direction of travel, effectively use manpower sparingly not extravagant.
2. This hovercraft of magnetic suspension function passes through inside baroceptor and inspects the inside atmospheric pressure of hull, and when atmospheric pressure becomes little, baroceptor carries out analysis processes with data transmission to intelligent processor to warn the user through control switch control alarm device, effectively guarantee safe in utilizationly.
3. This hovercraft of magnetic suspension function uses through the suspension device cooperation of three rows, extrudees the shrink through suspension device to the inflatable packer, guarantees to meet the slope that the wave caused when the hull uses, supports the inflatable packer through suspension device to the balance in the guarantee hull traveles, the function is various.
Drawings
Fig. 1 is a schematic structural diagram of a hovercraft with magnetic levitation function according to the present invention;
fig. 2 is a schematic structural diagram of a steering device of a hovercraft with magnetic levitation function according to the invention;
FIG. 3 is a schematic structural diagram of a first motor of a hovercraft with magnetic levitation function according to the present invention;
fig. 4 is a schematic structural diagram of a suspension device of a hovercraft with magnetic suspension function according to the invention;
FIG. 5 is a schematic structural diagram of a coil of a hovercraft with magnetic levitation function according to the present invention;
FIG. 6 is a schematic structural diagram of an intelligent system of a hovercraft with magnetic levitation function according to the present invention;
in the figure: 1-ship body, 2-inflatable cushion, 3-bottom plate, 4-fixing frame, 5-fixing groove, 6-fixing plate, 7-box body, 8-mounting barrel, 9-supporting plate, 10-fixing hanger, 11-inflatable interface, 12-mounting plate, 13-motor I, 14-motor II, 15-output shaft I, 16-gear I, 17-rotating rod, 18-gear II, 19-movable plate, 20-output shaft II, 21-fan blade, 22-suspension device I, 23-suspension device II, 24-suspension device III, 25-coil I, 26-coil II, 27-outer cylinder, 28-inner cylinder, 29-pressure sensor, 30-air pressure sensor, 31-control box, 32-intelligent processor, 33-control switch, 34-power supply device and 35-alarm device.
Detailed Description
In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the invention easy to understand, the invention is further described with the specific embodiments.
Referring to fig. 1 to 6, the present invention provides a technical solution: a hovercraft with a magnetic suspension function comprises a hovercraft body, wherein the hovercraft body comprises a hull 1 and an intelligent system, the intelligent system comprises a pressure sensor 29, an air pressure sensor 30, a control box 31, an intelligent processor 32, a control switch 33, a power supply device 34, a first motor 13, a second motor 14, an alarm device 35, a first coil 25 and a second coil 26, an inflatable cushion 2 is arranged at the bottom of the hull 1, a first suspension device 22 is arranged between the inflatable cushion 2 and the hull 1, two sides of the first suspension device 22 are respectively provided with a second suspension device 23 and a third suspension device 24, a bottom plate 3 is arranged inside the hull 1, a fixing frame 4 is arranged between the bottom plate 3 and the hull 1, a fixing groove 5 is arranged on the fixing frame 4, a fixing plate 6 is arranged inside the fixing groove 5, and a box body 7 is arranged at one end of the hull 1, be provided with the through-hole on the box 7, the inside of through-hole is provided with mounting panel 12, install on mounting panel 12 motor one 13, be provided with two 20 of output shaft on the motor one 13, install fan blade 21 on two 20 of output shaft, one side welding of box 7 has installation bucket 8, two 14 of motors are installed on installation bucket 8, be provided with output shaft one 15 on two 14 of motors, the bottom of output shaft one 15 is provided with gear one 16, the inside of installation bucket 8 is provided with dwang 17, be provided with gear two 18 on the dwang 17, gear one 16 cooperatees with gear two 18, the welding has fly leaf 19 on dwang 17, the inside at hull 1 is installed to control box 31.
As a preferred embodiment of the present invention, the control box 31 includes an intelligent processor 32 and a control switch 33, and the intelligent processor 32 includes a circuit board, and a microprocessor and a processing chip disposed on the circuit board, and the microprocessor and the processing chip are connected by a wire.
In a preferred embodiment of the present invention, the control box 31 is electrically connected to the pressure sensor 29 and the air pressure sensor 30 through wires, the control box 31 is electrically connected to the power supply device 34 through wires, and the power supply device 34 is electrically connected to the first motor 13, the second motor 14, the alarm device 35, the first coil 25 and the second coil 26 through wires.
In a preferred embodiment of the present invention, the pressure sensor 29 is installed at the bottom of the bottom plate 3, and the air pressure sensor 30 is installed inside the hull 1.
In a preferred embodiment of the present invention, an inflation connector 11 is provided at one end of the hull 1, and a control valve is provided on the inflation connector 11.
In a preferred embodiment of the present invention, both ends of the rotating rod 17 are fixed inside the installation barrel 8 through bearings.
In a preferred embodiment of the present invention, an outer cylinder 27 is disposed at the bottom of the first coil 25, an inner cylinder 28 is disposed at the top of the second coil 26, and the inner cylinder 28 is fixed inside the outer cylinder 27.
In a preferred embodiment of the present invention, the number of the second suspension devices 23 and the third suspension devices 24 is 2 columns, and the number of the first suspension devices 22 is 1 column.
In a preferred embodiment of the present invention, the hull 1 is provided with a support plate 9, and the support plate 9 is provided with a fixing lug 10.
In a preferred embodiment of the present invention, the width of the movable plate 19 matches the diameter of the installation barrel 8.
The working principle is as follows: the device provides required electric energy for electrical appliances inside the device through an internal power supply device 34, when the device is used, firstly, the ship body 1 and the inflatable cushion 2 are inflated through the inflatable connector 11 for use, after inflation is completed, the inflatable connector 11 is closed through a control valve so as to ensure that gas is not leaked, after inflation is completed, the fixing plate 6 and the fixing groove 5 on the fixing frame 4 are installed on the bottom plate 3 for supporting between the ship bodies 1, when the device is used, the motor I13 is controlled to work through the control switch 33, the motor I13 drives the fan blades 21 to rotate inside the installation barrel 8 through the output shaft II 20 to form thrust for driving the ship body 1 to move, when the driving direction of the ship body 1 needs to be changed, pressure is monitored through slight left and right inclination on the fixing plate 6 of the ship body 1, pressure sensors 29 on two sides monitor the pressure, data are transmitted to the intelligent processor 32 for analysis and processing after the pressure is monitored, the motor II 14 is controlled to work through the control switch 33, the motor II 14 drives the gear I16 to rotate, the gear II 18 is matched with the gear II to drive the movable plate 19 on the rotating rod 17 to rotate while the movable plate 19 rotates, the direction of thrust is changed while the movable plate 19 rotates, so that the change of the direction is completed, unnecessary waste of manpower is effectively saved, when the contact area of the ship body 1 and the water surface needs to be changed for fast running, the suspension device I22, the suspension device II 23 and the suspension device III 24 are electrified, the current of the suspension device I22 is larger than the current of the suspension device II 23 and the suspension device III 24 on two sides, the coil II 26 on the suspension device I22 is larger than the distance between the suspension device II 23 and the suspension device III 24, so that the inflatable cushion 2 forms a triangular shape with a high middle part, the contact area with the water is reduced, and the running speed of the, in addition, when the ship body 1 inclines, the pressure sensor 29 transmits data to the intelligent processor 32 for analysis processing, when one side of the second suspension device 23 inclines, the first coil 25 and the second coil 26 in the second suspension device 23 are electrified to support the inflatable cushion 2, so that balance is kept, use safety is guaranteed, internal air pressure in the ship body 1 is monitored through the air pressure sensor 30, when the internal air pressure changes, the data is transmitted to the intelligent processor 32 for analysis processing, and the alarm device 35 is controlled through the control switch 33 to give an alarm for reminding, so that the use safety is increased.
While there have been shown and described what are at present considered the fundamental principles and essential features of the invention and its advantages, it will be apparent to those skilled in the art that the invention is not limited to the details of the foregoing exemplary embodiments, but is capable of other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.

Claims (10)

1. The utility model provides a hovercraft of magnetic suspension function, includes the hovercraft body, its characterized in that: the hovercraft body comprises a hovercraft body (1) and an intelligent system, wherein the intelligent system comprises a pressure sensor (29), an air pressure sensor (30), a control box (31), an intelligent processor (32), a control switch (33), a power supply device (34), a first motor (13), a second motor (14), an alarm device (35), a first coil (25) and a second coil (26), an inflatable cushion (2) is arranged at the bottom of the hovercraft body (1), a first suspension device (22) is arranged between the inflatable cushion (2) and the hovercraft body (1), two sides of the first suspension device (22) are respectively provided with a second suspension device (23) and a third suspension device (24), a bottom plate (3) is arranged inside the hovercraft body (1), a fixing frame (4) is arranged between the bottom plate (3) and the hovercraft body (1), and a fixing groove (5) is arranged on the fixing frame, the inside of fixed slot (5) is provided with fixed plate (6), the one end of hull (1) is provided with box (7), be provided with the through-hole on box (7), the inside of through-hole is provided with mounting panel (12), install on mounting panel (12) motor (13), be provided with output shaft two (20) on motor (13), install fan blade (21) on output shaft two (20), the welding of one side of box (7) has installation bucket (8), motor two (14) are installed on installation bucket (8), be provided with output shaft one (15) on motor two (14), the bottom of output shaft one (15) is provided with gear one (16), the inside of installation bucket (8) is provided with dwang (17), be provided with gear two (18) on dwang (17), gear one (16) and gear two (18) cooperate, the welding has fly leaf (19) on dwang (17), the inside at hull (1) is installed in control box (31).
2. A hovercraft with magnetic levitation function as claimed in claim 1, wherein: the control box (31) comprises an intelligent processor (32) and a control switch (33), wherein the intelligent processor (32) comprises a circuit main board, and a microprocessor and a processing chip which are arranged on the circuit main board and connected through an electric wire.
3. A hovercraft with magnetic levitation function as claimed in claim 1, wherein: the control box (31) is electrically connected with the pressure sensor (29) and the air pressure sensor (30) through electric wires, the control box (31) is electrically connected with the power supply device (34) through electric wires, and the power supply device (34) is electrically connected with the first motor (13), the second motor (14), the alarm device (35), the first coil (25) and the second coil (26) through electric wires.
4. A hovercraft with magnetic levitation function as claimed in claim 1, wherein: the pressure sensor (29) is arranged at the bottom of the bottom plate (3), and the air pressure sensor (30) is arranged inside the ship body (1).
5. A hovercraft with magnetic levitation function as claimed in claim 1, wherein: an inflation connector (11) is arranged at one end of the ship body (1), and a control valve is arranged on the inflation connector (11).
6. A hovercraft with magnetic levitation function as claimed in claim 1, wherein: the two ends of the rotating rod (17) are fixed in the installation barrel (8) through bearings.
7. A hovercraft with magnetic levitation function as claimed in claim 1, wherein: an outer cylinder (27) is arranged at the bottom of the first coil (25), an inner cylinder (28) is arranged at the top of the second coil (26), and the inner cylinder (28) is fixed inside the outer cylinder (27).
8. A hovercraft with magnetic levitation function as claimed in claim 1, wherein: the number of the second suspension devices (23) and the third suspension devices (24) is 2 columns, and the number of the first suspension devices (22) is 1 column.
9. A hovercraft with magnetic levitation function as claimed in claim 1, wherein: the boat body (1) is provided with a supporting plate (9), and the supporting plate (9) is provided with a fixing hanger (10).
10. A hovercraft with magnetic levitation function as claimed in claim 1, wherein: the width of the movable plate (19) is matched with the diameter of the mounting barrel (8).
CN201910736603.0A 2019-08-09 2019-08-09 Hovercraft with magnetic suspension function Active CN110371099B (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
CN202011087077.9A CN112224195A (en) 2019-08-09 2019-08-09 Hovercraft with detectable magnetic suspension function
CN202011067790.7A CN112172777A (en) 2019-08-09 2019-08-09 Hovercraft based on magnetic suspension
CN201910736603.0A CN110371099B (en) 2019-08-09 2019-08-09 Hovercraft with magnetic suspension function

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910736603.0A CN110371099B (en) 2019-08-09 2019-08-09 Hovercraft with magnetic suspension function

Related Child Applications (2)

Application Number Title Priority Date Filing Date
CN202011087077.9A Division CN112224195A (en) 2019-08-09 2019-08-09 Hovercraft with detectable magnetic suspension function
CN202011067790.7A Division CN112172777A (en) 2019-08-09 2019-08-09 Hovercraft based on magnetic suspension

Publications (2)

Publication Number Publication Date
CN110371099A CN110371099A (en) 2019-10-25
CN110371099B true CN110371099B (en) 2020-12-01

Family

ID=68258915

Family Applications (3)

Application Number Title Priority Date Filing Date
CN202011087077.9A Withdrawn CN112224195A (en) 2019-08-09 2019-08-09 Hovercraft with detectable magnetic suspension function
CN201910736603.0A Active CN110371099B (en) 2019-08-09 2019-08-09 Hovercraft with magnetic suspension function
CN202011067790.7A Withdrawn CN112172777A (en) 2019-08-09 2019-08-09 Hovercraft based on magnetic suspension

Family Applications Before (1)

Application Number Title Priority Date Filing Date
CN202011087077.9A Withdrawn CN112224195A (en) 2019-08-09 2019-08-09 Hovercraft with detectable magnetic suspension function

Family Applications After (1)

Application Number Title Priority Date Filing Date
CN202011067790.7A Withdrawn CN112172777A (en) 2019-08-09 2019-08-09 Hovercraft based on magnetic suspension

Country Status (1)

Country Link
CN (3) CN112224195A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112206110B (en) * 2020-09-25 2022-02-22 泗县微腾知识产权运营有限公司 Movable air cushion

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2219040A2 (en) * 1973-02-26 1974-09-20 Boulch Claude
DE4126453A1 (en) * 1991-08-09 1993-02-11 Withold Richert TRACKED TRANSPORT VEHICLE
CN205150186U (en) * 2015-11-30 2016-04-13 刘文敏 High steamer of security
CN205203001U (en) * 2015-12-18 2016-05-04 安溪县凤城建金产品外观设计服务中心 Keep out wind and prevent sinking formula M type aircushion vehicle
CN108312891A (en) * 2018-03-26 2018-07-24 江苏理工学院 A kind of intelligent automobile of equipment magnetic suspension wheel

Also Published As

Publication number Publication date
CN112172777A (en) 2021-01-05
CN110371099A (en) 2019-10-25
CN112224195A (en) 2021-01-15

Similar Documents

Publication Publication Date Title
CN110371099B (en) Hovercraft with magnetic suspension function
CN108583182B (en) Air-land amphibious spherical robot
CN103786879A (en) Variable-pitch aircraft
CN201686015U (en) Remote airship propulsion device
CN103786878A (en) Multi-shaft aircraft
JP2016188770A (en) Propeller characteristics measuring apparatus
KR101617763B1 (en) Verticle axis wind turbine including apparatus for controlling pitch angle of turbine blades simulataneously
CN203753398U (en) Multi-axis aircraft
CN116605388B (en) Underwater vector propeller driven by single motor and vector device thereof
CN105626362B (en) A kind of wave energy lighthouse
CN209320730U (en) Vehicular charging vehicle-mounted charging device
CN211853340U (en) Monitoring device and monitoring system
CN214985726U (en) 5G heavy-duty wall climbing robot with built-in gyroscope and high-definition monitoring
CN205768419U (en) It is applicable to aeroamphibious aircraft
CN208216989U (en) A kind of multi-rotor unmanned aerial vehicle with searchlighting function
CN112693441A (en) Hovercraft with spiral propelling function
CN215265184U (en) Unmanned aerial vehicle drives teaching equipment
CN108820234A (en) A kind of multi-rotor unmanned aerial vehicle with searchlighting function
CN221067697U (en) Anti-tipping amphibious aircraft
CN213200133U (en) Many rotor unmanned aerial vehicle keep away barrier device
CN220032229U (en) Unmanned aerial vehicle patrols and examines that figure is accurate to be obtained
CN110116597A (en) Multitask environment quadrotor with the raw electricity of magnetic
CN203666985U (en) Variable-pitch aircraft
CN217198637U (en) Four rotor unmanned aerial vehicle with vector thrust function
CN219142969U (en) Electric field sensing device

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
TA01 Transfer of patent application right

Effective date of registration: 20201111

Address after: Room 2-88h, building 1, No.27 Huli Road, Mawei District, Fuzhou City, Fujian Province, 350015 (within the pilot Free Trade Zone)

Applicant after: Fuzhou jianjinjian Intelligent Technology Co.,Ltd.

Address before: 233000 408, 4 / F, Ande complex, Chung Ping Street, Bengbu, Anhui.

Applicant before: BENGBU CITY CIRCULATION RATE ELECTRONIC TECHNOLOGY Co.,Ltd.

TA01 Transfer of patent application right
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20240626

Address after: No. 31, Gate 2, 58th Floor, No. 19 West Third Ring Middle Road, Haidian District, Beijing, 100080

Patentee after: Wang Yuejin

Country or region after: China

Patentee after: Du Xin

Patentee after: Fu Qianshao

Patentee after: Chang Li

Patentee after: Song Xinzhi

Address before: Room 2-88H, Building 1, No. 27 Huli Road, Mawei District, Fuzhou City, Fujian Province (within the Free Trade Zone)

Patentee before: Fuzhou jianjinjian Intelligent Technology Co.,Ltd.

Country or region before: China

TR01 Transfer of patent right