CN108622396A - A kind of airflight rescue robot - Google Patents
A kind of airflight rescue robot Download PDFInfo
- Publication number
- CN108622396A CN108622396A CN201810489970.0A CN201810489970A CN108622396A CN 108622396 A CN108622396 A CN 108622396A CN 201810489970 A CN201810489970 A CN 201810489970A CN 108622396 A CN108622396 A CN 108622396A
- Authority
- CN
- China
- Prior art keywords
- gear
- cabin
- shaft
- speed reducer
- link arm
- 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.)
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Links
- 239000003638 chemical reducing agent Substances 0.000 claims abstract description 37
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 19
- 238000005096 rolling process Methods 0.000 claims description 10
- 108010066114 cabin-2 Proteins 0.000 description 8
- 238000010586 diagram Methods 0.000 description 5
- 210000003128 head Anatomy 0.000 description 5
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 210000003027 ear inner Anatomy 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 239000010931 gold Substances 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface wheeled type, e.g. multi-wheeled bogies
- B64C25/36—Arrangements or adaptations of wheels, tyres or axles in general
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Retarders (AREA)
Abstract
The present invention provides a kind of airflight rescue robot, including flight instruments, cabin, side door, emergency cot, deliverance apparatus, landing gear, searchlight, shaft plate, the first speed reducer, the flight instruments are mounted on the top of cabin, side door is mounted on the both sides of cabin, emergency cot is placed in cabin, three landing gears are triangular in shape mounted on the bottom surface of cabin, searchlight is mounted on the front of cabin, first speed reducer is mounted on the lower section of cabin, shaft plate is inserted into the hollow shaft of the first speed reducer, and deliverance apparatus is connect with shaft plate；The present invention makes robot be moved near emergency place by flight instruments, realizes that height rescue works by multivariant deliverance apparatus, considerably increases the range for implementing rescue, improve the adaptability to complex building or environment.
Description
Technical field
The present invention relates to the technical field of the relevant device for air rescue, more particularly to a kind of airflight rescuing machine
Device people.
Background technology
High-rise is increasingly common in modern city at present, when in high-rise occur fire incident or
When some other sudden accident, the personnel inside high-rise can usually be stranded.When above-mentioned emergency occurs,
The prior art is typically to use the expansion rescue of the rescue aids such as motor ladder by fire department.But work as the height of building too
When height or the scene of the accident are in environment topography more special position, it is possible that motor ladder can not be close to accident building
Situation, to make rescue personnel and rescue aid quickly and effectively safe can not enter the scene of the accident, this will delay gold
Rescue time can bring immeasurable damage to the life security of captive, therefore this kind of situation needs to be rescued in the air
Help, although having there is some air rescue equipment in the market, but there are some defects, such as application No. is
201520330574.5 disclosing one kind《Unmanned plane air rescue robot》, including cabin, rotor, mechanical arm pick-and-place device,
Its mechanical arm pick-and-place device function vertical telescopic, degree of freedom is less, and enforceable rescue is limited in scope, it is therefore desirable to a kind of novel
Airflight rescue robot.
Invention content
In view of the above-mentioned problems, the present invention provides a kind of airflight rescue robot, robot is set to move by flight instruments
It moves to emergency place, realizes that height rescue works by multivariant deliverance apparatus, considerably increase implementation rescue
Range, improve the adaptability to complex building or environment.
Technical solution used in the present invention is：A kind of airflight rescue robot, including flight instruments, cabin, side
Door, emergency cot, deliverance apparatus, landing gear, searchlight, shaft plate, the first speed reducer, the flight instruments are mounted on machine
The top in cabin, side door are mounted on the both sides of cabin, and emergency cot is placed in cabin, and three landing gears are triangular in shape to be mounted on machine
The bottom surface in cabin, searchlight are mounted on the front of cabin, and the first speed reducer is mounted on the lower section of cabin, and shaft plate is inserted into first and slows down
In the hollow shaft of machine, deliverance apparatus is connect with shaft plate.
Further, the flight instruments include head cover, wing plate, the first pedestal, propeller, steering engine, the second pedestal, bottom
Disk, described eight the second pedestals of first layer are mounted on four wing plates of first layer, and head cover is solid with eight the second pedestals of first layer
Fixed, two layers of eight wing plates are linked together by the first pedestal, and eight the second pedestals of bottom are mounted on four wing plates of the second layer
On, eight the second pedestals in chassis and bottom are fixed, and steering engine is mounted on the end of wing plate, the spindle nose connection of propeller and steering engine.
Further, the deliverance apparatus includes pedestal, short axle, the second speed reducer, first gear, second gear,
One link arm, axle bumper, first rotating shaft, third gear, the second link arm, the 4th gear, the second shaft, safeguard station, the pedestal with
Shaft plate is fixed, and the first link arm head end is connect by short axle with pedestal, and second gear is fixed with short axle, and first second is slowed down
Machine is mounted on the head end of the first link arm, and first gear is inserted in the projecting shaft of the second speed reducer and is engaged with second gear, by second
A second speed reducer is mounted on the end of the first link arm, and first gear is inserted in the projecting shaft of the second speed reducer, and first rotating shaft is by the
One link arm is connected with the second link arm, and axle bumper is put in end, and third gear is inserted in first rotating shaft and is engaged with first gear, by third
A second speed reducer is mounted on the end of the second link arm, and first gear is inserted in the projecting shaft of the second speed reducer, and the second shaft passes through
Second link arm, one end are inserted in the 4th gear and are engaged with first gear, and the other end is connect with safeguard station.
Further, the landing gear includes cylinder block, cylinder, hinge, rolling bearing units, connecting shaft, wins in succession, supports
Wheel carrier, support wheel, the cylinder block and rolling bearing units are fixed on the bottom of cabin, and cylinder is mounted on cylinder block, connecting shaft two
End is inserted into rolling bearing units, is won in succession and is fixed with connecting shaft, and the cylinder rod of hinge one end and cylinder is fixed, the other end and fixation of winning in succession,
Support wheel carrier one end is fixed with connecting shaft, and a support wheel is respectively installed in other end both sides.
Beneficial effects of the present invention：（1）By the way of the present invention implements rescue using airflight, building height is breached
The case where limitation of degree and congestion in road so that rescue team can reach scene at the first time, and can rescue nothing on ground
It is rescued in the place that method reaches height；（2）The deliverance apparatus of the present invention uses the structure of multi freedom degree mechanical link arm so that rescues
The building that mechanism is adapted to different labyrinths is helped, the range of rescue is increased.
Description of the drawings
Fig. 1 is the overall structure diagram of the present invention.
Fig. 2 is partial structural diagram below the cabin of the present invention.
Fig. 3 is the flight instruments structural schematic diagram of the present invention.
Fig. 4 is the deliverance apparatus structural schematic diagram of the present invention.
Fig. 5 is the landing gear structural schematic diagram of the present invention.
Drawing reference numeral：1- flight instruments；2- cabins；3- side doors；4- emergency cots；5- deliverance apparatus；6- landing gears；7-
Searchlight；8- shaft plates；The first speed reducers of 9-；101- head covers；102- wing plates；The first pedestals of 103-；104- propellers；105- rudders
Machine；The second pedestals of 106-；The chassis 107-；501- pedestals；502- short axles；The second speed reducers of 503-；504- first gears；505-
Two gears；The first link arms of 506-；507- axle bumpers；508- first rotating shafts；509- third gears；The second link arms of 510-；511- the 4th
Gear；The second shafts of 512-；513- safeguard stations；601- cylinder blocks；602- cylinders；603- hinges；604- rolling bearing units；605- connects
Axis；606- wins in succession；607- supports wheel carrier；608- support wheels.
Specific implementation mode
With reference to specific embodiment, the invention will be further described, in the illustrative examples and explanation of the invention
For explaining the present invention, but it is not as a limitation of the invention.
Embodiment：A kind of airflight rescue robot as shown in figure 1, figure 2, figure 3, figure 4 and figure 5, including flight instruments
1, cabin 2, side door 3, emergency cot 4, deliverance apparatus 5, landing gear 6, searchlight 7, shaft plate 8, the first speed reducer 9, flight
Device 1 is mounted on the top of cabin 2, and side door 3 is mounted on the both sides of cabin 2, places emergency cot 4 in cabin 2, three rise and fall it is rack-mounted
Set 6 triangular in shape mounted on the bottom surface of cabin 2, searchlight 7 is mounted on the front of cabin 2, and the first speed reducer 9 is mounted on cabin 2
Lower section, shaft plate 8 be inserted into the first speed reducer 9 hollow shaft in, deliverance apparatus 5 is connect with shaft plate 8.
Flight instruments 1 include head cover 101, wing plate 102, the first pedestal 103, propeller 104, steering engine 105, the second pedestal
106, chassis 107, eight the second pedestals 106 of first layer are mounted on four wing plates 102 of first layer, head cover 101 and first layer eight
A second pedestal is fixed, and two layers of eight wing plates 102 are linked together by the first pedestal 103, eight the second pedestals 106 of bottom
On four wing plates 102 of the second layer, eight the second pedestals in chassis 107 and bottom are fixed, and steering engine 105 is mounted on wing plate 102
End, propeller 104 connect with the spindle nose of steering engine 105.
Deliverance apparatus 5 includes pedestal 501, short axle 502, the second speed reducer 503, first gear 504, second gear 505, the
One link arm 506, axle bumper 507, first rotating shaft 508, third gear 509, the second link arm 510, the 4th gear 511, the second shaft
512, safeguard station 513, pedestal 501 are fixed with shaft plate 8, and 506 head end of the first link arm is connect by short axle 502 with pedestal 501, the
Two gears 505 are fixed with short axle 502, and first the second speed reducer 503 is mounted on to the head end of the first link arm 506, first gear
504 are inserted in the projecting shaft of the second speed reducer 503 and are engaged with second gear 505, and second the second speed reducer 503 is mounted on the
The end of one link arm 506, first gear 504 are inserted in the projecting shaft of the second speed reducer 503, and first rotating shaft 508 is by the first link arm 506
It connects with the second link arm 510, axle bumper 507 is put in end, and third gear 509 is inserted in first rotating shaft 508 and is nibbled with first gear 504
It closes, the second speed reducer 503 of third is mounted on to the end of the second link arm 510, first gear 504 is inserted in the second speed reducer 503
Projecting shaft, the second shaft 512 passes through the second link arm 510, and one end is inserted in the 4th gear 511 and engaged with first gear 504, separately
One end is connect with safeguard station 513.
Landing gear 6 includes cylinder block 601, cylinder 602, hinge 603, rolling bearing units 604, connecting shaft 605, win 606 in succession,
Wheel carrier 607, support wheel 608, cylinder block 601 and rolling bearing units 604 is supported to be fixed on the bottom of cabin 2, cylinder 602 is mounted on gas
In cylinder seat 601,605 both ends of connecting shaft are inserted into rolling bearing units 604, win in succession 606 and the fixation of connecting shaft 605,603 one end of hinge and cylinder
602 cylinder rod is fixed, and the other end and 606 fixations of winning in succession, support 607 one end of wheel carrier are fixed with connecting shaft 605, and other end both sides are each
One support wheel 608 is installed.
The operation principle of the present invention：The work of steering engine 105 drives propeller 104 to rotate the flight function of realizing robot,
The work of first speed reducer 9 drives shaft plate 8 to rotate that deliverance apparatus 5 is driven to rotate, first the second speed reducer 503 work band
The dynamic rotation of first gear 504 is to drive the second gear 505 engaged rotation to realize the rotation of the first link arm 506, and second
A work of second speed reducer 503 drives the rotation of first gear 504 to drive the third gear 509 engaged to rotate, third
The rotation of gear 509 drives the rotation of first rotating shaft 508 to drive the rotation of the second link arm 510, third the second speed reducer 503 work
The rotation of first gear 504 is driven to drive the 4th gear 511 engaged rotation, the rotation of the 4th gear 511 to drive second
The rotation of shaft 512 to drive the rotation of safeguard station 513, cylinder 602 shrink by win in succession 606 and connecting shaft 605 so that support wheel
Frame 607 is packed up, cylinder 602 contraction protrude through win in succession 606 and connecting shaft 605 so that support wheel carrier 607 put down.
Claims (1)
1. a kind of airflight rescue robot, including flight instruments（1）, cabin（2）, side door（3）, emergency cot（4）, rescue dress
It sets（5）, landing gear（6）, searchlight（7）, shaft plate（8）, the first speed reducer（9）, it is characterised in that：The flight dress
It sets（1）Mounted on cabin（2）Top, side door（3）Mounted on cabin（2）Both sides, cabin（2）Interior placement emergency cot（4）, three
A landing gear（6）It is triangular in shape to be mounted on cabin（2）Bottom surface, searchlight（7）Mounted on cabin（2）Front, first
Speed reducer（9）Mounted on cabin（2）Lower section, shaft plate（8）It is inserted into the first speed reducer（9）Hollow shaft in, deliverance apparatus（5）
With shaft plate（8）Connection；
The flight instruments（1）Including head cover（101）, wing plate（102）, the first pedestal（103）, propeller（104）, steering engine
（105）, the second pedestal（106）, chassis（107）, described eight the second pedestals of first layer（106）Mounted on four wings of first layer
Plate（102）On, head cover（101）It is fixed with eight the second pedestals of first layer, two layers of eight wing plates（102）Pass through the first pedestal
（103）It links together, eight the second pedestals of bottom（106）Mounted on four wing plates of the second layer（102）On, chassis（107）With
Eight the second pedestals of bottom are fixed, steering engine（105）Mounted on wing plate（102）End, propeller（104）With steering engine（105）'s
Spindle nose connects；
The deliverance apparatus（5）Including pedestal（501）, short axle（502）, the second speed reducer（503）, first gear（504）,
Two gears（505）, the first link arm（506）, axle bumper（507）, first rotating shaft（508）, third gear（509）, the second link arm
（510）, the 4th gear（511）, the second shaft（512）, safeguard station（513）, the pedestal（501）With shaft plate（8）It is fixed,
First link arm（506）Head end passes through short axle（502）With pedestal（501）Connection, second gear（505）With short axle（502）It is fixed, it will
First the second speed reducer（503）Mounted on the first link arm（506）Head end, first gear（504）It is inserted in the second speed reducer
（503）Projecting shaft and and second gear（505）Engagement, by second the second speed reducer（503）Mounted on the first link arm（506）
End, first gear（504）It is inserted in the second speed reducer（503）Projecting shaft, first rotating shaft（508）By the first link arm（506）
With the second link arm（510）Series connection, axle bumper is put in end（507）, third gear（509）It is inserted in first rotating shaft（508）And with first
Gear（504）Engagement, by the second speed reducer of third（503）Mounted on the second link arm（510）End, first gear（504）
It is inserted in the second speed reducer（503）Projecting shaft, the second shaft（512）Across the second link arm（510）, the 4th gear is inserted in one end
（511）And and first gear（504）Engagement, the other end and safeguard station（513）Connection；
The landing gear（6）Including cylinder block（601）, cylinder（602）, hinge（603）, rolling bearing units（604）, connecting shaft
（605）, win in succession（606）, support wheel carrier（607）, support wheel（608）, the cylinder block（601）And rolling bearing units（604）Gu
It is scheduled on cabin（2）Bottom, cylinder（602）Mounted on cylinder block（601）On, connecting shaft（605）Rolling bearing units are inserted at both ends（604）
In, it wins in succession（606）With connecting shaft（605）It is fixed, hinge（603）One end and cylinder（602）Cylinder rod fix, the other end with win in succession
606 fix, and support wheel carrier（607）One end and connecting shaft（605）Fixed, a support wheel 608 is respectively installed in other end both sides.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810489970.0A CN108622396A (en) | 2018-05-21 | 2018-05-21 | A kind of airflight rescue robot |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810489970.0A CN108622396A (en) | 2018-05-21 | 2018-05-21 | A kind of airflight rescue robot |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108622396A true CN108622396A (en) | 2018-10-09 |
Family
ID=63693790
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810489970.0A Withdrawn CN108622396A (en) | 2018-05-21 | 2018-05-21 | A kind of airflight rescue robot |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108622396A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109606683A (en) * | 2019-01-28 | 2019-04-12 | 陈利娟 | A kind of fixed emergency rescuing system of transport based on unmanned plane and its method |
-
2018
- 2018-05-21 CN CN201810489970.0A patent/CN108622396A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109606683A (en) * | 2019-01-28 | 2019-04-12 | 陈利娟 | A kind of fixed emergency rescuing system of transport based on unmanned plane and its method |
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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 | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20181009 |
|
| WW01 | Invention patent application withdrawn after publication |