CN107243119A - A kind of bar - Google Patents

A kind of bar Download PDF

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Publication number
CN107243119A
CN107243119A CN201710708960.7A CN201710708960A CN107243119A CN 107243119 A CN107243119 A CN 107243119A CN 201710708960 A CN201710708960 A CN 201710708960A CN 107243119 A CN107243119 A CN 107243119A
Authority
CN
China
Prior art keywords
aircraft
bar
fire
thread
building
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.)
Pending
Application number
CN201710708960.7A
Other languages
Chinese (zh)
Inventor
杨卫国
何宇
陈静
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.)
Zhenjiang Pierre Nano Technology Co Ltd
Original Assignee
Zhenjiang Pierre Nano 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 Zhenjiang Pierre Nano Technology Co Ltd filed Critical Zhenjiang Pierre Nano Technology Co Ltd
Priority to CN201710708960.7A priority Critical patent/CN107243119A/en
Publication of CN107243119A publication Critical patent/CN107243119A/en
Pending legal-status Critical Current

Links

Classifications

    • AHUMAN NECESSITIES
    • A62LIFE-SAVING; FIRE-FIGHTING
    • A62CFIRE-FIGHTING
    • A62C3/00Fire prevention, containment or extinguishing specially adapted for particular objects or places
    • AHUMAN NECESSITIES
    • A62LIFE-SAVING; FIRE-FIGHTING
    • A62CFIRE-FIGHTING
    • A62C31/00Delivery of fire-extinguishing material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for

Abstract

The invention discloses a kind of bar, there is the part that can limit or fetter thread or ribbon motion above the bar, and the bar connects two buildings in the air.

Description

A kind of bar
Technical field
It is more particularly to a kind of to contribute to the bar of fire-fighting the invention belongs to draining field of feeding water.
Background technology
The fire extinguishing of skyscraper is a global problem, and current fire fighting truck more than ten floors that can only largely go out are high Fire.The solution of the problem has great social benefit and economic benefit.Therefore, applicant be directed to always solve this ask Topic.
The content of the invention
Goal of the invention:In order to solve the Fire-fighting Problems of high-rise, high-rise building, fire extinguishing is contributed to the invention provides one kind Bar.
Technical scheme is as follows:
Made using metal or carbon fiber sets some to limit or fetter thread or ribbon above a stock, bar The part of motion, the part includes but is not limited to enclose, saved, bolt, stub, and the bar connects two buildings in the air, is labeled as Build A and building B.
Preferably, the bar is arranged on building top or from the ground 100 meters high position above, the building top is Refer to the position and the part of the above of the half of the maximum height of building.
Preferably, bar is arranged on the top of building.So, any part of building is caught fire, and can be looked after and be obtained.
The building height that the present invention is not required for interconnecting bar is equal or similar, because bar is not required for level and put Put.
Preferably, the purpose of the above-mentioned bar in the present invention is, for fire-fighting, to play a part of fire-fighting;But except fire-fighting Outside, it is also used as other purposes.
Meanwhile, prepare a frame rotor type aircraft, the aircraft includes motor, the wing installed on motor(Blade), machine Frame and control unit.Thread is connected with the frame of aircraft;The thread refers to that draw ratio is more than 10 or long The business of degree and the square root in section is more than 10 object.Using heavy-duty motor, the loading capacity of the aircraft is set to reach that 400 is public Jin.
The weight range that the thread can be born is 100 ~ 50000 newton, or the load that the thread can be born Quality it is also bigger more than M kilograms than the quality of aircraft, M scope is 20 ~ 5000, and thread can be one or more.
The thread is electrically conductive, can also be non-conductive, including but not limited to wire, steel wire rope, nylon rope, can also be Recombination line/rope that conductive material is combined with electrically non-conductive material.
Thread can also be non-conductive, for example with the higher steel wire rope of intensity, nylon rope, now, the safety of aircraft Ensured by threads such as steel wire rope, nylon ropes.Aircraft is powered using battery, or adopts the power supply for being wired to outside Power supply.
Thread can be made using rigid material or elastomeric material, preferably, be made of elastomeric material, can also The composite rope that the composite being made up of elastomeric material and rigid material is made.
Preferably, the aircraft of the present invention is connected to wire, wire is connected to the power supply outside aircraft(External power supply) Aircraft is powered;Or power interface has been reserved in the frame of aircraft/aircraft, in order to wire when aircraft works It is connected to the power supply outside aircraft.
Preferably, the cross-sectional area of the conductive part of wire is more than 10 square millimeters.
Thread can also serve as thread in itself for wire, i.e. wire.For example with thicker copper cable or electricity In line, or the part of wire in addition to current-carrying part, insulated part, also pulling force strengthening part, the pulling force increases Strong part includes but is not limited to steel wire, steel wire.Now, after thread is connected firmly on board the aircraft, then with aircraft The members such as electric tunes, motor, power.
Preferably, the wire not only plays conduction, stress can also be played a part of, the two ends of wire are except even Energization source is with outside aircraft, also having done fixation so that when aircraft carries more than M kilograms of load and power-off, wire can Hold aircraft, avoid aircraft from falling;Described fixation includes but is not limited to the mechanics strengthening part in wire or wire Using tying up, it is, pricks etc. that mode is fixed on aircraft/aircraft parking stand, power supply position firm or can bear wire tension Place, M scope is 20 ~ 5000.
Described external power supply is including but not limited to generator, civilian electricity(Line)Or commercial power(Line), it is battery, architectural Power supply, aerial power supply etc..As needed, external power supply can be directly connected to aircraft, or pacified on board the aircraft Reused after dress transformer, progress transformation.
Preferably, power supply uses civilian or commercial power.
Manned or loading part, such as platform, nacelle or other forms can be installed on aircraft.Now, fireman can To carry the fire-fighting material landing vehicles such as water pipe, water band, fire extinguisher, fire extinguisher bomb, then take off, go near the place that catches fire and spray Above-water method.
Loading part can be used for carrying article, food of rescue etc..Other works can also be installed on aircraft Tool or accessory, to meet application of the aircraft in terms of fire-fighting, fire extinguishing, rescue.
Rescue passage can be set on aircraft, can be the forms such as staircase, bridge or passageway, for connect aircraft with Indicator of trapped personnel position, personnel's landing vehicles are rescued to allow.Rescuing passage can be using detachable, folding or scalable Device, used when to need.
Because the intensity of thread is big, when aircraft hinders for some reason to fall, it can be held by thread.
Winder folding and unfolding wire or thread can be used, with the position of pilot, the length of thread and aircraft Put and mutually coordinate, it is ensured that can be held in time when aircraft falls, being unlikely to fall too, decrease speed is too fast long afterwards.
Described Winder can be used and manually or mechanically controlled, it would however also be possible to employ remote control.
The control section of aircraft, it is possible to use external power supply is directly powered, will can also power after external power supply transformation, Or be powered using battery.Stand-by power supply can be included in aircraft, such as battery pack can also not have.Stand-by power supply For being in case of emergency powered to motor, but the power supply of the power section of aircraft primarily or entirely outside is supplied Electricity.Powered under normal circumstances using external power supply, once because power supply is out of order, stand-by power supply can be rapidly switched to, to prevent Only aircraft is fallen due to power failure.
Motor of the present invention can be direct current generator or alternating current generator.
It is mounted with aircraft interior for measuring the instrument that height changes with horizontal level, including but not limited to ultrasonic wave Sensor, barometer, GPS etc..Aircraft interior is also provided with Inertial Measurement Unit, including gyroscope, acceierometer sensor And other control units.
In operator scheme, all adopted using direct manipulation one of both of which on remote control, aircraft, or both of which With.Both patterns can switch mutually, to learn from other's strong points to offset one's weaknesses, ensure flight safety.Directly manipulation refers to people on the aircraft Aircraft is directly manipulated according to operation button, handle or operation interface etc. on board the aircraft.Such as in the case of having remote control mode May have signal and the situation such as disturb, block, at this moment using it is artificial directly manipulate on board the aircraft it is more efficient.
The aircraft of the present invention can install the monitoring device of camera etc, by directly being grasped in remote control or aircraft Control, can easily monitoring objective situation.The aircraft of the present invention can also include landing and buffering system, to reduce flight Impulsive force when device lands, the buffer system can be contact to earth position mounting bracket or the elastomeric element in aircraft, or gas Pad etc..
In order to prevent wire, thread from being encountered by blade, blade can be covered using guard, so, on the one hand avoided Blade encounters wire, thread, on the one hand can also protect blade.
The fire extinguishing system of the building of the present invention has gone out containing outside bar, aircraft, also containing pump, water tank, other extinguishing pipes One or more in road, water pipe, water band.
The fire-fighting mode of the present invention is as follows:
When finding that building A catches fire, inner utilization fire hydrant that on the one hand at that time can be directly from building A is put out a fire, and also may be used With using of the invention that scheme is put out a fire;When fire than it is larger when, into building A fire extinguishing it is abnormally dangerous, at this moment, of the invention goes out Fiery scheme will play a role, specific as follows:
Fire fighter enters building B, one end of the thread of aircraft or wire is fixed on building B, the other end is fixed on On aircraft.
Preferably, one end of thread or wire is fixed near the connecting portion of building B and bar, and wire is connected Connect power supply.
Aircraft can take off from ground, can also be taken off near the connecting portion of building B and bar, or architectural Take off at other positions.
Aircraft can be unmanned flight or manned.
The outlet at the water sources such as the tubes such as water pipe, water band and fire protection pipeline, roof tank is connected by fire fighter, the other end Fix on board the aircraft, the correct position that then aircraft flies on bar bar, tube, thread or wire are tried again solid Fixed, then fly to the place sprinkling fire nearby that catches fire.
Certainly, in the case where ensureing safety, above operation can also be carried out from building A.
The aircraft of the present invention typically flies downwards, i.e., the position when extreme lower position when aircraft works is set out less than it Put, extreme lower position when extreme lower position when either it works is less than the position of external power supply or its work connects less than it The position of the water pipe, water band or the water tank that connect, or it work when extreme lower position set low 2 meters than the highest order of wire or thread More than.
The solution of the present invention is used, once the building of building or surrounding is caught fire, then can take off aircraft, be put out a fire.
Beneficial effect:
The method provided using this programme, can efficiently solve the problem of present high-rise, high-rise building puts out a fire difficult.The present invention Bar can not only play a part of provide water, additionally it is possible to be used as aerial mechanical support.
For the ease of understanding the present invention, drawings and Examples, which are provided below, to be used to explain the present invention, but they are not constituted pair The restriction of the present invention.
Brief description of the drawings
Fig. 1 is the schematic diagram of the bar of the present invention.
The description of symbols of accompanying drawing 1:
1- stubs
2- bars
3- is enclosed
Embodiment
Below by the bar that the present invention is described in detail in conjunction with the embodiments.
The one long 150 meters, steel shank of 5 centimetres of diameter is made, and some circle, stubs are set above.
Described above is only some examples of embodiment of the present invention, it should be pointed out that:For the technology people of the art For member, under the premise without departing from the principles of the invention, some improvements and modifications can also be made, these improvements and modifications also should It is considered as protection scope of the present invention.

Claims (5)

1. a kind of bar, it is characterised in that:There are the part that can limit or fetter thread or ribbon motion, institute above the bar State part include but is not limited to enclose, save, bolt, stub, and the bar connects two buildings in the air.
2. a kind of bar according to claim 1, it is characterised in that:The purpose of the bar be for fire-fighting, or the water pipe tool There is fire-fighting.
3. a kind of bar according to claim 1, it is characterised in that:The bar is arranged on building top or 100 meters from the ground Position more than high, the building top refers to the position and the part of the above of the half of the maximum height of building.
4. a kind of bar according to claim 1, it is characterised in that:The bar is made up of metal or carbon fibre material.
5. a kind of bar according to claim 1, it is characterised in that:The bar can be used as the part for bearing pulling force.
CN201710708960.7A 2017-08-17 2017-08-17 A kind of bar Pending CN107243119A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710708960.7A CN107243119A (en) 2017-08-17 2017-08-17 A kind of bar

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710708960.7A CN107243119A (en) 2017-08-17 2017-08-17 A kind of bar

Publications (1)

Publication Number Publication Date
CN107243119A true CN107243119A (en) 2017-10-13

Family

ID=60012445

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710708960.7A Pending CN107243119A (en) 2017-08-17 2017-08-17 A kind of bar

Country Status (1)

Country Link
CN (1) CN107243119A (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3608322B2 (en) * 1996-12-24 2005-01-12 能美防災株式会社 Sprinkler equipment
US20090301736A1 (en) * 2008-06-05 2009-12-10 Tieck Craig I Deployable exterior fire protection system
US20130134254A1 (en) * 2011-11-29 2013-05-30 Jason Moore UAV Fire-fighting System
CN203790491U (en) * 2014-03-25 2014-08-27 沈有宁 High-rise building fire extinguishing device
CN104014098A (en) * 2014-03-24 2014-09-03 华金义 Hard fire-fighting water pipe with transverse tooth lines on transverse and vertical triangular suspended and fixed out walls
CN105214269A (en) * 2014-10-20 2016-01-06 华金义 The guiding round buss of groove and single-end is had to coordinate the hard fire extinguisher canvas hose pushed
CN206214616U (en) * 2016-09-28 2017-06-06 沈有宁 A kind of tall-building fire fighting aerial ladder

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3608322B2 (en) * 1996-12-24 2005-01-12 能美防災株式会社 Sprinkler equipment
US20090301736A1 (en) * 2008-06-05 2009-12-10 Tieck Craig I Deployable exterior fire protection system
US20130134254A1 (en) * 2011-11-29 2013-05-30 Jason Moore UAV Fire-fighting System
CN104014098A (en) * 2014-03-24 2014-09-03 华金义 Hard fire-fighting water pipe with transverse tooth lines on transverse and vertical triangular suspended and fixed out walls
CN203790491U (en) * 2014-03-25 2014-08-27 沈有宁 High-rise building fire extinguishing device
CN105214269A (en) * 2014-10-20 2016-01-06 华金义 The guiding round buss of groove and single-end is had to coordinate the hard fire extinguisher canvas hose pushed
CN206214616U (en) * 2016-09-28 2017-06-06 沈有宁 A kind of tall-building fire fighting aerial ladder

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Application publication date: 20171013