CN110182358A - A kind of high-rise rescue equipment based on unmanned air vehicle technique - Google Patents
A kind of high-rise rescue equipment based on unmanned air vehicle technique Download PDFInfo
- Publication number
- CN110182358A CN110182358A CN201910476697.2A CN201910476697A CN110182358A CN 110182358 A CN110182358 A CN 110182358A CN 201910476697 A CN201910476697 A CN 201910476697A CN 110182358 A CN110182358 A CN 110182358A
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- China
- Prior art keywords
- cabin
- air vehicle
- equipment based
- unmanned air
- rescue equipment
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- 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
- 238000000034 method Methods 0.000 title claims abstract description 22
- 230000007246 mechanism Effects 0.000 claims abstract description 21
- 238000009434 installation Methods 0.000 claims abstract description 8
- 239000011521 glass Substances 0.000 abstract description 11
- 230000000694 effects Effects 0.000 abstract description 4
- 108010066057 cabin-1 Proteins 0.000 description 17
- 238000010586 diagram Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000000630 rising effect Effects 0.000 description 2
- 239000002893 slag Substances 0.000 description 2
- 239000000779 smoke Substances 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- 241000883990 Flabellum Species 0.000 description 1
- 239000002775 capsule Substances 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
-
- 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
-
- 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
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- 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
- 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
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- 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)
- Remote Sensing (AREA)
- Window Of Vehicle (AREA)
Abstract
The present invention relates to high-rise rescue equipment technical fields, and disclose a kind of high-rise rescue equipment based on unmanned air vehicle technique, including cabin, hatch door, window, connector and multiaxis aviation mechanism, the quantity of the window is five, the quantity of the multiaxis aviation mechanism is six, five windows and hatch door are located at the side of the cabin, the connector rotational installation is in the top of the cabin, six multiaxis aviation mechanism rotational installations are on the connector, the bottom of the cabin is fixedly installed with link block, multi-stage expansion cylinder is rotatably equipped on front side of the link block.The high-rise rescue equipment based on unmanned air vehicle technique, after sucker is fixed on the glass of bottom, sucker can be connect by multi-stage expansion cylinder with cabin, therefore when handling fire behavior, multi-stage expansion cylinder can play restriction effect to the movement of cabin, it prevents cabin under the impact force by heat wave, pushed away from too far.
Description
Technical field
The present invention relates to high-rise rescue equipment technical field, specially a kind of skyscraper based on unmanned air vehicle technique
Rescue aid.
Background technique
China's " technical specification for concrete structures of high-rise building " (JGJ 3-2010) 1.0.2 item provides 10 layers and 10 layers or more
Or other high-rise civil building concrete structures of residential housing of the height of house greater than 28m and height of house greater than 24 meters are
Skyscraper.Fire of high-rise building rescue is one of Three Difficult Issues generally acknowledged in the world at present, because layer height is excessively high, at present absolutely
Most of fire-fighting equipments are difficult to reach, and fire hydrant pressure is inadequate etc., and adopt helicopter rescue because scene of a fire situation is multiple
It is miscellaneous be difficult to it is close.
Therefore, a kind of high building fire-proof rescue flight cabin is disclosed in the patent document of Publication No. CN205113740U,
The flight capsule includes cabin, hatch door, multiaxis aviation mechanism etc., is a kind of high-rise rescue cabin based on unmanned air vehicle technique, Ke Yitong
The control for crossing rescue personnel rises to cabin at the floor that is in danger, and for rescue, rescues compared to traditional aerial ladder, this is rescued
It is higher to help the floor that cabin is adapted to, still, which when in use, needs vacantly to stop for a period of time to put out a fire to inside
Processing, within this time, will receive the impact of heat wave, due to there is no supporting mechanism, can pushed away from, in the sky can pole not
Stablize, meanwhile, when entering implementation rescue in building, the fixing support rack support of cabin landing only two sides, after being impacted,
In the presence of the hidden danger toppled over.
Summary of the invention
The invention provides the following technical scheme: a kind of high-rise rescue equipment based on unmanned air vehicle technique, including cabin,
The quantity of hatch door, window, connector and multiaxis aviation mechanism, the window is five, and the quantity of the multiaxis aviation mechanism is
Six, five windows and hatch door are located at the side of the cabin, and the connector rotational installation is in the cabin
Top, on the connector, the bottom of the cabin is fixedly installed with connection for six multiaxis aviation mechanism rotational installations
Block is rotatably equipped with multi-stage expansion cylinder on front side of the link block, and one end of the multi-stage expansion cylinder is rotatably equipped with sucker, institute
The side for stating sucker offers through-hole, and fixing sleeve is connected to control valve in the through-hole.
Preferably, the direction and hatch door position consistency of the multi-stage expansion cylinder.
Preferably, the two sides of the bottom of the cabin are fixedly installed with fixed bracket, and the link block is located at described in two
Between fixed bracket, the bottom of the cabin is fixedly installed with U-shaped connector, and the quantity of U-shaped connector is two, two institutes
It states and is rotatably equipped with U-shaped support frame in U-shaped connector, the inside of two the U-shaped support frames and two U-shaped connectors
Between be fixedly installed with torsionspring.
Preferably, the direction of the U-shaped support frame bottom is with the position of hatch door on the contrary, the U-shaped support frame is located at two
Between the fixed bracket.
Preferably, wiper is rotatably equipped on the window, and the quantity of wiper is two, two wipers
It is rotatablely installed respectively in the top and bottom of the window.
Preferably, the height of the wiper is the half of the height, the height of the wiper and the window
Family it is of same size.
Preferably, it is fixedly installed with baffle at the top of the multiaxis aviation mechanism, offers venthole on the baffle.
Preferably, the venthole is round table-like inclined hole, and the diameter of the venthole bottom is less than the diameter at top.
With high building fire-proof rescue flight cabin compare, the present invention have it is following the utility model has the advantages that
1, it is somebody's turn to do the high-rise rescue equipment based on unmanned air vehicle technique, after sucker is fixed on the glass of bottom,
Sucker can be connect by multi-stage expansion cylinder with cabin, therefore when handling fire behavior, and multi-stage expansion cylinder can play the movement of cabin
To restriction effect, prevents cabin under the impact force by heat wave, pushed away from too far.
2, it is somebody's turn to do the high-rise rescue equipment based on unmanned air vehicle technique, the U-shaped support frame at rear portion is pressed by cabin, it is U-shaped
Support frame rotates around U connector, and torsionspring is driven to rotate, and the elasticity of torsionspring can play the twisting resistance
The effect of power is unloaded, that is, the maximum endurance of cabin can be improved, prevents cabin by toppling over after impact force.
Detailed description of the invention
Fig. 1 is the whole structural schematic diagram of the present invention；
Fig. 2 is the structural schematic diagram of bottom of the present invention；
Fig. 3 is the partial enlarged view of A in Fig. 2；
Fig. 4 is the structural schematic diagram of U-shaped connector of the present invention.
In figure: 1, cabin；2, hatch door；3, window；4, connector；5, multiaxis aviation mechanism；6, link block；7, multi-stage expansion
Cylinder；8, through-hole；9, control valve；10, fixed bracket；11, U-shaped connector；12, U-shaped support frame；13, torsionspring；14, windscreen wiper
Device；15, baffle；16, venthole；17, sucker.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Fig. 1-4, including cabin 1, hatch door 2, window 3, connector 4 and multiaxis aviation mechanism 5 are please referred to, cabin is six sides
Shape, the quantity of window 3 are five, and the quantity of multiaxis aviation mechanism 5 is six, and five windows 3 and hatch door 2 are located at cabin 1
Side, the rotational installation of connector 4 is in the top of cabin 1, and six rotational installations of multiaxis aviation mechanisms 5 are on connector 4, cabin
1 bottom is fixedly installed with link block 6, and the front side of link block 6 is rotatably equipped with multi-stage expansion cylinder 7, the direction of multi-stage expansion cylinder 7
, in order to improve rescue efficiency, make to enter cabin 1 at the first time by rescue personnel, need in rescue with 2 position consistency of hatch door
Make the glass of the position alignment of hatch door 2 floor, wastes rescue time in order to avoid adjustment multi-stage expansion cylinder 7, which can
Sucker 17 is directed at glass stretching with more convenient, one end of multi-stage expansion cylinder 7 is rotatably equipped with sucker 17, the side of sucker 17
Through-hole 8 is offered, fixing sleeve is connected to control valve 9 in through-hole 8, and the two sides of the bottom of cabin 1 are fixedly installed with fixed bracket 10, even
Block 6 is connect between two fixed brackets 10, the bottom of cabin 1 is fixedly installed with U-shaped connector 11, and U-shaped connector 11
Quantity is two, and U-shaped support frame 12, the direction of U-shaped 12 bottom of support frame and cabin are rotatably equipped in two U-shaped connectors 11
The position of door 2 is on the contrary, U-shaped support frame 12 is located between two fixed brackets 10, when the alignment glass of hatch door 2 enters rear, when cabin 1
When being hit, the direction of power is face hatch door 2, and U-shaped support frame 12 is contrary with hatch door 2, and the maximum of cabin 1 can be improved
Endurance, is fixedly installed with torsionspring 13 between two U-shaped support frames 12 and the inside of two U-shaped connectors 11, is arranged
In the side in rotation axis, being individually fixed in U-shaped support frame 12 and U-shaped connector 11, wiper is rotatably equipped on window 3
14, wiper 14 is located at the outside of glass, and the quantity of wiper 14 is two, and the height of wiper 14 is 3 height of window
Half, this height can guarantee contact with each other when two wipers 14 are run, influence to rotate, the height of wiper 14 with
Window 3 it is of same size, wiper 14 can carry out 90 degree of rotation, improve the cleaning area of glass, two wipers 14
It is rotatablely installed when the top and bottom of window 3, fire respectively, has thick smoke generation, the window of the cabin 1 can be by dense smoke
It covers, influences the visual field of rescue personnel, delay rescue time, wiper 14 can clear up window 3 in time, guarantee the visual field, multiaxis
The top of aviation mechanism 5 is fixedly installed with baffle 15, and venthole 16 is offered on baffle 15, and venthole 16 is round table-like inclined hole,
The diameter of 16 bottom of venthole is less than the diameter at top, can fall into avoid the glass disintegrating slag of small volume along venthole 16 more
It in axis aviation mechanism 5, prevents top from thering is glass disintegrating slag to fall into multiaxis aviation mechanism 5, damage is generated to the blade of high-speed rotation,
Venthole 16 can not influence the air-flow in flabellum.
Working principle is opened multistage firstly, cabin 1 is transported to below the layer that is in danger one layer using multiaxis aviation mechanism 5
Telescoping cylinder 7, so that sucker 17 is adsorbed on the glass of bottom, and the gas between sucker 17 and glass is discharged by control valve 9,
It controls cabin 1 again to fly upwards, since the rotational installation of multi-stage expansion cylinder 7 is between sucker 17 and link block 6, in cabin 1
When rising, cabin 1 can be followed mobile, motion track is to rotate around sucker 17, i.e. the rising of cabin 1 not will receive multi-stage expansion
The influence of cylinder 7, cabin 1 rises to when being in danger layer, handles internal fire behavior；When cabin 1 is landed and rescued, impacted
Afterwards, the U-shaped support frame 12 at rear portion can be pressed, U-shaped support frame 12 rotates around U-shaped connector 11, and drives torsionspring
The elasticity of 13 rotations, torsionspring 13 can play the effect for unloading power to the twisting resistance.
It should be noted that, in this document, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also including other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (8)
1. a kind of high-rise rescue equipment based on unmanned air vehicle technique, including cabin (1), hatch door (2), window (3), connector
(4) and multiaxis aviation mechanism (5), it is characterised in that: the quantity of the window (3) is five, the multiaxis aviation mechanism (5)
Quantity is six, and five windows (3) and hatch door (2) are located at the side of the cabin (1), and the connector (4) turns
The dynamic top for being installed on the cabin (1), six multiaxis aviation mechanisms (5) rotational installations are on the connector (4), institute
The bottom for stating cabin (1) is fixedly installed with link block (6), is rotatably equipped with multi-stage expansion cylinder on front side of the link block (6)
(7), one end of the multi-stage expansion cylinder (7) is rotatably equipped with sucker (17), and the side of the sucker (17) offers through-hole
(8), the interior fixing sleeve of the through-hole (8) is connected to control valve (9).
2. a kind of high-rise rescue equipment based on unmanned air vehicle technique according to claim 1, it is characterised in that: described
Direction and hatch door (2) position consistency of multi-stage expansion cylinder (7).
3. a kind of high-rise rescue equipment based on unmanned air vehicle technique according to claim 1, it is characterised in that: described
The two sides of the bottom of cabin (1) are fixedly installed with fixed bracket (10), and the link block (6) is located at two fixed brackets
(10) between, the bottom of the cabin (1) is fixedly installed with U-shaped connector (11), and the quantity of U-shaped connector (11) is two
It is a, it is rotatably equipped with U-shaped support frame (12) in two U-shaped connectors (11), two U-shaped support frames (12) and two
Torsionspring (13) are fixedly installed between the inside of a U-shaped connector (11).
4. a kind of high-rise rescue equipment based on unmanned air vehicle technique according to claim 3, it is characterised in that: described
The direction of U-shaped support frame (12) bottom and the position of hatch door (2) are on the contrary, the U-shaped support frame (12) is located at two fixations
Between bracket (10).
5. a kind of high-rise rescue equipment based on unmanned air vehicle technique according to claim 1, it is characterised in that: described
It is rotatably equipped on window (3) wiper (14), and the quantity of wiper (14) is two, two wipers (14) are respectively
It is rotatablely installed in the top and bottom of the window (3).
6. a kind of high-rise rescue equipment based on unmanned air vehicle technique according to claim 5, it is characterised in that: described
The height of wiper (14) is the half of the window (3) height, the height of the wiper (14) and the width of the window (3)
It spends identical.
7. a kind of high-rise rescue equipment based on unmanned air vehicle technique according to claim 1, it is characterised in that: described
It is fixedly installed at the top of multiaxis aviation mechanism (5) baffle (15), offers venthole (16) on the baffle (15).
8. a kind of high-rise rescue equipment based on unmanned air vehicle technique according to claim 7, it is characterised in that: described
Venthole (16) is round table-like inclined hole, and the diameter of venthole (16) bottom is less than the diameter at top.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910476697.2A CN110182358A (en) | 2019-06-03 | 2019-06-03 | A kind of high-rise rescue equipment based on unmanned air vehicle technique |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910476697.2A CN110182358A (en) | 2019-06-03 | 2019-06-03 | A kind of high-rise rescue equipment based on unmanned air vehicle technique |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110182358A true CN110182358A (en) | 2019-08-30 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910476697.2A Pending CN110182358A (en) | 2019-06-03 | 2019-06-03 | A kind of high-rise rescue equipment based on unmanned air vehicle technique |
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| Country | Link |
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| CN (1) | CN110182358A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105173108A (en) * | 2015-09-20 | 2015-12-23 | 孙正鼐 | High-rise fire rescue flight cabin |
| CN206155780U (en) * | 2016-10-11 | 2017-05-10 | 天津中德应用技术大学 | Unmanned aerial vehicle undercarriage vaulting pole lock |
| US20170158354A1 (en) * | 2015-12-04 | 2017-06-08 | Sikorsky Aircraft Corporation | Detachable power transfer device for a rotary-wing aircraft |
| CN107235147A (en) * | 2017-07-18 | 2017-10-10 | 深圳市雷凌广通技术研发有限公司 | It is a kind of to improve the unmanned plane of fire-fighting efficiency for tall-building fire fighting |
| CN109204814A (en) * | 2018-09-03 | 2019-01-15 | 王浩 | A kind of high-storey fire rescue method |
| JP2019073160A (en) * | 2017-10-16 | 2019-05-16 | 株式会社安田測量 | Underwater probe device and terrain probe system |
-
2019
- 2019-06-03 CN CN201910476697.2A patent/CN110182358A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105173108A (en) * | 2015-09-20 | 2015-12-23 | 孙正鼐 | High-rise fire rescue flight cabin |
| US20170158354A1 (en) * | 2015-12-04 | 2017-06-08 | Sikorsky Aircraft Corporation | Detachable power transfer device for a rotary-wing aircraft |
| CN206155780U (en) * | 2016-10-11 | 2017-05-10 | 天津中德应用技术大学 | Unmanned aerial vehicle undercarriage vaulting pole lock |
| CN107235147A (en) * | 2017-07-18 | 2017-10-10 | 深圳市雷凌广通技术研发有限公司 | It is a kind of to improve the unmanned plane of fire-fighting efficiency for tall-building fire fighting |
| JP2019073160A (en) * | 2017-10-16 | 2019-05-16 | 株式会社安田測量 | Underwater probe device and terrain probe system |
| CN109204814A (en) * | 2018-09-03 | 2019-01-15 | 王浩 | A kind of high-storey fire rescue method |
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| SE01 | Entry into force of request for substantive examination | ||
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Application publication date: 20190830 |