CN108528736A - Light passenger's flight slide plate - Google Patents
Light passenger's flight slide plate Download PDFInfo
- Publication number
- CN108528736A CN108528736A CN201810520338.8A CN201810520338A CN108528736A CN 108528736 A CN108528736 A CN 108528736A CN 201810520338 A CN201810520338 A CN 201810520338A CN 108528736 A CN108528736 A CN 108528736A
- Authority
- CN
- China
- Prior art keywords
- slide plate
- flight
- riser
- main
- light passenger
- 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
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 11
- 239000000203 mixture Substances 0.000 claims abstract description 8
- 230000005611 electricity Effects 0.000 claims description 7
- 239000002828 fuel tank Substances 0.000 claims description 6
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 2
- 239000000956 alloy Substances 0.000 claims description 2
- 239000004917 carbon fiber Substances 0.000 claims description 2
- 230000002708 enhancing effect Effects 0.000 claims description 2
- 239000000446 fuel Substances 0.000 claims description 2
- 239000000463 material Substances 0.000 claims description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 2
- -1 oily filter Substances 0.000 claims description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims 1
- 229910052782 aluminium Inorganic materials 0.000 claims 1
- 239000004411 aluminium Substances 0.000 claims 1
- 230000008450 motivation Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000003344 environmental pollutant Substances 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 239000003350 kerosene Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 231100000719 pollutant Toxicity 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
-
- B64D27/026—
Abstract
The present invention provides a kind of light passenger's flight slide plates, and oil electric mixed dynamic mode is used to fly in the air with stance for people.The slide plate by fixer for feet part, upper layer it is main hold riser, lower layer master holds riser, duct engine, undercarriage, turbojet engine, oil piping system, connection column, flight control system and circuit system form, connection column composition strengthens structural strength, rigidity, turbojet engine provides the main lift that flies, duct engine provides additional lift and pose adjustment function, undercarriage plays the role of ground supports and landing buffer, fixed foot portion when being taken for personnel is fixed by foot, and also energy recycle device converts the kinetic energy that whirlpool is sprayed to electric energy and stores.Therefore, the present invention can take the liftoff flight of people's stance, have many advantages, such as small, light-weight, easy manipulation, can be used as single using flight tool in short-term.
Description
Technical field
The invention belongs to fields of carrying people to fly, and are related to a kind of manned vehicle, fly more particularly, to a kind of light passenger
Row slide plate is flown for a people with stance and while having oil electric mixed dynamic in the air.
Background technology
In recent years, due in size and cost advantage and wide application prospect, light passenger's aircraft just by
More and more concerns.Requirement in view of lightweight aircraft to flying speed and mobility is relatively low, generally all selects piston type
Petrol engine or electro-motor provide power for it.With people to the more attention of clean energy resource and aviation field to useless
The more stringent control of the pollutants such as gas, electric propulsion will be also more favored.
It will be appreciated that light passenger's aircraft should have the characteristics that small, light weight, VTOL, have a smooth flight, so
And the cruise duration of light passenger's aircraft existing in the prior art is all kept in check by motor and battery technology, can not do
To it is small and have certain cruise duration.
In addition, since turbojet engine thrust-weight ratio is big, pass through Throttle Opening Control low-response, it is difficult to meet aircraft held stationary
The requirement of flight attitude.
Therefore, it is badly in need of designing a kind of novel light passenger's flight slide plate, using high intensity, lightweight structure, and
Oil electric mixed dynamic solves the problems, such as cruise duration and has a smooth flight.
Invention content
Therefore, in order to solve the problems in the existing technology, the present invention proposes a kind of light passenger's flight slide plate, tool
There is the characteristics of small, light-weight, VTOL, have a smooth flight, cruise duration is solved the problems, such as by oil electric mixed dynamic.
The present invention provides a kind of light passenger's flight slide plates, and oil electric mixed dynamic mode is used to exist with stance for people
Airflight.The slide plate by fixer for feet part, upper layer it is main hold riser, lower layer master holds riser, duct engine, undercarriage, whirlpool are sprayed
Engine, oil piping system, connection column, flight control system and circuit system composition.
In the present invention, connection column is installed in that upper layer is main to hold riser and between lower layer master holds riser, whole for enhancing
Body structural strength and rigidity, fixer for feet part are installed in the main upper layer for holding riser in upper layer, turbojet engine with vertical direction
Slide plate centre position is mounted in a manner of 8~12 ° of angle symmetricals, duct engine is symmetrically mounted on slide plate both sides, oil circuit system
System, flight control system and circuit system are installed in that upper layer is main to hold riser and between lower layer master holds riser, undercarriage is installed in down
The main downside for holding riser of layer.
Preferably, upper layer it is main hold riser, lower layer master holds riser, undercarriage is made of high intensity carbon fiber material.Connection
Column is made of the aluminum alloy materials of high intensity.
In addition, turbojet engine is used to provide main lift, and the liter by controlling duct engine for entire slide plate
Force difference provides the gesture stability torque to entire slide plate.Oil piping system is made of main fuel tank, auxiliary fuel tank, oily filter, oil pump and group
It is connected via oil pipe between part, for being turbojet engine fuel feeding.Circuit system is adjusted by duct power supply, electricity, flies control power supply and company
Wiring cable forms.Electricity is called in providing power for duct engine.
Extraly, light passenger's flight slide plate further includes：Energy-recuperation system is used for the part kinetic energy of turbojet engine
It is converted into electric energy to store, with for flight control system and the power supply of duct engine.
Therefore, compared with traditional light passenger's aircraft in the prior art, the present invention uses turbojet engine and duct
Engine cooperation provides lift and control posture, reduces motor battery capacity requirement, and reduce battery weight, and by
In turbojet engine, small and thrust-weight ratio is big, can effectively reduce aircraft volume and weight.
Description of the drawings
Fig. 1 is the composite structural diagram of light passenger's flight slide plate of the present invention；
Fig. 2 is the circuit and oil circuit schematic diagram of light passenger's flight slide plate shown in FIG. 1.
Specific implementation mode
It will be appreciated that light passenger's flight slide plate of the present invention is by flight slide plate agent structure, turbojet engine, oil circuit system
The compositions such as system, duct engine, circuit system, flight control system, undercarriage, foot fixing device.
Specifically, there is flight slide plate main body upper layer and lower layer master to hold riser, and there is connection column to reinforce knot between two-ply
Structure intensity, rigidity, turbojet engine provide the main lift that flies, a TongAn such as same oil piping system, circuit system, flight control system
Between master holds riser, duct engine is symmetrically arranged on flight slide plate both sides, provides additional lift and pose adjustment function.
In addition, in the present invention, undercarriage is held mounted on lower layer master below riser, plays ground supports and landing buffer
Effect.Foot fixing device is installed on that upper layer is main to hold above riser, fixed foot portion when being taken for personnel.The light-duty load of the present invention
People's flight slide plate can take the liftoff flight of people's stance, have many advantages, such as small, light-weight, easy manipulation, can be used as one makes
With flight tool in short-term.
In the present invention, turbojet engine is for providing slide plate flight main lift, synchronous control throttle, and duct starts
Machine provides additional lift, poor by controlling to adjust lift, provides pose adjustment torque, light passenger's flight slide plate is enable to accomplish
It is small, it is light-weight, it has a smooth flight.In addition, the slide plate of the present invention also has energy recycle device, it can be by the dynamic of turbojet engine
Electric energy can be converted into store, for providing the energy for flight control system and duct engine.
The present invention is described in detail for 1-2 and specific implementation mode below in conjunction with the accompanying drawings.
As shown in Figure 1, the basic structure form of light passenger's aircraft of the present invention is given, by fixer for feet part
(1), upper layer it is main hold riser (2), lower layer master holds riser (3), duct engine (4), undercarriage (5), turbojet engine (6), oil
Road system, connection column (8), flight control system (9), circuit system composition.
Upper layer is main to hold riser (2) and lower layer master holds installation connection column (8) between riser (3), play reinforcement structure intensity,
Stiffness.Fixer for feet part (1) is mounted on the main top for holding riser (2) in upper layer, and turbojet engine (6) is in 8 with vertical direction
~12 ° are symmetrically arranged on flight slide plate centre position, and duct engine (4) is symmetrically arranged on flight slide plate both sides, oil piping system,
Flight control system (9), circuit system installation upper layer be main to hold riser (2) and between lower layer master holds riser (3), undercarriage (5) is mounted on
Lower layer master holds on the downside of riser (3).
As shown in Fig. 2, giving the circuit and oil circuit composition figure of Fig. 1 light passenger's flight slide plates.Specifically, circuit system
It adjusts (9) to power from duct power supply (10) to electricity, is to fly control by flying control power supply (15) by being converted into duct engine (4) power supply
(12) it powers, flies control (12) and handle telecommand, resolve attitude of flight vehicle, adjust (9) to send instruction to electricity, control duct engine
(4) rotating speed.Oil piping system stores aviation kerosine by main fuel tank (11), is connected to auxiliary fuel tank (7), being connected to oily filter (13) will be in oil
Impurity removal, be connected to oil pump (14), oil be finally transported to turbojet engine (6).
In conclusion light passenger's flight slide plate of the present invention, reduces motor battery capacity requirement, and reduce electricity
Pond weight, and since turbojet engine is small and thrust-weight ratio is big, aircraft volume and weight can be effectively reduced.
It is not specified in the present invention and partly belongs to techniques known.
Claims (8)
1. a kind of light passenger's flight slide plate, uses oil electric mixed dynamic mode to fly in the air with stance for people, special
Sign is, by fixer for feet part, upper layer it is main hold riser, lower layer master holds riser, duct engine, undercarriage, turbojet engine, oil
Road system, connection column, flight control system and circuit system composition,
Wherein,
The connection column is installed in that the upper layer is main to hold riser and between lower layer master holds riser, strong for enhancing overall structure
Degree and rigidity,
The fixer for feet part is installed in the main upper layer for holding riser in the upper layer, and step is fixed when for being taken for people,
The turbojet engine by with vertical direction in 8~12 ° it is symmetrical in a manner of be mounted on slide plate centre position,
The duct engine is symmetrically mounted on slide plate both sides,
The oil piping system, the flight control system and the circuit system are installed in that the upper layer is main to hold riser and the lower layer
Between master holds riser,
The undercarriage is installed in the downside that the lower layer master holds riser, for carrying out ground supports and landing buffer.
2. light passenger's flight slide plate according to claim 1, which is characterized in that the upper layer is main hold riser, it is described under
Layer master holds riser, the undercarriage is made of high intensity carbon fiber material.
3. light passenger's flight slide plate according to claim 1, which is characterized in that described to connect aluminium of the column by high intensity
Alloy material is made.
4. light passenger's flight slide plate according to claim 1, which is characterized in that the turbojet engine is for being entire
Slide plate provides main lift, and the lift by controlling the duct engine is poor, provides the gesture stability to entire slide plate
Torque.
5. light passenger's flight slide plate according to claim 4, which is characterized in that the oil piping system is by main fuel tank, pair
It is connected via oil pipe between fuel tank, oily filter, oil pump composition and component, for being the turbojet engine fuel feeding.
6. light passenger's flight slide plate according to claim 4, which is characterized in that the circuit system by duct power supply,
Electricity is adjusted, flies control power supply and cable composition.
7. light passenger's flight slide plate according to claim 6, which is characterized in that the electricity is called to be sent out in for the duct
Motivation provides power.
8. light passenger's flight slide plate according to claim 7, which is characterized in that further include：
Energy-recuperation system is stored for converting the part kinetic energy of the turbojet engine to electric energy, to fly to be described
Control system and duct engine power supply.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810520338.8A CN108528736A (en) | 2018-05-25 | 2018-05-25 | Light passenger's flight slide plate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810520338.8A CN108528736A (en) | 2018-05-25 | 2018-05-25 | Light passenger's flight slide plate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108528736A true CN108528736A (en) | 2018-09-14 |
Family
ID=63472877
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810520338.8A Pending CN108528736A (en) | 2018-05-25 | 2018-05-25 | Light passenger's flight slide plate |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108528736A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113716039A (en) * | 2021-08-30 | 2021-11-30 | 山东元一动力科技有限公司 | Jet power flight pedal device |
| CN113911374A (en) * | 2021-11-12 | 2022-01-11 | 北京航空航天大学 | Oil moves duct engine mounting structure |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104290907A (en) * | 2014-10-15 | 2015-01-21 | 西南科技大学 | Novel hybrid vertical/short take-off and landing (V/STOL) unmanned aerial vehicle |
| CN204341404U (en) * | 2014-12-17 | 2015-05-20 | 曹运 | Photoelectric intelligent flight slide plate |
| CN105457256A (en) * | 2015-12-22 | 2016-04-06 | 江苏数字鹰科技发展有限公司 | Flying skateboard |
| CN205627020U (en) * | 2016-03-15 | 2016-10-12 | 欧泽金 | Slide that suspends from electrified source of remote control |
| US20160340035A1 (en) * | 2014-01-07 | 2016-11-24 | 4525612 Canada Inc. Dba Maginaire | Personal flight vehicle |
| CN205906213U (en) * | 2016-08-19 | 2017-01-25 | 阚震林 | Can freely turn to and self -balancing recovering flight slide a steering system |
| CN206087296U (en) * | 2016-10-13 | 2017-04-12 | 中交遥感载荷（北京）科技有限公司 | Flight slide plate structure |
| CN106994874A (en) * | 2017-03-14 | 2017-08-01 | 北京航空航天大学 | Suspended and promoted and the dual-purpose novel intelligent walking-replacing tool of ground roll-out based on wind-force |
| CN107308630A (en) * | 2016-04-27 | 2017-11-03 | 江苏数字鹰科技发展有限公司 | A kind of flight slide plate using brand-new control mode |
-
2018
- 2018-05-25 CN CN201810520338.8A patent/CN108528736A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20160340035A1 (en) * | 2014-01-07 | 2016-11-24 | 4525612 Canada Inc. Dba Maginaire | Personal flight vehicle |
| CN104290907A (en) * | 2014-10-15 | 2015-01-21 | 西南科技大学 | Novel hybrid vertical/short take-off and landing (V/STOL) unmanned aerial vehicle |
| CN204341404U (en) * | 2014-12-17 | 2015-05-20 | 曹运 | Photoelectric intelligent flight slide plate |
| CN105457256A (en) * | 2015-12-22 | 2016-04-06 | 江苏数字鹰科技发展有限公司 | Flying skateboard |
| CN205627020U (en) * | 2016-03-15 | 2016-10-12 | 欧泽金 | Slide that suspends from electrified source of remote control |
| CN107308630A (en) * | 2016-04-27 | 2017-11-03 | 江苏数字鹰科技发展有限公司 | A kind of flight slide plate using brand-new control mode |
| CN205906213U (en) * | 2016-08-19 | 2017-01-25 | 阚震林 | Can freely turn to and self -balancing recovering flight slide a steering system |
| CN206087296U (en) * | 2016-10-13 | 2017-04-12 | 中交遥感载荷（北京）科技有限公司 | Flight slide plate structure |
| CN106994874A (en) * | 2017-03-14 | 2017-08-01 | 北京航空航天大学 | Suspended and promoted and the dual-purpose novel intelligent walking-replacing tool of ground roll-out based on wind-force |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113716039A (en) * | 2021-08-30 | 2021-11-30 | 山东元一动力科技有限公司 | Jet power flight pedal device |
| CN113911374A (en) * | 2021-11-12 | 2022-01-11 | 北京航空航天大学 | Oil moves duct engine mounting structure |
| CN113911374B (en) * | 2021-11-12 | 2023-06-20 | 北京航空航天大学 | Oil moves duct engine mounting structure |
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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 | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180914 |