CN108316166A - A kind of electric rotary type helideck - Google Patents
A kind of electric rotary type helideck Download PDFInfo
- Publication number
- CN108316166A CN108316166A CN201710029343.4A CN201710029343A CN108316166A CN 108316166 A CN108316166 A CN 108316166A CN 201710029343 A CN201710029343 A CN 201710029343A CN 108316166 A CN108316166 A CN 108316166A
- Authority
- CN
- China
- Prior art keywords
- rotary type
- plate face
- ground connection
- helicopter
- positioning area
- 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
Links
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
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Road Paving Structures (AREA)
Abstract
The present invention provides a kind of electric rotary type helidecks; including helicopter platform, rotary type ground connection/positioning area plate face and electric drive; rotary type ground connection/positioning area the plate face is stayed with airplane parking area plane sets the rotation that handing-over seam facilitates ground connection/positioning area plate face; mobile pulley is installed between plate face and helideck; the transmission device is connected with ground connection/positioning area, and ground connection/positioning area plate can be rotated and then when starting electric device.The aircraft being parked on helicopter platform can be allowed to rotate that helicopter is allowed to take off in specified direction on airplane parking area using the technical solution of rotary type helicopter platform, reduce the limitation that barrier takes off to helicopter.Compared with prior art; technical solution provided by the invention uses electronic rotary type helideck; the construction range and use scope of airplane parking area can largely be improved; make helicopter safer in take-off process, while the science of whole system more is a kind of technological revolution to conventional helicopters level ground.
Description
Technical field
The present invention is applied to helideck field, especially a kind of electric rotary type helideck.
Background technology
Helicopter is due to unique flight characteristic, whether militarily or civilian man the helo is all played the part of emphatically
The role wanted, especially China, because city effect of the rapid development helicopter on fire-fighting and rescue and commercial use increasingly
Obviously.Simultaneously, the construction of helideck also in extensive development and carries out.Classification in helideck structure mainly has three
Kind it is concrete structure, steel construction, aluminium alloy structure respectively, while this several class is widely used in ground helideck, overhead
Helideck, ship helideck, offshore platform helideck.The general finite object requirement of taking off of helicopter, airplane parking area is wanted
Safety zone is set, while ground and overhead helideck there cannot be barrier into close take off with climbing face, in helideck water
Clear sector will be arranged in upper mounting plate.By restriction of obstacle, some need to be arranged helideck because of limit on conventional helicopters level ground
Barrier processed is not up to standard and can not build airplane parking area, and on built helideck, aircraft is easy to cause because shutting down anisotropy
Security risk is generated when helicopter takes off.It proposes in structure and to be in form all different from the market based on this background
There is a kind of electric rotary type helideck of helideck.
Invention content
In view of above, it is necessary to provide a kind of electric rotary type helideck, electronic rotary type helideck
Helicopter direction can be adjusted, helicopter is allowed to take off towards assigned direction, reduces restriction of obstacle, the peace that enhancing helicopter takes off
Full property is achieved by the following technical solution:
A kind of electric rotary type helideck includes ground connection/positioning area plate face of helicopter platform, embedded rotary type
And the electric device of control plate face rotation.
The ground connection/positioning area plate face using embedded plate face and concordant with airplane parking area platform, ground connection/positioning area plate face with
Helideck platform, which stays, sets the rotation that corner connection seam facilitates plate face.
The ground connection/installation pulley adds between plate face and airplane parking area simultaneously between positioning area plate face and helicopter platform
Pulley helps to be grounded/rotation of positioning area plate face and bear the pressure of takeoff and landing.
The ground connection of the airplane parking area/positioning area plate face is connected with electric drive, be grounded after opening electric device/
Positioning area plate face can rotate therewith.
The side of taking off of helicopter can be changed using electronic rotary type helideck by implementing technical scheme of the present invention
To reduction barrier limits while enhancing the safety protection helicopter and airplane parking area that helicopter takes off to airplane parking area
The personal safety of surrounding and property safety, whole system design more reasonable and science, are changed to the technology on conventional helicopters level ground
Leather and in-depth.
Description of the drawings
Fig. 1 is a kind of schematic diagram of electric rotary type helideck of the present invention.
Fig. 2 is a kind of vertical view of electric rotary type helideck of the present invention.
Specific implementation mode
The embodiment of the present invention is described in detail below in conjunction with attached drawing, but the present invention can be defined by the claims
Implement with the multitude of different ways of covering.
As shown in Figure 1, Fig. 1 is a kind of schematic diagram of electric rotary type helideck of the present invention, a kind of Novel electric
Dynamic rotary type helideck, including 1, helicopter platform 2, rotary type ground connection/positioning area plate face 3, electric device 4, pulley.
In Fig. 1, it can also be deck structure that helicopter platform 1, which can be concrete structure,.Rotary type ground connection/positioning
Area's platform drives the rotation of plate face, people to can adjust ground connection/positioning area plate face 2 by manipulating electric device 3 by electric device 3
Rotation angle.Rotary type ground connection/positioning area plate face 2 is using embedded and installation pulley 4, help between airplane parking area plane
Ground connection/rotation of positioning plate face 2 and the weight for bearing aircraft.
As shown in Fig. 2, Fig. 2 is a kind of vertical view of electric rotary type helideck of the present invention, handing-over seam 5 be
Rotary type ground connection/stayed between positioning area plate face and helicopter plane sets, and handing-over seam should not be equipped under too wide and handing-over seam
Drainage system.
In the present invention, since rotary type ground connection/positioning area plate face 2 is in contact but is not an overall structure face,
So the plate face will do reinforcement consolidation process.Pulley is due to that will bear prodigious pressure so with special material.
In a specific embodiment of the present invention, operation principle is that a kind of electric rotary type for being used in the design is straight
The machine of liter level ground has the function of rotation.When helicopter standby for takeoff helicopter land are driven by controlling electric device
The rotation in area, to allow the direction that helicopter is needed towards oneself to take off operation.Using technical side provided by the invention
Case, it is possible to reduce barrier limits the construction of helideck, the safety that enhancing helicopter takes off.
It these are only the preferred embodiment of the present invention, be not intended to restrict the invention, for those skilled in the art
For member, the invention may be variously modified and varied.Any modification made by all within the spirits and principles of the present invention,
Equivalent replacement, improvement etc., should all be included in the protection scope of the present invention.
Claims (4)
1. a kind of electric rotary type helideck, including helicopter platform, rotary type ground connection/positioning area plate face and
Electric drive, electric drive drive the rotation of rotary ground connection/positioning plate face.
2. a kind of electric rotary type helideck according to claim 1 is characterized in that the airplane parking area connects
Ground/positioning area can rotate, and can change helicopter by the rotation of ground connection/positioning area plate face after helicopter lands
Direction.
3. a kind of electric rotary type helideck according to claim 1 is characterized in that the airplane parking area connects
Ground/positioning area plate face is connected with electric drive, and ground connection/positioning area plate face can rotate therewith after opening electric device.
4. a kind of electric rotary type helideck according to claim 1, which is characterized in that the rotary type
Ground connection/positioning area plate face uses damascene structures, while adding pulley help between plate face and airplane parking area and being grounded/positioning area plate
Face rotates and bears the pressure of takeoff and landing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710029343.4A CN108316166A (en) | 2017-01-16 | 2017-01-16 | A kind of electric rotary type helideck |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710029343.4A CN108316166A (en) | 2017-01-16 | 2017-01-16 | A kind of electric rotary type helideck |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108316166A true CN108316166A (en) | 2018-07-24 |
Family
ID=62890838
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710029343.4A Pending CN108316166A (en) | 2017-01-16 | 2017-01-16 | A kind of electric rotary type helideck |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108316166A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108860644A (en) * | 2018-07-30 | 2018-11-23 | 广州黑鹰停机坪建设有限公司 | A kind of movable folding airplane parking area |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1145608A (en) * | 1994-04-04 | 1997-03-19 | 洛克希德·马丁公司 | A docking systemf for a lighter-than-air vehicle |
| JP2001514125A (en) * | 1997-08-28 | 2001-09-11 | エン．ファウ．ルシタヴェン シフォル | Apron for aircraft alignment and maintenance |
| KR101674344B1 (en) * | 2016-03-07 | 2016-11-08 | 사단법인 한국선급 | Helicopter Take-off and Landing Facilities with Movable Access Platform |
| CN106223215A (en) * | 2015-03-31 | 2016-12-14 | 王选明 | Helistop with protection network |
| CN106284110A (en) * | 2016-09-30 | 2017-01-04 | 深圳市天域智能有限公司 | Airplane parking area and control system thereof |
| CN205874998U (en) * | 2016-08-12 | 2017-01-11 | 抚顺欧柏丽实业股份有限公司 | Trapezoidal chamber deck that separates in helicopter air park |
| CN207510738U (en) * | 2017-02-15 | 2018-06-19 | 广东博达机场建设实业有限公司 | A kind of electric rotary type helideck |
-
2017
- 2017-01-16 CN CN201710029343.4A patent/CN108316166A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1145608A (en) * | 1994-04-04 | 1997-03-19 | 洛克希德·马丁公司 | A docking systemf for a lighter-than-air vehicle |
| JP2001514125A (en) * | 1997-08-28 | 2001-09-11 | エン．ファウ．ルシタヴェン シフォル | Apron for aircraft alignment and maintenance |
| CN106223215A (en) * | 2015-03-31 | 2016-12-14 | 王选明 | Helistop with protection network |
| KR101674344B1 (en) * | 2016-03-07 | 2016-11-08 | 사단법인 한국선급 | Helicopter Take-off and Landing Facilities with Movable Access Platform |
| CN205874998U (en) * | 2016-08-12 | 2017-01-11 | 抚顺欧柏丽实业股份有限公司 | Trapezoidal chamber deck that separates in helicopter air park |
| CN106284110A (en) * | 2016-09-30 | 2017-01-04 | 深圳市天域智能有限公司 | Airplane parking area and control system thereof |
| CN207510738U (en) * | 2017-02-15 | 2018-06-19 | 广东博达机场建设实业有限公司 | A kind of electric rotary type helideck |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108860644A (en) * | 2018-07-30 | 2018-11-23 | 广州黑鹰停机坪建设有限公司 | A kind of movable folding airplane parking area |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN203902789U (en) | Marine handrail structure | |
| CN107933914B (en) | Water-air amphibious sightseeing electric rotor aircraft | |
| CN204822073U (en) | Many rotor unmanned aerial vehicle's software protective housing | |
| EP2552771B1 (en) | Active platform for the landing of an aircraft on an access facility | |
| CN108466567A (en) | Multi-functional unmanned plane moors steady charging platform and method | |
| CN105088934B (en) | Flat rotation type bascule bridge | |
| CN103318405A (en) | Unmanned plane | |
| CN106976566A (en) | Level can be kept automatically and adjusts the aircraft landing platform of height | |
| CN205076045U (en) | Combined type aircraft of varistructure | |
| CN106240809A (en) | Novel guide based on fanjet controls multi-rotor aerocraft and control method | |
| CN108316166A (en) | A kind of electric rotary type helideck | |
| CN207510738U (en) | A kind of electric rotary type helideck | |
| CN204876139U (en) | Short building roof high wind suction developments suppression device | |
| CN107719695A (en) | The Flight Test Method on large-scale amphibious aircraft water surface pitching examination border | |
| CN207173991U (en) | Can automatically keep level and adjust height aircraft landing platform | |
| CN101462592A (en) | Propeller vertically taking off and landing flyer with rectifying device | |
| CN106058283A (en) | Heat radiation structure and method for fuel cell of unmanned aerial vehicle | |
| RU2664851C1 (en) | Vertical take-off and landing aircraft | |
| CN2036159U (en) | Gas rudder apparatus for jet planes | |
| CN207089674U (en) | A kind of aircraft laser lamp | |
| CN214464690U (en) | Wind power generator cabin with parking apron | |
| CN106741896A (en) | A kind of quadrotor | |
| CN209795758U (en) | Ladder-turning drift device of movable accommodation ladder | |
| CN104326084A (en) | Dish-shaped aircraft | |
| CN201604798U (en) | Remote-control rescue aircraft |
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 | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180724 |
|
| RJ01 | Rejection of invention patent application after publication |