CN111204453A - Large-load unmanned aerial vehicle rescue device - Google Patents
Large-load unmanned aerial vehicle rescue device Download PDFInfo
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- CN111204453A CN111204453A CN202010221201.XA CN202010221201A CN111204453A CN 111204453 A CN111204453 A CN 111204453A CN 202010221201 A CN202010221201 A CN 202010221201A CN 111204453 A CN111204453 A CN 111204453A
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- rescue
- aerial vehicle
- unmanned aerial
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- rescue cabin
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- 238000009434 installation Methods 0.000 claims description 13
- 229910003460 diamond Inorganic materials 0.000 claims description 2
- 239000010432 diamond Substances 0.000 claims description 2
- 230000005389 magnetism Effects 0.000 claims description 2
- 230000006378 damage Effects 0.000 abstract description 4
- 238000004519 manufacturing process Methods 0.000 abstract description 3
- 208000027418 Wounds and injury Diseases 0.000 description 2
- 208000014674 injury Diseases 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000007789 sealing Methods 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- 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
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/22—Taking-up articles from earth's surface
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Lowering Means (AREA)
Abstract
A rescue device of a heavy-load unmanned aerial vehicle comprises the heavy-load unmanned aerial vehicle, a rescue cabin, an equipment frame, a winch, a pulley block and a remote control locking part, can be used for aerial rapid rescue in emergency states such as war, natural disasters, epidemic situations and the like, does not need pilot driving due to the adoption of the unmanned aerial vehicle flight technology, can get into any danger, unknown area expandes the rescue, unmanned aerial vehicle need not to descend, can suspend and put down the rescue cabin in the air, wait to need the rescue personnel to get into and lift up the rescue cabin through the capstan winch after the rescue cabin, fix in unmanned aerial vehicle bottom through the remote control electronic lock when arriving the highest point, this device can fix the rescue cabin in the unmanned aerial vehicle bottom, flight is steady, very big guarantee that the wounded can not receive the secondary damage, take comfortablely, safety, the cost of manufacture is low, can use manpower sparingly, financial resources, also can solve present aerial rescue resource shortage problem.
Description
Technical Field
An air rescue device belongs to the field of flight, and particularly relates to an air rescue device and a mode.
Background
The existing emergency rescue device is limited by the environment, disasters and traffic, timely rescue is often not achieved, the existing air rescue at home and abroad is limited by the number of helicopters and pilots, the high manufacturing cost of the helicopters and the difficulty of pilot culture are not solved, the helicopter is not popularized and applied, no helicopter equipment exists in most urban areas, the high cost and the low utilization rate are important reasons for the popularization of the helicopter rescue, the existing helicopter rescue device is too simple in structure, the probability of secondary injury is high in the rescue process, multiple helicopters are generated at home and abroad to cause secondary injury or even death of rescuers, and the problem that the rescue device is too simple is solved.
Disclosure of Invention
In view of the above, the invention is a large-load unmanned aerial vehicle rescue device, and in order to solve the above problems, the technical scheme of the invention is as follows: this device includes big load unmanned aerial vehicle (1), rescue cabin (2), equipment rack (3), capstan winch (4), assembly pulley (5), remote control locking part, this device can be used to the war, natural disasters, the aerial quick rescue under emergency such as epidemic situation, unmanned aerial vehicle need not to descend, can suspend and put down rescue cabin (2) in the air, wait to need the salvage personnel to get into after rescue cabin (2) and lift up rescue cabin (2) through capstan winch (4), flight is steady, very big guarantee that the wounded can not receive the secondary damage, take comfortablely, safety, the cost of manufacture is low, can use manpower sparingly, financial resources, also can solve present aerial rescue resource shortage problem.
Rescue cabin (2) and unmanned aerial vehicle (1) adopt detachable, outer cabin body installation GPS (7) and night flashing lamp (8), convenient location is look for, install U type becket (9) in the middle of rescue cabin (2) top, the horizontal line increase friction in top, bellied square magnet (10) are inlayed to U type becket (9) both sides, rescue cabin (2) adopt the design of opening the door, adopt two lock (11) guarantee safety, rescue cabin (2) body top both sides installation triangle-shaped cabin frame (12), cabin frame (12) top installation ring (13), the ring inner ring is threaded, be used for and couple inseparable combination do not have the slip.
Equipment frame (3) adopt bilayer structure, first layer installation capstan winch (4) and left and right sides capstan winch rope guide (14), circular port (22) are opened to the both sides about the equipment frame, the remote control lock (15) of customization is installed on the second floor, recess installation electromagnetism board (16) are opened to the both sides of remote control lock and are relative with the bellied magnet (10) position in rescue cabin (2), magnetism attracts mutually, U type becket (9) just correspond remote control lock (15) below. The capstan winch is for customizing single motor double rotary table structure, and double rotary table drives the assembly pulley about respectively.
Pulley block (5) adopt two fixed pulley (18) single wheel (19) structure to constitute, two sets of assembly pulley (5) in both sides, and four fixed pulley (18) are fixed in equipment rack (3) both sides, unmanned aerial vehicle (1) bottom, four-point atress carry rescue cabin (2), and rope guide (20) are installed to leftmost and rightmost fixed pulley, and guarantee rescue cabin (2) rise to accurate position.
The movable pulley (19) is welded with a diamond frame by taking a wheel axle as a diagonal line, the upper end of the movable pulley is connected with a winch rope (23), and the lower end of the movable pulley is connected with a D-shaped buckle (21).
The rescue unmanned aerial vehicle (1) and the rescue cabin (2) can be used separately, when the rescue cabin (2) is available, a wounded person only needs to lie in the rescue cabin (2) to wait for rescue, the flashing lamp (8) is turned on at night to be conveniently found, after the unmanned aerial vehicle (1) reaches an accurate position, the D-shaped buckle (21) is connected with the circular ring (13) on the rescue cabin (2), the rescue cabin (2) is lifted to the position below the unmanned aerial vehicle (1) by opening the winch (4), the rescue cabin (2) is fixed through the two pairs of electromagnetic locks (16), the rescue cabin (2) can be rewound by locking the remote control lock (15), when the rescue cabin (2) is not available, the unmanned aerial vehicle (1) can carry the rescue cabin (2) to go to rescue, when the unmanned aerial vehicle reaches a rescue ground, the winch (4) is started to tighten up, the remote control lock (15) is opened, then the rescue cabin (2) is put down to a proper position, after the wounded person enters the rescue cabin (, the rescue cabin (2) is fixed through two pairs of electromagnetic locks (15), and the rescue cabin can return to the home by locking the remote control locks (15).
Drawings
Fig. 1 is an axial view of a heavy-load unmanned aerial vehicle rescue device.
Fig. 2 is a bottom view of a rescue device equipment frame of a heavy-load unmanned aerial vehicle.
Fig. 3 is a capstan axis view of a large-load unmanned aerial vehicle rescue device.
Fig. 4 is a side view of a rescue cabin of a large-load unmanned aerial vehicle rescue device.
Fig. 5 is a top view of a rescue cabin of a large-load unmanned aerial vehicle rescue device.
Detailed Description
In consideration of the requirement of large load capacity of the unmanned aerial vehicle (1), the load capacity of the unmanned aerial vehicle (1) is more than 200 kg.
Triangular cabin frames (12) are installed on two sides above the rescue cabin (2), the bottom edges of the cabin frames (12) are fixed on four corners above the rescue cabin and can be folded by 90 degrees, a ring (13) is installed at the top end, the grain and the size of the inner ring of the ring are matched with a D-shaped buckle (21), the total height, the D-shaped buckle (21) and a pulley block (5) are equal to the height of the equipment frame (3), the rescue cabin (2) is just matched with the equipment frame (2) when lifted to the highest position, flashing lamps (8) are installed at four corners of the rescue cabin (2) to facilitate locking at night, a GPS device (7) is installed above the rescue cabin, the rapid locking position is convenient to separate for use, a U-shaped metal ring (9) is installed at the center position above the rescue cabin (2), a remote control lock (15) corresponding to the equipment frame is corresponding to the U-shaped metal ring (9), convex square electromagnetic lock female plates (10) are, the rescue cabin (2) adopts a side-opening door design, and the door lock (11) opens the door from the upper part to the lower part.
Equipment frame (3) divide two-layer design, rope guider (14) about first layer installation capstan winch (4) and the capstan winch, trompil (22) are qualified for the next round of competitions about equipment frame (3) first layer, sunken electronic lock (16) of installation about the second layer, the size corresponds bellied magnet master (10) in rescue cabin (2), installation customization remote control lock (15) in the middle of equipment frame (3), sunken U type becket (9) on corresponding the rescue cabin in the middle of remote control lock (15), treat that the lock core can pass U type becket (9) and lock when U type becket (9) combine.
The winch (4) is customized to have a structure with a single motor (16) and double rotating discs (17), the pulling force of the motor is about 1000 pounds, and the double discs (17) respectively drive the left and right pulley blocks (5) to enable the left and right pulley blocks (5) to ascend synchronously.
The pulley block (5) adopts a design of double fixed wheels (18) and a driving wheel (19) to reduce the tension of the winch (4), a rope guide (20) is fixedly arranged at the leftmost side and the rightmost side, a connecting line of the rope guide and the driving wheel (19) is vertical to the plane of the rescue cabin (2), and a rope (23) is prevented from dragging the pulley by sealing the lower part of the driving wheel (19).
The invention has the advantages that: the problem of rapid and safe rescue under emergency is solved by combining the unmanned aerial vehicle and the rescue cabin; the unmanned aerial vehicle rescue device is low in overall cost and use limitation, and does not need a professional pilot to drive; adopt unmanned aerial vehicle autopilot technique, can overcome the puzzlement that unusual weather brought, like big fog, unknown danger area, battlefield etc..
Claims (7)
1. The utility model provides a big load unmanned aerial vehicle rescue device which characterized in that: the device comprises a heavy-load unmanned aerial vehicle (1), a rescue cabin (2), an equipment frame (3), a winch (4), a pulley block (5) and a remote control locking part.
2. A heavy load unmanned aerial vehicle rescue apparatus as claimed in claim 1, wherein: rescue cabin (2) and unmanned aerial vehicle (1) adopt detachable, outer cabin body installation GPS (7) and night flashing lamp (8), convenient location is look for, install in the middle of rescue cabin (2) top and fall U type becket (9), the horizontal line increase friction in top, bellied square magnet (10) are inlayed to U type becket (9) both sides, rescue cabin (2) adopt the design of side opening door, adopt two lock (11) guarantee safety, rescue cabin (2) body top both sides installation triangle-shaped cabin frame (12), cabin frame (12) top installation ring (13), the ring inner ring has the screw thread, be used for and couple inseparable combination do not have the slip.
3. A heavy load unmanned aerial vehicle rescue apparatus as claimed in claim 1, wherein: equipment frame (3) adopt bilayer structure, first layer installation capstan winch (4) and left and right sides capstan winch cord guide (14), circular port (22) are opened to the both sides of the equipment frame left and right sides, the remote control lock (15) of customization is installed on the second floor, recess installation electromagnetism board (16) are opened to the remote control lock both sides and are relative with the bellied magnet (10) position in rescue cabin (2), magnetism attracts mutually, U type becket (9) just correspond remote control lock (15) below.
4. A heavy load unmanned aerial vehicle rescue apparatus as claimed in claim 1, wherein: the winch (4) is of a customized single-motor (16) double-turntable (17) structure, and the double-turntable (17) drives the left pulley block and the right pulley block (5) respectively.
5. A heavy load unmanned aerial vehicle rescue apparatus as claimed in claim 1, wherein: pulley block (5) adopt two fixed pulley (18) single wheel (19) structure to constitute, two sets of assembly pulley (5) in both sides, four fixed pulley (18) are fixed in equipment rack (3) both sides, unmanned aerial vehicle (1) bottom, four-point atress carry rescue cabin (2), rope guide (20) are installed to leftmost and rightmost fixed pulley, guarantee rescue cabin (2) rise to accurate position.
6. A heavy load unmanned aerial vehicle rescue apparatus as claimed in claim 5, wherein: the movable pulley (19) uses a wheel axle as a diagonal line to weld the diamond frame, the upper end of the movable pulley is connected with the winch rope (20), and the lower end of the movable pulley is connected with the D-shaped buckle (21).
7. A heavy load unmanned aerial vehicle rescue apparatus as claimed in claim 1, wherein: the rescue unmanned aerial vehicle (1) and the rescue cabin (2) can be used separately, when the rescue cabin (2) is available, a wounded person only needs to lie in the rescue cabin (2) to wait for rescue, the flashing lamp (8) is turned on at night to be conveniently found, after the unmanned aerial vehicle (1) reaches an accurate position, the D-shaped buckle (21) is connected with the circular ring (13) on the rescue cabin (2), the rescue cabin (2) is lifted to the position below the unmanned aerial vehicle (1) by opening the winch (4), the rescue cabin (2) is fixed through the two pairs of electromagnetic locks (16), the rescue cabin (2) can be rewound by locking the remote control lock (15), when the rescue cabin (2) is not available, the unmanned aerial vehicle (1) can carry the rescue cabin (2) to go forward for rescue, when the wounded person reaches a rescue place, the remote control winch (4) is started to tighten, the remote control lock (15) is opened, then the rescue cabin (2) is put down to a proper position, after the wounded person enters the rescue cabin (2, the rescue cabin (2) is fixed through two pairs of electromagnetic locks (15), and the rescue cabin can return to the home by locking the remote control locks (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010221201.XA CN111204453A (en) | 2020-03-26 | 2020-03-26 | Large-load unmanned aerial vehicle rescue device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010221201.XA CN111204453A (en) | 2020-03-26 | 2020-03-26 | Large-load unmanned aerial vehicle rescue device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111204453A true CN111204453A (en) | 2020-05-29 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010221201.XA Pending CN111204453A (en) | 2020-03-26 | 2020-03-26 | Large-load unmanned aerial vehicle rescue device |
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| Country | Link |
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| CN (1) | CN111204453A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2024142267A1 (en) * | 2022-12-27 | 2024-07-04 | 株式会社クボタ | Flying object |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB755965A (en) * | 1953-11-19 | 1956-08-29 | Fairey Aviat Co Ltd | Improvements relating to rotary wing aircraft |
| US3934847A (en) * | 1974-10-04 | 1976-01-27 | Bentivegna Pasquale P | Rescue capsule for use with a helicopter |
| US4152019A (en) * | 1977-09-06 | 1979-05-01 | Challe Gilles A | Material handling system |
| DE3323513A1 (en) * | 1983-06-30 | 1985-01-10 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt | Winch for aircraft |
| US5826825A (en) * | 1994-04-12 | 1998-10-27 | Gabriel; Edwin Zenith | Automatically actuated cargo and personnel snatching apparatus with distance sensos, magnets and pivot pins for assistance |
| CN101289116A (en) * | 2007-04-20 | 2008-10-22 | 张国成 | One man relief helicopter |
| CN101823559A (en) * | 2009-03-02 | 2010-09-08 | 林建斌 | Lifting rescue cabin of military aircraft |
| US20120145832A1 (en) * | 2009-06-23 | 2012-06-14 | Matthias Schuster | Load lifting apparatus for a helicopter and helicopter |
| CN105083554A (en) * | 2014-05-14 | 2015-11-25 | 空客直升机德国有限公司 | External load mass rope of a rotorcraft |
| CN107108031A (en) * | 2015-11-03 | 2017-08-29 | 以色列宇航工业有限公司 | Hovering flight device and its control method |
-
2020
- 2020-03-26 CN CN202010221201.XA patent/CN111204453A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB755965A (en) * | 1953-11-19 | 1956-08-29 | Fairey Aviat Co Ltd | Improvements relating to rotary wing aircraft |
| US3934847A (en) * | 1974-10-04 | 1976-01-27 | Bentivegna Pasquale P | Rescue capsule for use with a helicopter |
| US4152019A (en) * | 1977-09-06 | 1979-05-01 | Challe Gilles A | Material handling system |
| DE3323513A1 (en) * | 1983-06-30 | 1985-01-10 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt | Winch for aircraft |
| US5826825A (en) * | 1994-04-12 | 1998-10-27 | Gabriel; Edwin Zenith | Automatically actuated cargo and personnel snatching apparatus with distance sensos, magnets and pivot pins for assistance |
| CN101289116A (en) * | 2007-04-20 | 2008-10-22 | 张国成 | One man relief helicopter |
| CN101823559A (en) * | 2009-03-02 | 2010-09-08 | 林建斌 | Lifting rescue cabin of military aircraft |
| US20120145832A1 (en) * | 2009-06-23 | 2012-06-14 | Matthias Schuster | Load lifting apparatus for a helicopter and helicopter |
| CN105083554A (en) * | 2014-05-14 | 2015-11-25 | 空客直升机德国有限公司 | External load mass rope of a rotorcraft |
| CN107108031A (en) * | 2015-11-03 | 2017-08-29 | 以色列宇航工业有限公司 | Hovering flight device and its control method |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2024142267A1 (en) * | 2022-12-27 | 2024-07-04 | 株式会社クボタ | Flying object |
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| PB01 | Publication | ||
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| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20200529 |