CN204056288U - A kind of middle and short distance passenger transportation equipment - Google Patents
A kind of middle and short distance passenger transportation equipment Download PDFInfo
- Publication number
- CN204056288U CN204056288U CN201420551535.3U CN201420551535U CN204056288U CN 204056288 U CN204056288 U CN 204056288U CN 201420551535 U CN201420551535 U CN 201420551535U CN 204056288 U CN204056288 U CN 204056288U
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Abstract
A kind of middle and short distance passenger transportation equipment, belongs to technical field of aerospace.Form by without main power plant aircraft and ground corollary equipment.Fuselage, movable left wing, activity right flank, empennage, alighting gear, control system and airborne equipment is comprised without main power plant aircraft.The leading portion of fuselage interior is driving compartment, and posterior segment is main cabin.Movable left wing is identical with activity right flank structure to be symmetrically arranged in the left and right sides of the symmetrical vertical section of fuselage.Control system is used for the folding of control activity left wing and activity right flank, and controls this aircraft turn and pitching flying attitude.Ground corollary equipment comprises ground go-cart, body feedway and signal sending and receiving equipment.It adopts ground-launched mode to take off without main power plant aircraft, until synchronously opening gradually close to chaufeur manipulation activities left wing during airport of destination overhead and activity right flank simultaneously, drop subsequently, then finds landing runway and this aircraft by driver and slowly land.This equipment energy-saving high-efficiency environment-friendly and safety.
Description
Technical field
A kind of middle and short distance passenger transportation equipment, belongs to technical field of aerospace, particularly relates to a kind of passenger transportation equipment.
Background technology
Traditional passenger plane is with main power plants such as driving engine propelling unit and oil storage fuel-feeds system.The ratio that these devices account for passenger plane gross weight is quite large, and can produce resistance, causes the efficiency of flight not high, and complex structure, cost is high.Due to machine having fuel oil, easily blast during fault, safety factor is not high.
Summary of the invention
The object of the invention is the above-mentioned deficiency overcoming traditional passenger plane, the structure of inventing a kind of low cost is simple, lightweight, flight efficiency is high and the middle and short distance passenger transportation equipment that safety factor is high.
A kind of middle and short distance passenger transportation equipment, forms by without main power plant aircraft and ground corollary equipment.Fuselage, movable left wing, activity right flank, empennage, alighting gear, control system and airborne equipment is comprised without main power plant aircraft.The leading portion of fuselage interior is driving compartment, and posterior segment is main cabin.In fuselage, all seats are furnished with safety strap and crash helmet.Movable left wing is identical with activity right flank structure to be symmetrically arranged in the left and right sides of the symmetrical vertical section of fuselage, and is placed in fuselage roof.Empennage comprises vertical tail and tailplane.The yaw rudder of the fixed fin that vertical tail is fixed by front portion and rear portion activity forms; The elevating rudder of the horizontal stabilizer that tailplane is fixed by front portion and rear portion activity forms.Elevating rudder deflects up and down under the manipulation of control system, upward deflects and this aircraft can be made to come back, realize facing upward; The change of team of elevating rudder downward bias makes this aircraft bow, and realizes nutation.Yaw rudder is deflection under the manipulation of control system, and this aircraft is gone off course to the left or to the right.Alighting gear adopts convenient retracted wheel undercarriage.Control system and airborne equipment adopt the lithium battery power supply of convenient charging.Control system is used for the folding of control activity left wing and activity right flank, and controls this aircraft turn and pitching flying attitude.Adopt the folding of electric hydaulic mode control activity left wing and activity right flank.Airborne equipment comprises communication facilities, spiral shell top instrument and gauge panel.Ground corollary equipment comprises ground go-cart, body feedway and signal sending and receiving equipment.Body feedway is made up of launcher, sprocket wheel chain conveyor, motor and speed governing system.Launcher is fixedly mounted on level land, airport.Sprocket wheel chain conveyor is arranged on launcher, sprocket wheel chain conveyor is curved, extreme lower position namely this aircraft launch time reference position and level and angle close to 0 ° of angle, along with the rising of position, the angle of sprocket wheel chain conveyor and horizontal surface increases gradually, until during highest point and horizontal plane angle be 45 °.Sprocket wheel chain conveyor by motor through deceleration rear drive.Sprocket wheel chain conveyor outside face fixedly mounts propelling stake.This airframe rear lower center ofthe is provided with one piece of energy and the force-bearing piece advancing stake to match.Motor is by governor system control start-stop and rotating speed.Communication facilities on the signal sending and receiving equipment on ground and this aircraft carries out signal communication.The right and left of launcher upper surface is provided with guide rail, and two, the left and right wheel playing support and this aircraft that leads is used.The middle wheel of this aircraft runs on sprocket wheel chain conveyor upper surface.Described middle wheel refers to: the alighting gear of this aircraft refers to front-wheel for during first three point type; If the alighting gear of this aircraft refers to trailing wheel when being rear bikini.
The operation scheme of middle and short distance passenger transportation equipment of the present invention is: it adopts ground-launched mode to take off without main power plant aircraft, after passenger boarding, after movable left wing and activity right flank draw in by chaufeur, this aircraft is pushed into the reference position of body feedway by ground go-cart, start the motor of body feedway, the force-bearing piece of this aircraft rear lower is withstood in propelling stake on sprocket wheel chain conveyor, along with the acceleration of motor is rotated, this aircraft accelerates to advance to the direction of destination under the drive of the sprocket wheel chain conveyor of body feedway, though advance stake to turn to descending this aircraft of the guiding owing to being subject to launcher track to continue to move ahead towards launcher top after arriving the top of sprocket wheel chain conveyor, because inertia is to fly to the track of near parabolic with the overhead of horizontal surface angle airport of destination about at 45 ° after leaving launcher.After this aircraft leaves launcher, chaufeur manipulation alighting gear is regained in fuselage.When this aircraft reaches parabola summit, this aircraft is in the overhead of the center position between county of emission and destination substantially, synchronously open gradually close to chaufeur manipulation activities left wing during airport of destination overhead and activity right flank until this aircraft simultaneously, drop subsequently, then finds landing runway and this aircraft by driver and slowly land.Whole flight course is fly according to the flight path preset substantially.This aircraft skyborne degradation of energy should be considered when precalculating initial velocity and preset flight path and leave enough energy balance so that safe landing.During this aircraft arrival airport of destination overhead, kinetic energy is also more, and chaufeur should be driven this aircraft and spiral to shell the kinetic energy subtracting this aircraft in airport of destination overhead, reduces landing speed, so that safe landing.
The outstanding advantages of a kind of middle and short distance passenger transportation equipment of this invention is: energy-saving high-efficiency environment-friendly and safety.Owing to machine not having the main power plant such as driving engine propelling unit and oil storage fuel-feed system, structure is simple, lightweight, energy-conservationly lowers consumption again; Machine does not have fuel oil, greatly reduces burning and explosion safety accident.Take off to the process close to airport of destination overhead and be in closed configuration due to movable left wing and activity right flank, the resistance that this aircraft is subject to is little, and degradation of energy is little, and speed is fast, and the used time is short, and efficiency is high.This aircraft is in open mode from close to airport of destination overhead to the procedure activation left wing of landing and activity right flank, and this air speed is slack-off, convenient and safe landing.A set of ground corollary equipment can support the use without main power plant aircraft for multi rack, can be cost-saving widely.
A kind of middle and short distance passenger of the present invention transportation equipment is particularly suitable for the transport of the passenger between the shorter fixed point airport of two distances.
Accompanying drawing explanation
Fig. 1 is the schematic side view of the body feedway of a kind of middle and short distance passenger transportation equipment of the present invention, the apical position being in launcher without main power plant aircraft of the present invention in this figure; Fig. 2 is of the present invention without schematic top plan view when the left movable wing of main power plant aircraft and the gathering of right movable wing; Fig. 3 is schematic top plan view when opening without the left movable wing of main power plant aircraft and right movable wing of the present invention.
In figure, 1-without main power plant aircraft, 11-fuselage, the movable left wing of 12-, 13-activity right flank, 14-empennage, 141-fixed fin, 142-yaw rudder, 143-horizontal stabilizer, 144-elevating rudder, 15-alighting gear, 16-force-bearing piece, 2-launcher, 21-track, 3-sprocket wheel chain conveyor, 31-advances stake, level land, 4-airport.In Fig. 1, the direction of the larger arrow indication in the upper right corner represents the direction taken off without main power plant of the present invention, angle at 45 ° with horizontal surface.
Detailed description of the invention
Now 1 ~ 3 couple of the present invention is illustrated by reference to the accompanying drawings: a kind of middle and short distance passenger transportation equipment, forms by without main power plant aircraft 1 and ground corollary equipment.Fuselage 11, movable left wing 12, activity right flank 13, empennage 14, alighting gear 15, control system and airborne equipment is comprised without main power plant aircraft 1.The leading portion of fuselage 1 inside is driving compartment, and posterior segment is main cabin.In fuselage 1, all seats are furnished with safety strap and crash helmet.Movable left wing 12 is identical with activity right flank 13 structure is symmetrically arranged in the left and right sides of the symmetrical vertical section of fuselage 1, and is placed in fuselage 1 top.Empennage 14 comprises vertical tail and tailplane.The yaw rudder 142 of the fixed fin 141 that vertical tail is fixed by front portion and rear portion activity forms; The elevating rudder 144 of the horizontal stabilizer 143 that tailplane is fixed by front portion and rear portion activity forms.Elevating rudder 144 deflects up and down under the manipulation of control system, upward deflects and this aircraft 1 can be made to come back, realize facing upward; The change of team of elevating rudder downward bias makes this aircraft 1 bow, and realizes nutation.Yaw rudder 142 is deflection under the manipulation of control system, and this aircraft 1 is gone off course to the left or to the right.Alighting gear 15 adopts convenient retracted wheel undercarriage.Control system and airborne equipment adopt the lithium battery power supply of convenient charging.Control system is used for the folding of control activity left wing 12 and activity right flank 13, and controls this aircraft 1 and turn and pitching flying attitude.Adopt the folding of electric hydaulic mode control activity left wing 12 and activity right flank 13.Airborne equipment comprises communication facilities, spiral shell top instrument and gauge panel.Ground corollary equipment comprises ground go-cart, body feedway and signal sending and receiving equipment.Body feedway is made up of launcher 2, sprocket wheel chain conveyor 3, motor and speed governing system.Launcher 2 is fixedly mounted on level land, airport 4.Sprocket wheel chain conveyor 3 is arranged on launcher, sprocket wheel chain conveyor 3 is curved, the reference position of extreme lower position when namely this aircraft 1 is launched and level and angle close to 0 ° of angle, along with the rising of position, sprocket wheel chain conveyor 3 increases gradually with the angle of horizontal surface, until during highest point and horizontal plane angle be 45 °.Sprocket wheel chain conveyor 3 by motor through deceleration rear drive.Sprocket wheel chain conveyor 3 outside face fixedly mounts propelling stake 31.This aircraft 1 fuselage 11 rear lower center ofthe is provided with one piece of energy and the force-bearing piece 16 advancing stake 31 to match.Motor is by governor system control start-stop and rotating speed.Communication facilities on the signal sending and receiving equipment on ground and this aircraft 1 carries out signal communication.The right and left of launcher 2 upper surface is provided with guide rail 21, and two, the left and right wheel playing support and this aircraft 1 that leads is used.The middle wheel of this aircraft 1 runs on sprocket wheel chain conveyor 3 upper surface.Described middle wheel refers to: the alighting gear of this aircraft 1 refers to front-wheel for during first three point type; If the alighting gear of this aircraft 1 refers to trailing wheel when being rear bikini.
The operation scheme of middle and short distance passenger transportation equipment of the present invention is: it adopts ground-launched mode to take off without main power plant aircraft 1, after passenger boarding, after movable left wing 12 and activity right flank 13 draw in by chaufeur, this aircraft 1 is pushed into the reference position of body feedway by ground go-cart, start the motor of body feedway, the force-bearing piece 16 of this aircraft 1 rear lower is withstood in propelling stake 31 on sprocket wheel chain conveyor 3, along with the acceleration of motor is rotated, this aircraft 1 accelerates to advance to the direction of destination under the drive of the sprocket wheel chain conveyor 3 of body feedway, though advance stake 31 to turn to descending this aircraft 1 of the guiding owing to being subject to launcher 2 track 21 to continue to move ahead towards launcher 2 top after arriving the top of sprocket wheel chain conveyor 3, because inertia is to fly to the track of near parabolic with the overhead of horizontal surface angle airport of destination about at 45 ° after leaving launcher 2.After this aircraft 1 leaves launcher 2, chaufeur manipulation alighting gear 15 is regained in fuselage.When this aircraft 1 reaches parabola summit, this aircraft 1 is in the overhead of the center position between county of emission and destination substantially, synchronously open gradually close to chaufeur manipulation activities left wing 12 during airport of destination overhead and activity right flank 13 until this aircraft 1 simultaneously, drop 15 subsequently, then finds landing runway and this aircraft 1 by driver and slowly land.Whole flight course is fly according to the flight path preset substantially.This aircraft 1 skyborne degradation of energy should be considered when precalculating initial velocity and preset flight path and leave enough energy balance so that safe landing.When this aircraft 1 arrives airport of destination overhead, kinetic energy is also more, and chaufeur should be driven this aircraft 1 and spiral to shell the kinetic energy subtracting this aircraft 1 in airport of destination overhead, reduces landing speed, so that safe landing.
A set of ground corollary equipment can support the use without main power plant aircraft 1 for multi rack, can be cost-saving widely.
Claims (5)
1. a middle and short distance passenger transportation equipment, form by without main power plant aircraft (1) and ground corollary equipment, it is characterized in that: comprise fuselage (11), movable left wing (12), activity right flank (13), empennage (14), alighting gear (15), control system and airborne equipment without main power plant aircraft (1); The leading portion of fuselage (11) inside is driving compartment, and posterior segment is main cabin; In fuselage (11), all seats are furnished with safety strap and crash helmet; Movable left wing (12) is identical with activity right flank (13) structure to be symmetrically arranged in the left and right sides of fuselage (11) symmetrical vertical section, and is placed in fuselage (11) top; Empennage (14) comprises vertical tail and tailplane; Vertical tail is made up of fixed fin (141) and yaw rudder (142); Tailplane is made up of horizontal stabilizer (143) and elevating rudder (144); Control system and airborne equipment adopt the lithium battery power supply of convenient charging; Control system is used for the folding of control activity left wing (12) and activity right flank (13), and controls this aircraft (1) and turn and pitching flying attitude; Airborne equipment comprises communication facilities, spiral shell top instrument and gauge panel; Ground corollary equipment comprises ground go-cart, body feedway and signal sending and receiving equipment; Body feedway is made up of launcher (2), sprocket wheel chain conveyor (3), motor and speed governing system; Launcher (2) is fixedly mounted on level land, airport (4); Sprocket wheel chain conveyor (3) is arranged on launcher (2), sprocket wheel chain conveyor (3) is curved, extreme lower position namely this aircraft (1) launch time reference position and level and angle close to 0 ° of angle, along with the rising of position, the angle of sprocket wheel chain conveyor (3) and horizontal surface increases gradually, until during highest point and horizontal plane angle be 45 °; Sprocket wheel chain conveyor (3) by motor through deceleration rear drive; Sprocket wheel chain conveyor (3) outside face fixedly mounts propelling stake (31); This aircraft (1) fuselage (11) rear lower center ofthe is provided with one piece of energy and the force-bearing piece (16) advancing stake (31) to match; Motor is by governor system control start-stop and rotating speed; Communication facilities on the signal sending and receiving equipment on ground and this aircraft (1) carries out signal communication; The right and left of launcher (2) upper surface is provided with guide rail (21), and two, the left and right wheel playing support and this aircraft (1) that leads is used; The middle wheel of this aircraft (1) runs on sprocket wheel chain conveyor (3) upper surface.
2. a kind of middle and short distance passenger transportation equipment according to claim 1, is characterized in that: alighting gear (15) adopts convenient retracted wheel undercarriage.
3. a kind of middle and short distance passenger transportation equipment according to claim 2, is characterized in that: alighting gear (15) adopts first three point type or rear bikini wheel undercarriage.
4. a kind of middle and short distance passenger transportation equipment according to claim 1, is characterized in that: the folding adopting electric hydaulic mode control activity left wing (12) and activity right flank (13).
5. a kind of middle and short distance passenger transportation equipment according to claim 1, is characterized in that: a set of ground corollary equipment is launched and controlled multi rack without main power plant aircraft (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420551535.3U CN204056288U (en) | 2014-09-24 | 2014-09-24 | A kind of middle and short distance passenger transportation equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420551535.3U CN204056288U (en) | 2014-09-24 | 2014-09-24 | A kind of middle and short distance passenger transportation equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204056288U true CN204056288U (en) | 2014-12-31 |
Family
ID=52197851
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420551535.3U Withdrawn - After Issue CN204056288U (en) | 2014-09-24 | 2014-09-24 | A kind of middle and short distance passenger transportation equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204056288U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104192297A (en) * | 2014-09-24 | 2014-12-10 | 佛山市神风航空科技有限公司 | Short-distance passenger transportation equipment |
| WO2018184519A1 (en) * | 2017-04-07 | 2018-10-11 | 程建评 | Launcher and transport device using mountain as support and using natural force as power |
-
2014
- 2014-09-24 CN CN201420551535.3U patent/CN204056288U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104192297A (en) * | 2014-09-24 | 2014-12-10 | 佛山市神风航空科技有限公司 | Short-distance passenger transportation equipment |
| WO2018184519A1 (en) * | 2017-04-07 | 2018-10-11 | 程建评 | Launcher and transport device using mountain as support and using natural force as power |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20141231 Effective date of abandoning: 20151216 |
|
| C25 | Abandonment of patent right or utility model to avoid double patenting |