CN106274324A - A kind of jet-propelled manned vehicle - Google Patents
A kind of jet-propelled manned vehicle Download PDFInfo
- Publication number
- CN106274324A CN106274324A CN201610691369.0A CN201610691369A CN106274324A CN 106274324 A CN106274324 A CN 106274324A CN 201610691369 A CN201610691369 A CN 201610691369A CN 106274324 A CN106274324 A CN 106274324A
- Authority
- CN
- China
- Prior art keywords
- motor
- frame
- spherical hinge
- hinge holder
- undercarriage
- 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
- 230000005611 electricity Effects 0.000 claims abstract description 15
- 238000009434 installation Methods 0.000 description 2
- HBBGRARXTFLTSG-UHFFFAOYSA-N Lithium ion Chemical compound [Li+] HBBGRARXTFLTSG-UHFFFAOYSA-N 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 229910001416 lithium ion Inorganic materials 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/02—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded
- B64C29/04—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded characterised by jet-reaction propulsion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
Abstract
The present invention provides a kind of jet-propelled manned vehicle, including 4 swing spans, undercarriage, 4 helical springs, frame, left safety rail, seat, right safety rail, controller, snap close, 2 support rings etc., frame side is made and be horizontally fixed on to described extension sleeve by hollow square tube, telescopic arm it is slidably fitted with in extension sleeve, the slip of telescopic arm is controlled by electricity cylinder B, described support ring is fixed on the front end of telescopic arm, 6 spherical hinge holder A are uniformly installed on the top of support ring, 6 spherical hinge holder B are installed in retainer ring bottom；The present invention uses turbojet engine to provide lift for aircraft, has the feature of hang time length, and duct and propeller by rear portion can provide, for aircraft, the power advanced very easily simultaneously.
Description
Technical field
The present invention relates to manned vehicle technical field, particularly to a kind of jet-propelled manned vehicle.
Background technology
Manned vehicle is made up of microjet and steerable system.The thrust that electromotor produces be enough to make single liter
Empty；Steerable system is in order to keep balance and change of flight state.Whole device is carried (being contained in back) by single more, can complete
Rise, decline, the actions such as peace flies of hovering.Due to the restriction of weight and volume, the fuel that individual lift device is carried is by lithium ion
Battery provides power, is only capable of for electromotor work several tens of seconds, and flying distance and airborne period are the shortest, is therefore badly in need of a kind of stagnant
The empty time is long, the manned vehicle of flexible operation.
Summary of the invention
For the problems referred to above, the present invention provides a kind of jet-propelled manned vehicle, and it uses turbojet engine to be aircraft
Thering is provided lift, have the feature of hang time length, duct and propeller by rear portion can be aircraft very easily simultaneously
The power advanced is provided.
Technical scheme used in the present invention is: a kind of jet-propelled manned vehicle, including undercarriage, 4 helical springs,
Frame, left safety rail, seat, right safety rail, controller, snap close, 2 support rings, 2 lift unit, landing pack, electricity
Cylinder C, slide block, motor A, turning rack, duct, brushless electric machine, propeller, driven gear, driving gear, motor B,
Electric machine support, 2 sleeve pipes, guide rails, 4 driver elements, it is characterised in that: 2 described lift unit are symmetrical at upper rack 2
Side, each lift unit includes that 6 electric cylinder A, retainer ring, turbojet engine, telescopic arm, extension sleeve, electricity cylinder B, 6 ball pivots prop up
Frame A, 6 spherical hinge holder B, frame side is made and be horizontally fixed on to described extension sleeve by hollow square tube, at extension sleeve
In be slidably fitted with telescopic arm, the slip of telescopic arm by electricity cylinder B control, described support ring is fixed on the front end of telescopic arm,
The top of support ring is uniformly provided with 6 spherical hinge holder A, is provided with 6 spherical hinge holder B, 6 described electricity in retainer ring bottom
The two ends of cylinder A are respectively hinged on 6 spherical hinge holder A and 6 spherical hinge holder B successively, and described turbojet engine is arranged on solid
Central authorities and its spout of determining ring are downward；
Described seat is arranged on the bottom of frame, is installed with 4 helical springs in the bottom of base, under helical spring
Portion is fixedly linked with undercarriage, is respectively provided with a driver element on four angles of undercarriage, and each driver element includes drawing
Spring, swing span, wheel, motor C, the upper end of described swing span is hingedly mounted on undercarriage, described extension spring one
End is hinged on the centre position of swing arm, and the other end is hinged on the bottom of undercarriage, and described motor C is fixed on swing arm
Bottom, motor C is provided with wheel；
Described left safety rail and right safety rail are separately mounted to the left and right sides of frame, in left safety rail and right safety
Being respectively provided with a circular hole, left safety rail and right safety rail on handrail uses snap close to connect in use, and described snap close divides
It is not inserted in two circular holes；Described controller is fixedly mounted on the top of right safety rail；
Described guide rail is vertically installed at the back of frame, and described slide block is slidably mounted on guide rail, and slide block is slidably mounted on
On guide rail, sliding up and down of slide block is controlled by electricity cylinder C, is provided with motor A at the rear portion of slide block；Before described turning rack
End middle position is installed with fixing axle, and the rear inside at turning rack is respectively provided with a bearing pin, and described motor is installed
Frame is arranged on the outside of turning rack, and turning rack is fixedly mounted on the motor shaft of motor A by fixing axle；
One electric machine support is installed in the middle of described duct, is installed with 2 sleeve pipes in the outside of duct, at the set in left side
Being installed with driven gear on pipe, duct is separately mounted on 2 bearing pins inside turning rack by 2 sleeves, described
Motor B be arranged on motor mounting plate, the motor shaft of motor B is provided with driving gear, described active
Gear intermeshes with driven gear, and described brushless electric machine is arranged on the center of electric machine support, at the electricity of brushless electric machine
Propeller is installed on arbor；Described landing pack is fixed on frame top.
Owing to present invention employs technique scheme, the invention have the advantages that
The present invention uses turbojet engine to provide lift for aircraft, has the feature of hang time length, simultaneously by rear portion
Duct and propeller can provide, for aircraft, the power advanced very easily.
Accompanying drawing explanation
The integral installation distribution structure schematic diagram of Fig. 1, Fig. 2, Fig. 3 present invention.
Fig. 4 is duct structural representation of the present invention.
Fig. 5 is the turning rack structural representation of the present invention.
Fig. 6 is the turbojet engine scheme of installation of the present invention.
Drawing reference numeral: 1-swing span；2-undercarriage；3-helical spring；4-frame；The left safety rail of 5-；6-seat；7-is right
Safety rail；8-controller；9-snap close；10-support ring；11-electricity cylinder A；12-retainer ring；13-turbojet engine；14-stretches
Arm；15-extension sleeve；16-electricity cylinder B；17-lands pack；18-electricity cylinder C；19-slide block；20-motor A；21-turns to and props up
Frame；22-duct；23-brushless electric machine；24-propeller；25-driven gear；26-driving gear；27-motor B；28-motor
Support；29-guide rail；30-wheel；31-motor mounting rack；32-fixes axle；33-spherical hinge holder A；34-spherical hinge holder B；35-walks
Enter motor C；36-sleeve pipe；37-extension spring；38-bearing pin.
Detailed description of the invention
Below by embodiment, and combine accompanying drawing, technical scheme is described in further detail.
Embodiment
As shown in Figure 1, Figure 2, shown in Fig. 3, Fig. 4, Fig. 5, Fig. 6, a kind of jet-propelled manned vehicle, including 2,4 spiral bullets of undercarriage
Spring 3, frame 4, left safety rail 5, seat 6, right safety rail 7, controller 8, snap close 10,2 lift lists of 9,2 support rings
Unit, landing pack 17, electricity cylinder C18, slide block 19, motor A20, turning rack 21, duct 22, brushless electric machine 23, propeller
24, driven gear 25, driving gear 26, motor B27,28,2 sleeve pipes 36 of electric machine support, 29,4 driver elements of guide rail,
It is characterized in that: 2 described lift unit are symmetrical in side, frame 4 top 2, each lift unit includes 6 electric cylinder A11, consolidates
Determine ring 12, turbojet engine 13, telescopic arm 14, extension sleeve 15, electricity cylinder B16,6 spherical hinge holder A33,6 spherical hinge holders
B34, described extension sleeve 15 is made and is horizontally fixed on frame 4 side by hollow square tube, slides and pacify in extension sleeve 15
Equipped with telescopic arm 14, the slip of telescopic arm 14 is controlled by electricity cylinder B16, and described support ring 10 is fixed on the front end of telescopic arm 14,
6 spherical hinge holder A33 are uniformly installed on the top of support ring 10, in retainer ring 12 bottom, 6 spherical hinge holder B34 are installed,
The two ends of 6 described electric cylinder A11 are respectively hinged on 6 spherical hinge holder A33 and 6 spherical hinge holder B34 successively, described whirlpool
Fuel-injection engine 13 is arranged on the central authorities of retainer ring 12 and its spout is downward；
Described seat 6 is arranged on the bottom of frame 4, is installed with 4 helical springs 3, helical spring 3 in the bottom of base
Bottom be fixedly linked with undercarriage 2, four angles of undercarriage 2 are respectively provided with a driver element, each driver element
Including extension spring 37, swing span 1, wheel 30, motor C35, the upper end of described swing span 1 is hingedly mounted on undercarriage 2
On, described extension spring 37 one end is hinged on the centre position of swing arm, and the other end is hinged on the bottom of undercarriage 2, described step
Enter motor C35 and be fixed on the bottom of swing arm, motor C35 is provided with wheel 30；
Described left safety rail 5 and right safety rail 7 are separately mounted to the left and right sides of frame 4, on left safety rail 5 and the right side
Being respectively provided with a circular hole on safety rail 7, left safety rail 5 and right safety rail 7 use snap close 9 to connect in use, described
Snap close 9 be respectively inserted in two circular holes；Described controller 8 is fixedly mounted on the top of right safety rail 7；
Described guide rail 29 is vertically installed at the back of frame 4, and described slide block 19 is slidably mounted on guide rail 29, and slide block 19 is sliding
Moving and be arranged on guide rail 29, sliding up and down of slide block 19 is controlled by electricity cylinder C18, is provided with motor at the rear portion of slide block 19
A20；Described turning rack 21 front center position is installed with fixing axle 32, and the rear inside at turning rack 21 respectively sets
Having a bearing pin 38, described motor mounting rack 31 to be arranged on the outside of turning rack 21, turning rack 21 is by fixing axle 32
It is fixedly mounted on the motor shaft of motor A20；
In the middle of described duct 22, an electric machine support 28 is installed, is installed with 2 sleeve pipes 36 in the outside of duct 22,
Being installed with driven gear 25 on the sleeve pipe 36 in left side, duct 22 is separately mounted to inside turning rack 21 by 2 sleeves
2 bearing pins 38 on, described motor B27 is arranged on motor mounting plate, on the motor shaft of motor B27 install
Having driving gear 26, described driving gear 26 to intermesh with driven gear 25, described brushless electric machine 23 is arranged on motor
The center of support 28, is provided with propeller 24 on the motor shaft of brushless electric machine 23；Described landing pack 17 is fixed on
Frame 4 top.
Operation principle of the present invention: the present invention uses 2 turbojet engines 13 to provide lift for aircraft, and the eruption of each whirlpool is dynamic
The attitude of machine 13 can be jointly controlled by 6 electric cylinder A11, and the distance between two turbojet engines 13 and frame 4 is passed through
Telescopic arm 14 adjusts；There is provided forward thrust by the propeller 24 at rear portion for aircraft, adjust its thrust position by slide block 19,
Control its thrust direction by motor A20 and motor B27, the when of traveling on the ground, use four wheel 30 row
Walk, release parachute safe landing in case of emergency.
Claims (1)
1. a jet-propelled manned vehicle, including undercarriage (2), 4 helical springs (3), frame (4), left safety rails
(5), seat (6), right safety rail (7), controller (8), snap close (9), 2 support rings (10), 2 lift unit, parachutes
Bag (17), electricity cylinder C(18), slide block (19), motor A(20), turning rack (21), duct (22), brushless electric machine (23), spiral shell
Rotation oar (24), driven gear (25), driving gear (26), motor B(27), electric machine support (28), 2 sleeve pipes (36), lead
Rail (29), 4 driver elements, it is characterised in that: 2 described lift unit are symmetrical at side, frame (4) top 2, each lift
Unit includes 6 electric cylinder A(11), retainer ring (12), turbojet engine (13), telescopic arm (14), extension sleeve (15), electricity cylinder B
(16), 6 spherical hinge holder A(33), 6 spherical hinge holder B(34), described extension sleeve (15) is made up and level of hollow square tube
Being fixed on frame (4) side, be slidably fitted with telescopic arm (14) in extension sleeve (15), the slip of telescopic arm (14) is by electricity cylinder
B(16) controlling, described support ring (10) is fixed on the front end of telescopic arm (14), is uniformly provided with on the top of support ring (10)
6 spherical hinge holder A(33), in retainer ring (12) bottom, 6 spherical hinge holder B(34 are installed), 6 described electric cylinder A(11)
Two ends are respectively hinged at 6 spherical hinge holder A(33 successively) and 6 spherical hinge holder B(34) on, described turbojet engine (13) peace
The central authorities and its spout that are contained in retainer ring (12) are downward；
Described seat (6) is arranged on the bottom of frame (4), is installed with 4 helical springs (3), spiral shell in the bottom of base
The bottom of rotation spring (3) is fixedly linked with undercarriage (2), is respectively provided with a driver element on four angles of undercarriage (2),
Each driver element includes extension spring (37), swing span (1), wheel (30), motor C(35), described swing span (1) upper
End is hingedly mounted on undercarriage (2), and described extension spring (37) one end is hinged on the centre position of swing arm, and the other end is hinged
In the bottom of undercarriage (2), described motor C(35) it is fixed on the bottom of swing arm, at motor C(35) upper install
There is wheel (30)；
Described left safety rail (5) and right safety rail (7) are separately mounted to the left and right sides of frame (4), hold up in left safety
It is respectively provided with a circular hole, left safety rail (5) and right safety rail (7) on hands (5) and right safety rail (7) to use in use
Snap close (9) connects, and described snap close (9) is respectively inserted in two circular holes；Described controller (8) is fixedly mounted on right safety and holds up
The top of hands (7)；
Described guide rail (29) is vertically installed at the back of frame (4), and described slide block (19) is slidably mounted on guide rail (29),
Slide block (19) is slidably mounted on guide rail (29), sliding up and down by electricity cylinder C(18 of slide block (19)) control, after slide block (19)
Portion is provided with motor A(20)；Described turning rack (21) front center position is installed with fixing axle (32), is turning
Rear inside to support (21) is respectively provided with a bearing pin (38), and described motor mounting rack (31) is arranged on turning rack (21)
Outside, turning rack (21) is fixedly mounted on motor A(20 by fixing axle (32)) motor shaft on；
In the middle of described duct (22), an electric machine support (28) is installed, is installed with 2 sets in the outside of duct (22)
Pipe (36), is installed with driven gear (25) on the sleeve pipe (36) in left side, and duct (22) is separately mounted to by 2 sleeves
On 2 bearing pins (38) of turning rack (21) inner side, described motor B(27) it is arranged on motor mounting plate, in stepping
Motor B(27) motor shaft on driving gear (26) is installed, described driving gear (26) is nibbled mutually with driven gear (25)
Closing, described brushless electric machine (23) is arranged on the center of electric machine support (28), pacifies on the motor shaft of brushless electric machine (23)
Equipped with propeller (24)；Described landing pack (17) is fixed on frame (4) top.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610691369.0A CN106274324A (en) | 2016-08-21 | 2016-08-21 | A kind of jet-propelled manned vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610691369.0A CN106274324A (en) | 2016-08-21 | 2016-08-21 | A kind of jet-propelled manned vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106274324A true CN106274324A (en) | 2017-01-04 |
Family
ID=57661376
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610691369.0A Pending CN106274324A (en) | 2016-08-21 | 2016-08-21 | A kind of jet-propelled manned vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106274324A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109703751A (en) * | 2019-02-22 | 2019-05-03 | 中船重工(武汉)凌久信息技术有限公司 | A kind of military survey mission instrument |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020003188A1 (en) * | 1998-12-16 | 2002-01-10 | Michael Moshier | Single passenger aircraft |
| US20020113165A1 (en) * | 2000-12-13 | 2002-08-22 | Michael Moshier | Aircraft and control system |
| CN102874408A (en) * | 2012-11-02 | 2013-01-16 | 冯小淋 | Double ducted-propeller electric manned aircraft capable of taking off and landing vertically |
| CN105000176A (en) * | 2015-08-10 | 2015-10-28 | 徐金鹏 | Jet aircraft |
| CN105173074A (en) * | 2015-08-16 | 2015-12-23 | 徐金鹏 | Double-duct tilt aircraft |
-
2016
- 2016-08-21 CN CN201610691369.0A patent/CN106274324A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020003188A1 (en) * | 1998-12-16 | 2002-01-10 | Michael Moshier | Single passenger aircraft |
| US20020113165A1 (en) * | 2000-12-13 | 2002-08-22 | Michael Moshier | Aircraft and control system |
| CN102874408A (en) * | 2012-11-02 | 2013-01-16 | 冯小淋 | Double ducted-propeller electric manned aircraft capable of taking off and landing vertically |
| CN105000176A (en) * | 2015-08-10 | 2015-10-28 | 徐金鹏 | Jet aircraft |
| CN105173074A (en) * | 2015-08-16 | 2015-12-23 | 徐金鹏 | Double-duct tilt aircraft |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109703751A (en) * | 2019-02-22 | 2019-05-03 | 中船重工(武汉)凌久信息技术有限公司 | A kind of military survey mission instrument |
| CN109703751B (en) * | 2019-02-22 | 2022-01-28 | 韩绍泽 | Military detection flight instrument |
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|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into 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: 20170104 |