CN107054682A - A kind of track drawing aerocraft system - Google Patents
A kind of track drawing aerocraft system Download PDFInfo
- Publication number
- CN107054682A CN107054682A CN201710258113.5A CN201710258113A CN107054682A CN 107054682 A CN107054682 A CN 107054682A CN 201710258113 A CN201710258113 A CN 201710258113A CN 107054682 A CN107054682 A CN 107054682A
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- CN
- China
- Prior art keywords
- hawser
- aircraft
- track
- tractor
- gap
- 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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- 238000009434 installation Methods 0.000 claims abstract description 13
- 230000005540 biological transmission Effects 0.000 claims abstract description 6
- 239000000835 fiber Substances 0.000 claims description 3
- 238000000034 method Methods 0.000 description 4
- 238000012544 monitoring process Methods 0.000 description 4
- 238000013461 design Methods 0.000 description 2
- 238000003032 molecular docking Methods 0.000 description 2
- 230000009184 walking Effects 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 208000025157 Oral disease Diseases 0.000 description 1
- 238000004378 air conditioning Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000003344 environmental pollutant Substances 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 231100000719 pollutant Toxicity 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000013519 translation Methods 0.000 description 1
Classifications
-
- 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
- B64F1/22—Ground or aircraft-carrier-deck installations for handling aircraft
- B64F1/223—Ground or aircraft-carrier-deck installations for handling aircraft for towing aircraft
- B64F1/225—Vehicles specially adapted therefor, e.g. aircraft tow tractors
- B64F1/228—Vehicles specially adapted therefor, e.g. aircraft tow tractors remotely controlled; operating autonomously
-
- 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
- B64F1/04—Ground or aircraft-carrier-deck installations for launching aircraft
- B64F1/10—Ground or aircraft-carrier-deck installations for launching aircraft using self-propelled vehicles
-
- 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
- B64F3/00—Ground installations specially adapted for captive aircraft
- B64F3/02—Ground installations specially adapted for captive aircraft with means for supplying electricity to aircraft during flight
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Train Traffic Observation, Control, And Security (AREA)
Abstract
The invention provides a kind of track drawing aerocraft system, track side is provided with contact net, for providing electric energy to the electric supply installation on tractor, hawser is also equipped with tractor, electric supply installation is used to power to traveling motor, hawser retracting motor and hawser, and hawser one end is connected with aircraft, and its flying power is used as providing tractive force to aircraft, and electric energy is provided as its part and the energy of equipment to aircraft, hawser is additionally operable to aircraft transmission of control signals；Operation management and control center is used for the flying height and flight attitude for controlling aircraft, is additionally operable to control the operation of tractor；Shut down layer to be located above track, shutting down layer and being provided with is used for the gap that hawser passes through, and the center line of track coincides in the projection shut down on layer with the gap, the gap is provided with arc port with shutting down the intersection at layer edge, and the arc port and the gap are tangent.
Description
Technical field
The present invention relates to track traffic design field, more particularly to a kind of track drawing aerocraft system.
Background technology
Existing Urban Traffic Modes have walking, bicycle, kart, subway, train and aircraft etc., statistical investigation form
It is bright, less than the 5 kilometers preferred walkings of distances trip, less than the 10 kilometers preferred bicycles of distances trip, less than 30 kilometers distances trips
It is preferred that kart, less than the 100 kilometers preferred subways of distances trip, more than the 100 kilometers preferred trains of distances trip, 500 kilometers
The preferred aircraft of distance trip, but for comprehensive travel distance and psychological comfort degree, 50 kilometers to 200 kilometers of distance segment is above
The above-mentioned vehicles fail the region of covering, it is therefore desirable to a kind of trip is designed between 50 kilometers to 200 kilometers of distance segment
Distance and psychological comfort degree are attained by the mode of transportation of standard.
The content of the invention
To overcome the defect that above-mentioned prior art is present, the invention provides a kind of track drawing aerocraft system, including
Aircraft, tractor, track, shutdown layer and operation management and control center；
Traveling motor, hawser retracting motor, hawser retractable unit and electric supply installation, electric supply installation are housed on tractor
For being powered to traveling motor, hawser retracting motor and hawser, traveling motor is used to provide to the traveling of tractor
Be wound with hawser on electric power, hawser retractable unit, hawser retracting motor is used for the releasing and withdrawal for controlling hawser, one end of hawser with
Aircraft is connected, and hawser is used to provide tractive force as its flying power to aircraft, and is used as it to aircraft offer electric energy
The energy of part and equipment, hawser is additionally operable to aircraft transmission of control signals；
Track is used to provide course for tractor, and track is monorail track, track side provided with contact net, for
Electric supply installation provides electric energy, i.e., in tractor traveling process, electric supply installation is connected with contact net all the time；
The operation management and control center is used for the flying height and flight attitude for controlling aircraft, is additionally operable to control tractor
Operation, i.e., equal non-driver on aircraft and tractor, entirely with remote control run；
Shut down layer to be located above track, shutting down layer and being provided with is used for the gap that hawser passes through, the center line of track is shutting down layer
On projection coincided with the gap, the gap is provided with arc port with shutting down the intersection at layer edge, the arc port with
The gap is tangent, and the arc port is used in aircraft toward shutting down on layer during stop, and hawser, which can smoothly enter, shuts down
Layer, if hawser has angle in the projection of bottom surface and track centerline, in aircraft docking process, hawser can be with the arc
Mouth bumps against, and is introduced into then along the arc port in the gap.
It is preferred that, aircraft is laid out using blended wing-body, and its trailing edge is sequentially provided with interior from inside to outside along spanwise
Winglet is provided with wing flap, outer wing flap and aileron, wing wingtip, tail is provided with elevator, by interior wing flap, outer wing flap, aileron, small
The wing and elevator control the flying height and flight attitude of aircraft.
It is preferred that, the undercarriage of aircraft is laid out using trolley type, and nose-gear has turning function.
It is preferred that, the landing gate of aircraft is located at ventral, and the landing gate is set after putting down as airstair, aircraft top
There is escape hatch, landing gate and airstair unite two into one in order to save space.
It is preferred that, wheel is housed, traveling motor driving moment is advanced in orbit on tractor.
It is preferred that, hawser includes high strength fibre, power line, signal wire and lightning conducter, and hawser two ends, which are provided with, to be used to detect
The sensor of tension force, wherein power line are used to transmit electric power to aircraft, and signal wire is used to give aircraft transmission of control signals, and
By monitoring the data that the Sensor monitoring is obtained, the hawser automatic deploying and retracting during cruise can be achieved, to tackle turbulent flow.
It is preferred that, the operation management and control controls aircraft and tractor centrally through wireless signal, is easy to signal transmitting and receiving, saves
Maintaining cables work is gone.
A kind of track drawing aerocraft system that the present invention is provided, has the advantages that：
1st, without pilot on aircraft, railroad hauling car saves personnel cost also without driver；
2nd, using electric energy, non-pollutant discharge；
3rd, the system makes full use of city low latitude field, realizes that traffic is efficiently convenient, expands the trip mode of people；
4th, the system can be used for it is manned, freight, travel, go on patrol monitor etc. a variety of operation scenes.
Brief description of the drawings
Structural representation when Fig. 1 is the aircraft standby for takeoff of track drawing aerocraft system；
Structural representation when Fig. 2 is the aircraft preparation landing of track drawing aerocraft system；
Fig. 3 is the schematic three dimensional views of the tractor in track drawing aerocraft system；
Fig. 4 is the schematic rear view of the tractor in track drawing aerocraft system；
Fig. 5 is the schematic top plan view of the aircraft in track drawing aerocraft system.
Reference：Aircraft 1, interior wing flap 11, outer wing flap 12, aileron 13, winglet 14, tractor 2, traveling motor
21, hawser retracting motor 22, hawser retractable unit 23, hawser 24, electric supply installation 25, wheel 26, track 3 shuts down layer 4, contact
Net 5.
Embodiment
To make the purpose, technical scheme and advantage of the invention implemented clearer, below in conjunction with the embodiment of the present invention
Accompanying drawing, the technical scheme in the embodiment of the present invention is further described in more detail.In the accompanying drawings, identical from beginning to end or class
As label represent same or similar element or the element with same or like function.Described embodiment is the present invention
A part of embodiment, rather than whole embodiments.The embodiments described below with reference to the accompanying drawings are exemplary, it is intended to uses
It is of the invention in explaining, and be not considered as limiting the invention.Based on the embodiment in the present invention, ordinary skill people
The every other embodiment that member is obtained under the premise of creative work is not made, belongs to the scope of protection of the invention.
In the description of the invention, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", "front", "rear",
The orientation or position relationship of the instruction such as "left", "right", " vertical ", " level ", " top ", " bottom ", " interior ", " outer " is based on accompanying drawing institutes
The orientation or position relationship shown, is for only for ease of the description present invention and simplifies description, rather than indicate or imply meaning
Device or element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that to present invention guarantor
Protect the limitation of scope.
Below by specific embodiment, the present invention is described in further detail.
Specific embodiment：
As shown in Figures 1 and 2, the invention provides a kind of track drawing aerocraft system, including aircraft 1, tractor
2nd, track 3, shutdown layer 4 and operation management and control center；
As shown in Figures 3 and 4, traveling motor 21, hawser retracting motor 22, hawser folding and unfolding list are housed on tractor 2
Member 23, electric supply installation 25 and wheel 26, electric supply installation 25 are used for traveling motor 21, hawser retracting motor 22 and hawser 24
Power supply, traveling motor 21 is advanced on the track 3 for driving moment 26, and hawser 24, cable are wound with hawser retractable unit 23
Rope retracting motor 22 is used for the releasing and withdrawal for controlling hawser 24, and particularly, hawser retracting motor 22 is settable two, and two
Simultaneously work, if one failure, another can improve power and maintain two when operating efficiency；Tractor 2 can be with
The form for taking bicycle or many cars to organize into groups, to adapt to the tractive force demand and reliability requirement of different weight level aircraft 1.
One end of hawser 24 is connected with aircraft 1, and hawser 24 is used for dynamic as its flight to the offer tractive force of aircraft 1
Power, i.e. aircraft 1 rely only on the tractive force of hawser 24 as the power of flight, hawser 24 is also without engine, propeller and fuel oil
Electric energy, which is provided, to aircraft 1 is used as its part and the energy of equipment, such as flight control system, communication system, illuminator, air-conditioning
System etc.；Hawser 24 is additionally operable to the transmission of control signals of aircraft 1；Hawser 24 include high strength fibre, power line, signal wire and
Lightning conducter, the two ends of hawser 24 are provided with the sensor for being used for detecting tension force, and wherein power line is used to transmit electric power, letter to aircraft 1
Number line is used to give the transmission of control signals of aircraft 1, and by monitoring the data that the Sensor monitoring is obtained, can be achieved to cruise
The automatic deploying and retracting of hawser 24 in journey, to tackle turbulent flow.
Track 3 is used to provide course for tractor 2, and track 3 is monorail track, and the side of track 3 is provided with contact net 5,
For providing electric energy to electric supply installation 25, i.e., in the traveling process of tractor 2, electric supply installation 25 is connected with contact net 5 all the time, rail
Road 3 can both lay on the ground, overhead form can also be taken, the present embodiment middle orbit 3 is laid on the ground.
The operation management and control controls the flying height and flight attitude of aircraft 1 centrally through wireless signal, is additionally operable to
The operation of tractor 2 is controlled, i.e., equal non-driver on aircraft 1 and tractor 2 runs with remote control, is easy to signal to receive entirely
Hair, eliminates maintaining cables work.
As shown in Figures 1 and 2, shut down layer 4 and be located at the top of track 3, shutting down layer 4 and being provided with is used for the gap that hawser 24 passes through,
The center line of track 3 coincides in the projection shut down on layer 4 with the gap, the gap and the intersection for shutting down the edge of layer 4
Provided with arc port, the arc port and the gap are tangent, and the arc port is used in aircraft 1 toward stopping on shutdown layer 4
During, hawser 24, which can smoothly enter, shuts down layer 4, if hawser 24 has angle in the projection of bottom surface and the center line of track 3, is flying
In the docking process of row device 1, hawser can bump against with the arc port, be introduced into then along the arc port in the gap.
As shown in figure 5, aircraft 1 is laid out using blended wing-body, its trailing edge is set successively from inside to outside along spanwise
Have at interior wing flap 11, outer wing flap 12 and aileron 13, wing wingtip be provided with winglet 14, tail be provided with elevator, by interior wing flap 11,
Outer wing flap 12, aileron 13, winglet 14 and elevator control the flying height and flight attitude of aircraft 1；Of aircraft 1
Fall frame to be laid out using trolley type, nose-gear has turning function；The landing gate of aircraft 1 is located at ventral, and the landing gate is put
As airstair after lower, the top of aircraft 1 is provided with escape hatch, and landing gate and airstair unite two into one in order to save space.
When aircraft 1 takes off, aircraft 1 is by the launch of tractor 1, with the increase of air speed, tractor 1 by
Hawser 24 is gradually discharged, aircraft 1 is smoothly flown away from ground while controlling the control surface of aircraft 1；
When aircraft 1 lands, tractor 2 slows down and progressively withdraws hawser 24, makes the reduction height of aircraft 1, controls simultaneously
The control surface of aircraft 1 makes aircraft 1 keep stable flight attitude, and when aircraft 1 enters and shuts down 4 region of layer, rise and fall dress
Ground connection is put, aircraft 1 slows down, complete to land.
Layer 4 is shut down provided with storehouse, loading area is shut down, treats winged aircraft 1 in sideline loading area passenger loading, passenger
After boarding, moved on the runway of landing area, taken off after being connected with tractor 1 by translation machine.
In the track drawing aerocraft system, the design standard of aircraft 1 is the people of standard carrying 20,300 meters of cruising altitude,
180 kilometer per hours of cruising speed, landing ground run distance is not more than 200 meters, and the target operation distance of aircraft is 50 kms to 200
Km, run time typically at 20 minutes to 60 minutes, meet 50 kms to the comprehensive travel between 200 km distance segments away from
From the requirement that standard is all reached with psychological comfort degree.
The foregoing is only a specific embodiment of the invention, but protection scope of the present invention is not limited thereto, any
Those familiar with the art the invention discloses technical scope in, the change or replacement that can be readily occurred in, all should
It is included within the scope of the present invention.Therefore, protection scope of the present invention should using the scope of the claims as
It is accurate.
Claims (7)
1. a kind of track drawing aerocraft system, it is characterised in that including aircraft (1), tractor (2), track (3), shutdown
Layer (4) and operation management and control center；
Equipped with traveling motor (21), hawser retracting motor (22), hawser retractable unit (23) and power supply dress on tractor (2)
Put (25), electric supply installation (25) is used to give the power supply of traveling motor (21), hawser retracting motor (22) and hawser (24), advances
Motor (21) is used to provide to the traveling of tractor (2) is wound with hawser (24), hawser on electric power, hawser retractable unit (23)
Retracting motor (22) is used for the releasing and withdrawal for controlling hawser (24), and one end of hawser (24) is connected with aircraft (1), hawser
(24) be used to provide tractive force as its flying power to aircraft (1), and to aircraft (1) provide electric energy as its part and
The energy of equipment, hawser (24) is additionally operable to aircraft (1) transmission of control signals；
Track (3) is used to provide course for tractor (2), and track (3) is monorail track, and track (3) side is provided with contact
Net (5), for providing electric energy to electric supply installation (25)；
The operation management and control center is used for the flying height and flight attitude for controlling aircraft (1), is additionally operable to control tractor
(2) operation；
Shut down layer (4) to be located above track (3), shutting down layer (4) and being provided with is used for the gap that hawser (24) passes through, in track (3)
Heart line coincides in the projection shut down on layer (4) with the gap, and the gap is provided with arc with shutting down the intersection at layer (4) edge
Shape mouthful, the arc port and the gap are tangent.
2. track drawing aerocraft system according to claim 1, it is characterised in that aircraft (1) uses blended wing-body
Layout, its trailing edge is sequentially provided with interior wing flap (11), outer wing flap (12) and aileron (13), wing along spanwise from inside to outside
Winglet (14) is provided with wingtip, tail is provided with elevator.
3. track drawing aerocraft system according to claim 1, it is characterised in that the undercarriage of aircraft (1) is used
Trolley type is laid out, and nose-gear has turning function.
4. track drawing aerocraft system according to claim 1, it is characterised in that the landing gate of aircraft (1) is located at
Ventral, the landing gate put down after as airstair, escape hatch is provided with the top of aircraft (1).
5. track drawing aerocraft system according to claim 1, it is characterised in that wheel is housed on tractor (2)
(26), traveling motor (21) driving moment (26) is advanced on track (3).
6. track drawing aerocraft system according to claim 1, it is characterised in that hawser (24) includes high strength fiber
Dimension, power line, signal wire and lightning conducter, hawser (24) two ends are provided with the sensor for being used for detecting tension force.
7. track drawing aerocraft system according to claim 1, it is characterised in that the operation management and control is centrally through nothing
Line signal control aircraft (1) and tractor (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710258113.5A CN107054682B (en) | 2017-04-19 | 2017-04-19 | Track traction aircraft system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710258113.5A CN107054682B (en) | 2017-04-19 | 2017-04-19 | Track traction aircraft system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107054682A true CN107054682A (en) | 2017-08-18 |
| CN107054682B CN107054682B (en) | 2021-05-28 |
Family
ID=59601140
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710258113.5A Active CN107054682B (en) | 2017-04-19 | 2017-04-19 | Track traction aircraft system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107054682B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108528754A (en) * | 2018-05-03 | 2018-09-14 | 中航通飞华南飞机工业有限公司 | A kind of near-earth personally instructs the electricity collection car system of electric aircraft |
| CN109573085A (en) * | 2018-12-12 | 2019-04-05 | 中国航空工业集团公司西安飞机设计研究所 | A kind of rail mounted takeoff and landing system |
| WO2024061095A1 (en) * | 2022-09-21 | 2024-03-28 | 亿航智能设备（广州）有限公司 | Adjustment device for aircraft entering hangar and hangar |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2414990Y (en) * | 1999-06-08 | 2001-01-17 | 茹强 | Combined traction and hoisting motor vehicle |
| CN205442270U (en) * | 2016-04-01 | 2016-08-10 | 淮南国力液压装备有限公司 | Rope winding and unwinding devices moors |
| US20170057663A1 (en) * | 2015-08-25 | 2017-03-02 | Airbus (S.A.S.) | Device for maneuvering and immobilizing an aircraft on the ground |
| KR20170027609A (en) * | 2015-09-02 | 2017-03-10 | 한국모노레일주식회사 | Multicopter catching system |
| CN206087359U (en) * | 2016-08-31 | 2017-04-12 | 马宏 | Electronic ground car |
-
2017
- 2017-04-19 CN CN201710258113.5A patent/CN107054682B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2414990Y (en) * | 1999-06-08 | 2001-01-17 | 茹强 | Combined traction and hoisting motor vehicle |
| US20170057663A1 (en) * | 2015-08-25 | 2017-03-02 | Airbus (S.A.S.) | Device for maneuvering and immobilizing an aircraft on the ground |
| KR20170027609A (en) * | 2015-09-02 | 2017-03-10 | 한국모노레일주식회사 | Multicopter catching system |
| CN205442270U (en) * | 2016-04-01 | 2016-08-10 | 淮南国力液压装备有限公司 | Rope winding and unwinding devices moors |
| CN206087359U (en) * | 2016-08-31 | 2017-04-12 | 马宏 | Electronic ground car |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108528754A (en) * | 2018-05-03 | 2018-09-14 | 中航通飞华南飞机工业有限公司 | A kind of near-earth personally instructs the electricity collection car system of electric aircraft |
| CN109573085A (en) * | 2018-12-12 | 2019-04-05 | 中国航空工业集团公司西安飞机设计研究所 | A kind of rail mounted takeoff and landing system |
| WO2024061095A1 (en) * | 2022-09-21 | 2024-03-28 | 亿航智能设备（广州）有限公司 | Adjustment device for aircraft entering hangar and hangar |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107054682B (en) | 2021-05-28 |
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