CN106245543B - Helistop with locking device - Google Patents
Helistop with locking device Download PDFInfo
- Publication number
- CN106245543B CN106245543B CN201610615973.5A CN201610615973A CN106245543B CN 106245543 B CN106245543 B CN 106245543B CN 201610615973 A CN201610615973 A CN 201610615973A CN 106245543 B CN106245543 B CN 106245543B
- Authority
- CN
- China
- Prior art keywords
- parking area
- airplane parking
- bucket
- wedge block
- cover board
- 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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Classifications
-
- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01F—ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
- E01F3/00—Landing stages for helicopters, e.g. located above buildings
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C3/00—Fire prevention, containment or extinguishing specially adapted for particular objects or places
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C31/00—Delivery of fire-extinguishing material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/12—Ground or aircraft-carrier-deck installations for anchoring aircraft
-
- E—FIXED CONSTRUCTIONS
- E03—WATER SUPPLY; SEWERAGE
- E03B—INSTALLATIONS OR METHODS FOR OBTAINING, COLLECTING, OR DISTRIBUTING WATER
- E03B11/00—Arrangements or adaptations of tanks for water supply
- E03B11/02—Arrangements or adaptations of tanks for water supply for domestic or like local water supply
-
- E—FIXED CONSTRUCTIONS
- E03—WATER SUPPLY; SEWERAGE
- E03B—INSTALLATIONS OR METHODS FOR OBTAINING, COLLECTING, OR DISTRIBUTING WATER
- E03B9/00—Methods or installations for drawing-off water
- E03B9/02—Hydrants; Arrangements of valves therein; Keys for hydrants
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A20/00—Water conservation; Efficient water supply; Efficient water use
Landscapes
- Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Life Sciences & Earth Sciences (AREA)
- Water Supply & Treatment (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Structural Engineering (AREA)
- Hydrology & Water Resources (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Buildings Adapted To Withstand Abnormal External Influences (AREA)
- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
- Refuge Islands, Traffic Blockers, Or Guard Fence (AREA)
- Catching Or Destruction (AREA)
- Emergency Lowering Means (AREA)
- Train Traffic Observation, Control, And Security (AREA)
Abstract
The present invention relates to a kind of helistops with locking device; locking device includes flat panel; bucket-shaped bucket is provided in the middle part of panel; the notch section of bucket is more than slot bottom section; hitching post is set in bucket; the mast that hitching post is plugged respectively by casing and casing both ends is constituted; the first spring is provided between the abutting end of two masts; lock machine bolt is mounted in the pilot hole of airplane parking area ontology; openable cover board is provided at the notch of bucket, panel, cover board and the surface of airplane parking area ontology are arranged in concordant shape.The airplane parking area that above-mentioned technical proposal provides can guarantee that the reliable of helicopter lands and take off and other safety.
Description
It is on March 31st, 2015 that the present invention, which is the applying date, application No. is 2015101450448, entitled " helicopter
The divisional application of the patent of invention of airplane parking area ".
Technical field
The present invention relates to airplane parking area fields, and in particular to a kind of helistop with locking device.
Background technology
Helistop with locking device is mainly used for taking off and land, due to take off, land with
And the particularity of safety, therefore the requirement to airplane parking area is also complex.Currently, many helicopters with locking device are shut down
Level ground be arranged on tall building roof or overpass, therefore, it is necessary to be equipped with corresponding equipment to it, at the same need to roof flooring into
Row improves.
Invention content
It is an object of the invention to provide a kind of helistops with locking device, and helicopter can be realized in height
Effective takeoff and landing of building airplane parking area.
To achieve the above object, present invention employs following technical schemes to be implemented：
A kind of helistop with locking device, it is characterised in that：Including airplane parking area ontology, on airplane parking area ontology
The locking device for being provided with fire-fighting equipment and helicopter being fixed is provided with protection network on the side wall of airplane parking area ontology.
The airplane parking area that above-mentioned technical proposal provides can guarantee that the reliable of helicopter lands and take off and other peaces
Entirely.
Description of the drawings
Fig. 1 is the structural schematic diagram of airplane parking area ontology；
Fig. 2 is enlarged diagram at the C of Fig. 1；
Fig. 3 is the structural schematic diagram of shockproof landing plate；
Fig. 4 is the structural schematic diagram of fire-fighting equipment；
Fig. 5 is the structural schematic diagram that water inlet pipe is arranged on fire water box；
Fig. 6 is the structural schematic diagram of protection network；
Fig. 7 is the structural schematic diagram of web plate；
Fig. 8 is the scheme of installation of web plate on the support columns；
Fig. 9 is enlarged diagram at the A of Fig. 6；
Figure 10 is enlarged diagram at the B of Fig. 6；
Figure 11 is the structural schematic diagram of mounting plate；
Figure 12 is the structural schematic diagram of the present invention；
Figure 13 is the structural schematic diagram of adjusting part；
Figure 14 is the structural schematic diagram of hitching post.
Specific implementation mode
In order to make objects and advantages of the present invention be more clearly understood, the present invention is carried out specifically with reference to embodiments
It is bright.It should be appreciated that following word is only used to one or more of specific embodiments of the description present invention, not to the present invention
The protection domain specifically asked carries out considered critical.
The technical solution that the present invention takes is：A kind of helistop with locking device, including airplane parking area ontology,
The locking device for being provided with fire-fighting equipment on airplane parking area ontology and helicopter being fixed is set on the side wall of airplane parking area ontology
It is equipped with protection network.
It specifically operates and is：
As shown in Figure 1, 2, 3, airplane parking area ontology includes airplane parking area platform A11, and one layer is equipped on airplane parking area platform A11
The region that helicopter is parked on waterproof layer A12, waterproof layer A12 is inlaid with shockproof landing plate A20, the surface of shockproof landing plate A20
It is arranged in concordant shape with surfaces waterproof layer A12 of its periphery, the shockproof plate A20 that lands is by supporting layer A21, the bone arranged from top to bottom
Bed of material A22 and elastic layer A23 compositions, the surface setting of supporting layer paint the skid resistant course constituted by anti-skidding, and the thickness of supporting layer is
The thickness of 4mm, buffer layer are 20mm, and the thickness of elastic layer is 6mm, and supporting layer is the high hardness polyurethane structure of 50~60D of hardness
At the elastic layer of aggregate layer is that the ceramsite sand of 30~35 parts by weight and the microvoid polyurethane of 65~75 parts by weight are constituted, elastic layer
It is constituted for microvoid polyurethane, the hardness of microvoid polyurethane is 45~50A；
Microvoid polyurethane is reacted by following raw material to be made：The poly- butyrate of 95 parts by weight, the ethylene glycol of 25 parts by weight, 0.2
The triethylene diamine of parts by weight, the castor oil sodium sulfonate of 0.1 parts by weight, the polyether silicone of 0.15 parts by weight, 0.6 parts by weight
Polyurethane foams stabilizers, the water of 1 parts by weight, the methyl diphenylene diisocyanate of 70 parts by weight, 30 parts by weight dimethyl connection
Tetrahydrofuran-oxidation third of phenylene diisocyanate, the MDI of 5.2 parts by weight, the polyester adipate of 25 parts by weight and 30 parts by weight
Alkene copolymer glycols；Preparation method is：According to the raw material of microvoid polyurethane than weighing each raw material respectively, by poly- butyrate, ethylene glycol,
Triethylene diamine, castor oil sodium sulfonate, polyether silicone, polyurethane foams stabilizers, methyl diphenylene diisocyanate and water are anti-
Answer in kettle 55 DEG C of hybrid reactions that mixture A is made, by methyl diphenylene diisocyanate, dimethyl diphenyl diisocyanate,
MDI (liquid), polyester adipate, tetrahydrofuran-propylene oxide copolymer glycols 70 DEG C of hybrid reactions in the reaction kettle of inflated with nitrogen,
Mixture B is made in vacuum removal bubble, and mixture A, B, which are then carried out hybrid reaction, can be prepared by microvoid polyurethane material.
High hardness polyurethane is reacted by following components raw material to be made：The poly- butyrates of 25 parts by weight, 20 parts by weight gather oneself
Two acid esters, the paraphenylene diisocyanate of 45 parts by weight, the ethylene glycol of 5 parts by weight, the 1 of 15 parts by weight, 12- dodecanediols and
The antioxidant 1010 of 1.5 parts by weight.High hardness polyurethane is that each raw material is squeezed out to obtain by formula ratio mixed polymerization.Airplane parking area platform
It is constituted for concrete material, waterproof layer is that general airplane parking area is constituted with waterproof material.
The airplane parking area constituted using the vibrationproof landing plate (effectiveness in vibration suppression is splendid) of said components and structure is implemented,
Helicopter land when can play effective effectiveness in vibration suppression, can 100% eliminate resonance, oscillatory acceleration grade reduce 10dB or more, can
Effectively avoid the generation of safety accident.
As shown in Figure 4,5, fire-fighting equipment include water storage fire water box B10 and each fire hydrant B20, fire water box B10 and
Fixed froth installation B30 is provided between fire hydrant, fire water box B10 is connected by outlet pipe B13 with fixed froth installation B30
It connects, fixed froth installation is connected by connecting pipe with each fire hydrant B20, bottom face B101a (the bottom B101 of fire water box
Upper surface) arranged in 2~3 ° of inclinations angle, the high-end setting outlet pipe B13 of bottom of fire water box, the bottom of fire water box is low
Blow-off pipe is arranged in end, and fire pump is provided on outlet pipe B13, and blowdown valve, the entrance setting of outlet pipe B13 are arranged on blow-off pipe
There is strainer, water level detecting sensor B12 is provided in fire water box, water inlet pipe B11, water inlet pipe are additionally provided on fire water box
B11 includes the montant B111 of the vertical shape arrangement of the high-end top setting of the bottom of fire water box, and the lower end of montant is provided with and it
The transverse tube B112 of the horizontal shape arrangement of connection, faucet B16 is arranged in uniform intervals on the pipe shaft of transverse tube, and the water outlet direction of faucet refers to
To the high-end places that join with fire water box side wall B102 bottom B101 of fire water box, on the pipe shaft of vertical tube along its length
It is arranged at intervals with aperture B111a, electromotive intake valve and manual modulation valve are provided on water inlet pipe.
Water pump and electrically operated valve B50 are provided on outlet pipe, the starting switch setting of water pump and electrically operated valve B50 are in fire-fighting
In switch board B40, water level detecting sensor B12 is connected with switch board B40, and switch board is according to the detection of water level detecting sensor
As a result the open/close states for regulating and controlling electromotive intake valve, supplement fire demand water.Impurity in fire water box can be from fire water box bottom
Higher-end slides to the lower end of fire-fighting water phase bottom, to avoid impurity from being flowed out in other component from outlet pipe, in addition, can
Periodically fire-fighting system is checked, can be discharged into impurity such as the iron rust of fire water box from sewage draining exit.Water level monitoring senses
The setting of device can ensure that the water level in water tank is normal, ensure the reliability of fire extinguishing system.Fire-fighting system is according to water level sensor
The control of testing result automatic loading water can refer to the control of automatic loading water in existing other systems and specifically implemented, aperture
B111a can play the role of the noise reduction of the water inlet pipe to suspention shape arrangement.
Specific embodiment is：It is provided with the first and second road branch pipe on outlet pipe, is respectively set on the first and second road branch pipe
First and second water pump B71, B72, there are two fire hydrant settings.
As shown in Fig. 6~11, safety guard net include airplane parking area platform side wall D20 on extend outwardly obliquely setting
Support column D10, support column D10 are that rectangular pipe fitting is constituted by section, and the angle of inclination of support column D10 is 8~10 ° and along shutdown
The level ground intervals mesa sidewalls D20 are uniformly arranged, and are provided with web plate D30 between adjacent two support columns D10, web plate D30 by frame D31 and
Steel wire D33 in frame D31 is constituted, and L-shaped angle is respectively set perpendicular to the both sides edge of support column D10 and middle part in frame
Steel D32, L-shaped angle steel D32 are arranged along width (perpendicular to the direction of support column D10) range of frame, are uniformly provided on frame
Mounting hole, web plate D30 are fixed on support column D10 by bolt assembly D13, L-shaped installation part D12 and L-shaped angle steel D32
On, L-shaped installation part D12 and L-shaped angle steel D32 are arranged in the downside plate face of web plate D30, the side wall D20 of airplane parking area platform
On be provided with mounting plate D23 for installing support column D10, be embedded with embedded board D21 in side wall D20, embedded board D21 includes platform
The plate face of first and second plate body of scalariform arrangement, the first and second plate body is parallel to mounting plate D23 arrangements, mounting plate D23 and first and second
It is linked together respectively by pre-embedded bolt D22 between plate body.Bolt assembly and L-shaped installation part D12 combine the installation to web plate D30
0 is implemented referring to Fig.1, and the installation of web plate D30 is implemented in bolt assembly and the D32 combinations of L-shaped angle steel with reference to Fig. 9, L-shaped peace
Piece installing D12 can have L-shaped angle steel D32 to block to obtain.The angle of inclination of support column D10 blows to protection network when landing according to helicopter
Wind direction and determination, improve wind loading rating.
Specifically scheme is：It is provided with stiffener plate D11, reinforcing rib between the installation end and mounting plate D23 of support column D10
The plate face of plate D11 along vertical direction arrange, two adjacent stiffener plate D11 rim portions not with mounting plate D23 and support column D10
The faces downside wall D20 be welded as a whole, as shown in Fig. 6,11.In addition sides of the support column D10 far from side wall D20, which extends downwardly, sets
It is equipped with the extended segment D10a of vertical shape arrangement, the lower end of extended segment D10a is provided with tracheae D10b, and tracheae is arranged perpendicular to support column,
Interval setting air nozzle, the outgassing direction of air nozzle are directed toward the wire side of web plate obliquely on the pipe shaft of tracheae.By blowing net
Rubbish on plate D30 blows to the sides side wall D20 and gathers, the cleaning of personnel easy to operation.
As shown in Figure 12,13,14, locking device includes flat panel C21, is provided in the middle part of panel C21 bucket-shaped
Bucket, the notch section of bucket is more than slot bottom section, hitching post is arranged in bucket, hitching post is by cannula C 31 and 31 both ends of cannula C point
The mast C32 not plugged is constituted, and the first spring is provided between the abutting end of two mast C32, and hitching post is mounted on airplane parking area ontology
Pilot hole in, be provided with openable cover board C22 at the notch of bucket, panel C21, cover board C22 and airplane parking area ontology table
Face is arranged in concordant shape.Above-mentioned hitching post when mounted, is previously provided with pilot hole, is opened on the hole wall of pilot hole on airplane parking area ontology
Equipped with jack, first push mast C32 when mounted and compress the first spring, other component be installed in place after again by the end of hitching post
It is loose to be inserted into jack, realize the fixation of hitching post.When dismounting and change, it is only necessary to mast C32 be compressed the first spring and make hitching post
Shortening.
In addition, being connected with the copper conductor for lightning protection on hitching post.The intensity of cover board C22 in this way is big, prevents from being crushed.
Further scheme is that one end of cover board C22 is articulated and connected with airplane parking area ontology and the hinged edge is provided with
So that the torsional spring C23 of cover board C22 pop-ups, the cover board C22 other ends are extended into airplane parking area ontology pilot hole lock C24,
Lockhole is offered on lock C24, the hole heart direction of lockhole is arranged in the horizontal direction, and lock pin C43 is provided on the side wall of pilot hole,
Lock pin C43 is connected with its adjusting part moved along lockhole hole heart direction is driven, and adjusting part includes two mutual cooperations
First and second wedge block C41, C42, first and second wedge block C41, C42 be mounted in the mounting hole opened up on pilot hole side wall,
The one end of lock pin C43 far from lock C24 is connected with the first wedge block C41, and the first wedge block C41 is moved in the horizontal direction, the
Two wedge block C42 are moved along vertical direction, and the compression bar C44 of vertical shape arrangement is provided on the second wedge block C42, and lock pin C43 is in
Two states, one are：The end of lock pin C43 extend to pilot hole side-wall outer side with lock C24 match to cover board C22 into
The locking position of row locking, secondly being：Compression bar C44, which is pushed, makes the first and second wedge block composition be slidably matched, the second wedge block C42
Downlink, the first wedge block C42, lock pin C43 one carry out the mobile unlatching for being used to open cover board C22 to the side far from lock
, it is provided with third spring C46 on compression bar, second spring C45, the restoring force of third spring C46 are provided on the first wedge block
So that compression bar, the second wedge block one uplink, the restoring force of second spring C45 makes lock pin C43, the first wedge block C41 one
It is moved to close to the side of lock C24, when lock pin C43 is in locking position, upper surface and the airplane parking area ontology of compression bar are in concordant shape
Arrangement.Cover board C22 is improved using the above structure so that cover board C22 easily can be opened and be dismantled, and helicopter passes through
Iron chains latch is on hitching post.
In short, hitching post provided by the invention, can easily open cover board C22, in addition hitching post is easy for assemble or unload, and
It can be grounded lightning-arrest.
The above is only a preferred embodiment of the present invention, it is noted that for the ordinary skill people of the art
For member, after knowing content described in the present invention, without departing from the principle of the present invention, it can also be made several
Same transformation and replacement, these convert and substitute on an equal basis and also should be regarded as belonging to the scope of protection of the present invention.
Claims (1)
1. a kind of helistop with locking device, it is characterised in that：Including airplane parking area ontology, set on airplane parking area ontology
The locking device for being equipped with fire-fighting equipment and helicopter being fixed is provided with protection network on the side wall of airplane parking area ontology；
Locking device includes flat panel, and bucket-shaped bucket is provided in the middle part of panel, and the notch section of bucket is more than slot
Hitching post is arranged in bucket for basal cross section, and the mast that hitching post is plugged respectively by casing and casing both ends is constituted, the abutting ends of two masts it
Between be provided with the first spring, hitching post is mounted in the pilot hole of airplane parking area ontology, and openable lid is provided at the notch of bucket
Plate, panel, cover board and the surface of airplane parking area ontology are arranged in concordant shape；One end of cover board is articulated and connected with airplane parking area ontology and should
Hinged edge is provided with the torsional spring so that cover board pop-up, and the cover board other end is extended into airplane parking area pilot hole lock, locks
It buckles and offers lockhole, the hole heart direction of lockhole is arranged in the horizontal direction, and lock pin, lock pin and drive are provided on the side wall of pilot hole
It moves its adjusting part moved along lockhole hole heart direction to be connected, adjusting part includes two mutually matched first and second wedges
Shape block, the first and second wedge block are mounted in the mounting hole opened up on pilot hole side wall, lock pin one end and first wedge far from lock
Shape block is connected, and the first wedge block moves in the horizontal direction, and the second wedge block is moved along vertical direction, is arranged on the second wedge block
There are the compression bar of vertical shape arrangement, lock pin to be in two states, one is：The end of lock pin extends to pilot hole side-wall outer side and lock
The locking position locked to cover board is matched, secondly being：Compression bar, which pushes, makes the first and second wedge block composition be slidably matched, the
One wedge block, lock pin one carry out the mobile open position for being used to open cover board to the side far from lock, and the is provided on compression bar
Three springs, are provided with second spring on the first wedge block, and the restoring force of third spring makes compression bar, in the second wedge block one
The restoring force of row, second spring makes lock pin, the first wedge block one be moved to close to the side of lock, and lock pin is in locking position
When, the upper surface of compression bar is arranged with airplane parking area ontology in concordant shape；
Airplane parking area ontology includes airplane parking area platform, and one layer of waterproof layer is equipped on airplane parking area platform, helicopter is parked on waterproof layer
Region be inlaid with shockproof landing plate, the surface of shockproof landing plate and waterproof layer surface of its periphery are shockproof in concordant shape arrangement
Landing plate is made of the supporting layer, buffer layer and elastic layer arranged from top to bottom, and the surface of supporting layer is arranged by anti-skidding paint structure
At skid resistant course, the thickness of supporting layer is 4mm, and the thickness of buffer layer is 20mm, and the thickness of elastic layer is 6mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610615973.5A CN106245543B (en) | 2015-03-31 | 2015-03-31 | Helistop with locking device |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610615973.5A CN106245543B (en) | 2015-03-31 | 2015-03-31 | Helistop with locking device |
| CN201510145044.8A CN104746443B (en) | 2015-03-31 | 2015-03-31 | Heliport |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510145044.8A Division CN104746443B (en) | 2015-03-31 | 2015-03-31 | Heliport |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106245543A CN106245543A (en) | 2016-12-21 |
| CN106245543B true CN106245543B (en) | 2018-10-19 |
Family
ID=53586646
Family Applications (7)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610619094.XA Active CN106223219B (en) | 2015-03-31 | 2015-03-31 | Helistop with fire-fighting equipment |
| CN201610614553.5A Active CN106223216B (en) | 2015-03-31 | 2015-03-31 | A kind of helistop being equipped with protective net |
| CN201610615817.9A Active CN106223217B (en) | 2015-03-31 | 2015-03-31 | A kind of helistop being equipped with locking device |
| CN201610615973.5A Active CN106245543B (en) | 2015-03-31 | 2015-03-31 | Helistop with locking device |
| CN201510145044.8A Active CN104746443B (en) | 2015-03-31 | 2015-03-31 | Heliport |
| CN201610614535.7A Active CN106223215B (en) | 2015-03-31 | 2015-03-31 | Helistop with protective net |
| CN201610618963.7A Active CN106223218B (en) | 2015-03-31 | 2015-03-31 | A kind of helistop being equipped with fire-fighting equipment |
Family Applications Before (3)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610619094.XA Active CN106223219B (en) | 2015-03-31 | 2015-03-31 | Helistop with fire-fighting equipment |
| CN201610614553.5A Active CN106223216B (en) | 2015-03-31 | 2015-03-31 | A kind of helistop being equipped with protective net |
| CN201610615817.9A Active CN106223217B (en) | 2015-03-31 | 2015-03-31 | A kind of helistop being equipped with locking device |
Family Applications After (3)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510145044.8A Active CN104746443B (en) | 2015-03-31 | 2015-03-31 | Heliport |
| CN201610614535.7A Active CN106223215B (en) | 2015-03-31 | 2015-03-31 | Helistop with protective net |
| CN201610618963.7A Active CN106223218B (en) | 2015-03-31 | 2015-03-31 | A kind of helistop being equipped with fire-fighting equipment |
Country Status (1)
| Country | Link |
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| CN (7) | CN106223219B (en) |
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| CN106223219B (en) * | 2015-03-31 | 2018-11-20 | 泰兴市智谷科技孵化器中心 | Helistop with fire-fighting equipment |
| CN108316166A (en) * | 2017-01-16 | 2018-07-24 | 广东博达机场建设实业有限公司 | A kind of electric rotary type helideck |
| WO2019144329A1 (en) * | 2018-01-25 | 2019-08-01 | 南通知航机电科技有限公司 | Helipad stabilization equipment |
| CN108755461A (en) * | 2018-05-31 | 2018-11-06 | 浙江圣翔航空科技有限公司 | Airplane parking area protection network automatic turning system and control method |
| CN108954123A (en) * | 2018-06-06 | 2018-12-07 | 安徽艳阳电气集团有限公司 | A kind of LED underground lamp with dedusting function |
| CN110295537B (en) * | 2019-07-02 | 2021-05-07 | 中冶南方工程技术有限公司 | Bridge adds base device of sound barrier |
| CN112393361A (en) * | 2020-11-19 | 2021-02-23 | 湖州鸿进自动化科技有限公司 | Air purifier's apron mounting structure |
| CN113346403B (en) * | 2021-02-25 | 2023-05-23 | 中国南方电网有限责任公司超高压输电公司贵阳局 | Unmanned aerial vehicle electric wire netting line patrol relay docking station |
| CN112982572B (en) * | 2021-03-06 | 2022-07-15 | 福建省双龙消防科技有限公司 | Ground fire hydrant capable of mixing water with fire fighting foam |
| CN117141637B (en) * | 2023-11-01 | 2024-01-02 | 烟台市北海海洋工程技术有限公司 | Marine helicopter deck with passive fire extinguishing system |
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-
2015
- 2015-03-31 CN CN201610619094.XA patent/CN106223219B/en active Active
- 2015-03-31 CN CN201610614553.5A patent/CN106223216B/en active Active
- 2015-03-31 CN CN201610615817.9A patent/CN106223217B/en active Active
- 2015-03-31 CN CN201610615973.5A patent/CN106245543B/en active Active
- 2015-03-31 CN CN201510145044.8A patent/CN104746443B/en active Active
- 2015-03-31 CN CN201610614535.7A patent/CN106223215B/en active Active
- 2015-03-31 CN CN201610618963.7A patent/CN106223218B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN106223217B (en) | 2019-01-22 |
| CN104746443B (en) | 2017-01-11 |
| CN106223215B (en) | 2018-11-27 |
| CN106223217A (en) | 2016-12-14 |
| CN106223219A (en) | 2016-12-14 |
| CN106223218A (en) | 2016-12-14 |
| CN106245543A (en) | 2016-12-21 |
| CN106223215A (en) | 2016-12-14 |
| CN106223218B (en) | 2018-11-16 |
| CN106223216B (en) | 2018-11-23 |
| CN104746443A (en) | 2015-07-01 |
| CN106223219B (en) | 2018-11-20 |
| CN106223216A (en) | 2016-12-14 |
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Effective date of registration: 20180910 Address after: 350299 S03 1 storefront, 99 of Chaoyang North Road, Changle City, Fuzhou, Fujian. Applicant after: Changle Jing Yuan Building Materials Technology Co., Ltd. Address before: 246002 148 Jixian South Road, Daguan District, Anqing, Anhui Applicant before: Wang Xuanming |
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Effective date of registration: 20201229 Address after: 224000 room 403-405, 4th floor, Yongning International Auto City, Yancheng City, Jiangsu Province (No. 2, Kaichuang Road, New District, Yandu District, Yancheng City, Jiangsu Province) (b) Patentee after: Yancheng Dongfang automobile Square Investment Development Co.,Ltd. Address before: 350299 S03 1 storefront, 99 of Chaoyang North Road, Changle City, Fuzhou, Fujian. Patentee before: Changle Jing Yuan Building Materials Technology Co.,Ltd. |
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