CN105922832A - Double-rotor for providing lift for air-ground amphibious automobile - Google Patents

Double-rotor for providing lift for air-ground amphibious automobile Download PDF

Info

Publication number
CN105922832A
CN105922832A CN201610354403.5A CN201610354403A CN105922832A CN 105922832 A CN105922832 A CN 105922832A CN 201610354403 A CN201610354403 A CN 201610354403A CN 105922832 A CN105922832 A CN 105922832A
Authority
CN
China
Prior art keywords
wing
lift
main shaft
air
double
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
Application number
CN201610354403.5A
Other languages
Chinese (zh)
Inventor
温和
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201610354403.5A priority Critical patent/CN105922832A/en
Publication of CN105922832A publication Critical patent/CN105922832A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60FVEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
    • B60F5/00Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
    • B60F5/02Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Toys (AREA)

Abstract

The invention relates to a double-rotor for providing the lift for an air-ground amphibious automobile. The double-rotor is characterized in that a double-rotor body is provided with a main shaft (4) in the center, multiple rotatory shafts (5) connected to the main shaft (4) are arranged on the plane vertical to the main shaft (4), paddles (1) are arranged on the rotatory shafts (5), multiple blades (2) are uniformly arranged around the paddles (1), and the blades (2) are fixed to the paddles (1) through fixing rings (3). The double-rotor is matched with an ordinary automobile to form an air-ground amphibious automobile, the double-rotor is driven to rotate by an on-board engine of the air-ground amphibious automobile to generate the lift, to lift the manned air-ground amphibious automobile off and the manned an air-ground amphibious automobile can be made to vertically take off and land, hover, freely fly and run on the ground.

Description

Vacant lot two-purpose car provides the DCB Specimen of lift
Technical field
The invention belongs to vehicles device field, being specifically related to vacant lot two-purpose car provides the DCB Specimen of lift.
Background technology
At present, the device of moving air generation lift has: fixed-wing, rotary wings, the propeller wing, ducted fan, the rolling wing, fan The wing and flapping wing etc. are multiple, vacant lot two-purpose car compact conformation, close to general-utility car, can run, fly in the air in ground, VTOL, from By flying, the device of lift is provided must to be fulfilled for following four condition for it: one is in the confined space, i.e. projected area is close The projected area of general-utility car, terrain clearance is close to general-utility car height;Two is to produce enough lift;Three be own wt relatively Gently;Four is the required kinetic energy output close to general-utility car.Prior art provides nothing at overall volume and lift efficiency Method meets above-mentioned condition simultaneously, and aloft when hovering, VTOL state, lift efficiency is the lowest, thus it is dual-purpose to limit vacant lot The development of automobile.
Summary of the invention
It is an object of the invention to avoid the deficiencies in the prior art to provide a kind of vacant lot two-purpose car to provide the bispin of lift The wing.
For achieving the above object, the technical scheme that the present invention takes is: a kind of vacant lot two-purpose car provides the bispin of lift The wing, it is characterised in that: DCB Specimen body central is provided with main shaft (4), is provided with multiple and main shaft (4) with main shaft (4) vertical plane The rotating shaft (5) connected, rotating shaft (5) is provided with the slurry wing (1), and the slurry wing (1) is around uniformly provided with multiple fan blade (2), and fan blade (2) passes through Retainer ring (3) is fixed with the slurry wing (1).
Being provided with main shaft (4) vertical plane and starch the deflector that the wing (1) mates, deflector is by semicircle frid (6) and sets Arc (7) composition in semicircle frid (6) side, the slurry wing (1) is located at semicircle frid (6) top, between leave certain Space, it is simple to the slurry wing (1) rotates;Adjacent baffle is connected into entirety by link (8).
The described slurry wing (1) is shaped as cylinder, imitative hammer body or the Rotary-table of arbitrary shape.
Described fan blade (2) is shaped as flat board or cambered plate.
The invention has the beneficial effects as follows: structure is compact to design rationally, disturb in dynamic condition limited in limited space Moving air flow produces enough lift, and the condition meeting vacant lot two-purpose car limits.It is simple to manufacture.Mate with general-utility car and just constitute One vacant lot two-purpose car, vacant lot two-purpose car on-board engine drives DCB Specimen to rotate and produces lift, pull-up manned vacant lot Two-purpose car goes up to the air and accomplishes VTOL, hovering, free flight, ground run.
Accompanying drawing explanation
Fig. 1 is top view of the present invention;
Fig. 2 is that the present invention starches wing front view;
Fig. 3 is the embodiment of the present invention 2 top view;
Fig. 4 is the front view that the embodiment of the present invention 2 starches the wing;
In figure: 1-starches the wing, 2-fan blade, 3-retainer ring, 4-main shaft, 5-rotating shaft, 6-semicircle frid, 7-arc, and 8-connects Frame.
Detailed description of the invention
Embodiment 1, is shown in Fig. 1-2, and a kind of vacant lot two-purpose car provides the DCB Specimen of lift, it is characterised in that: DCB Specimen is originally Body center is provided with main shaft 4, is provided with multiple rotating shaft 5 being connected with main shaft 4 with main shaft 4 vertical plane, and rotating shaft 5 is provided with the slurry wing 1, Being uniformly provided with multiple fan blade 2 around the slurry wing 1, fan blade 2 is fixed with the slurry wing 1 by retainer ring 3.The slurry wing 1 is shaped as cylinder, fan blade 2 are shaped as cambered plate.
The installation direction of fan blade 2 has two kinds, when the slurry wing 1 is driven revolution and time rotational by onboard power, when fan blade 2 forwards the first half to The convex surface of fan blade 2 points to the slurry wing 1 and revolves round the sun direction.When the slurry wing 1 is driven revolution by onboard power, by air-flow time rotational, the peace of fan blade 2 Dress direction is contrary with the former.
Work process: onboard power drives the slurry wing 15 rotation around the shaft, revolves round the sun around main shaft 4 simultaneously,
The slurry wing 1 paddling air-flow produces lift pull-up vacant lot two-purpose car, and when now fan blade 2 goes to the first half, the concave surface of fan blade 2 refers to Rightabout to the slurry wing 1 revolution.When onboard power drives the slurry wing 1 to revolve round the sun, and rotation need not power, produces when relying on revolution Air-flow drives rotation, and now fan blade 2 concave surface points to the slurry wing 1 and revolves round the sun direction.
Embodiment 2, is shown in Fig. 3-4, and a kind of vacant lot two-purpose car provides the DCB Specimen of lift, it is characterised in that: in DCB Specimen body The heart is provided with main shaft 4, is provided with multiple rotating shaft 5 being connected with main shaft 4 with main shaft 4 vertical plane, and rotating shaft 5 is provided with the slurry wing 1, starches the wing Being uniformly provided with multiple fan blade 2 around 1, fan blade 2 is fixed with the slurry wing 1 by retainer ring 3;It is provided with main shaft 4 vertical plane and starches the wing The deflector of 1 coupling, deflector is made up of semicircle frid 6 and the arc 7 being located at semicircle frid 6 side, and the slurry wing 1 is located at Above semicircle frid 6, between leave a fixed gap, it is simple to the slurry wing 1 rotates;Adjacent baffle is connected into entirety by link 8. The slurry wing 1 is shaped as cylinder, and fan blade 2 is shaped as cambered plate.
Work process: onboard power drives the slurry wing 15 rotation around the shaft, revolves round the sun around main shaft 4 simultaneously, the slurry wing 1 paddling air-flow produces Raw lift pull-up vacant lot two-purpose car, when now fan blade 2 goes to the first half, the concave surface of fan blade 2 points to the phase negative side of the slurry wing 1 revolution To.When onboard power drives the slurry wing 1 to revolve round the sun, and rotation need not power, and the air-flow produced when relying on revolution drives rotation, now wind Leaf 2 concave surface points to the slurry wing 1 and revolves round the sun direction.

Claims (4)

1. the DCB Specimen of a vacant lot two-purpose car offer lift, it is characterised in that: DCB Specimen body central is provided with main shaft (4), Be provided with multiple rotating shaft (5) being connected with main shaft (4) with main shaft (4) vertical plane, rotating shaft (5) is provided with the slurry wing (1), starches the wing (1) being around uniformly provided with multiple fan blade (2), fan blade (2) is fixed with the slurry wing (1) by retainer ring (3).
2. vacant lot as claimed in claim 1 two-purpose car provides the DCB Specimen of lift, it is characterised in that: vertical with main shaft (4) Plane is provided with and starches the deflector that the wing (1) mates, and deflector is by semicircle frid (6) and is located at semicircle frid (6) side Arc (7) forms, and semicircle frid (6) top is located at by the slurry wing (1);Adjacent baffle is connected into entirety by link (8).
3. vacant lot as claimed in claim 1 two-purpose car provides the DCB Specimen of lift, it is characterised in that: the described slurry wing (1) shape Shape is cylinder, imitative hammer body or the Rotary-table of arbitrary shape.
4. vacant lot as claimed in claim 1 two-purpose car provides the DCB Specimen of lift, it is characterised in that: described fan blade (2) shape Shape is flat board or cambered plate.
CN201610354403.5A 2016-05-26 2016-05-26 Double-rotor for providing lift for air-ground amphibious automobile Pending CN105922832A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610354403.5A CN105922832A (en) 2016-05-26 2016-05-26 Double-rotor for providing lift for air-ground amphibious automobile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610354403.5A CN105922832A (en) 2016-05-26 2016-05-26 Double-rotor for providing lift for air-ground amphibious automobile

Publications (1)

Publication Number Publication Date
CN105922832A true CN105922832A (en) 2016-09-07

Family

ID=56841314

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610354403.5A Pending CN105922832A (en) 2016-05-26 2016-05-26 Double-rotor for providing lift for air-ground amphibious automobile

Country Status (1)

Country Link
CN (1) CN105922832A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113245024A (en) * 2021-05-24 2021-08-13 谢刚 Sample crushing equipment for geological sampling

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1050005A (en) * 1990-09-24 1991-03-20 韩培洲 The rolling-swing device that is used for aircraft
CN103863562A (en) * 2014-03-29 2014-06-18 郑全逸 Vertical-lifting device with combined propellers
CN104192308A (en) * 2014-09-05 2014-12-10 上海理工大学 Revolving wing flight power device capable of realizing charging and duration performance by wind power

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1050005A (en) * 1990-09-24 1991-03-20 韩培洲 The rolling-swing device that is used for aircraft
CN103863562A (en) * 2014-03-29 2014-06-18 郑全逸 Vertical-lifting device with combined propellers
CN104192308A (en) * 2014-09-05 2014-12-10 上海理工大学 Revolving wing flight power device capable of realizing charging and duration performance by wind power

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
杜帆,胡峪: "滚翼机滚转阶跃响应分析", 《飞行力学》 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113245024A (en) * 2021-05-24 2021-08-13 谢刚 Sample crushing equipment for geological sampling

Similar Documents

Publication Publication Date Title
CN103847960B (en) A kind of composite rotating drives vertically taking off and landing flyer
CN103072690A (en) Single-ducted coaxial rotor/propeller saucer-shaped aircraft
CN104590555A (en) Electrodynamic multi-rotor helicopter
CN103935517A (en) Aircraft
CN109665096A (en) A kind of shrouded propeller thrust coaxial double-rotor helicopter
CN206446792U (en) Aircraft
CN204399476U (en) A kind of micro flapping wing air vehicle
CN206871360U (en) A kind of multiple degrees of freedom flapping-wing modal with high propulsive efficiency
CN104443384A (en) Rotary wing blade type flapping wing air vehicle
CN101284570A (en) Centrifugal fan type lift/propulsion device and aerocraft with the device
CN208915439U (en) Adjustable wing swallow shape simulation type unmanned plane
CN207956057U (en) A kind of active main rotor vertically taking off and landing flyer
CN105922832A (en) Double-rotor for providing lift for air-ground amphibious automobile
CN112441229A (en) Flapping rotor wing device with upward shaft wing capable of vertically running and downward horizontally running
CN103991543B (en) A kind of rotary flapping wing aircraft with spring
CN203864998U (en) Small-sized rotating flapping wing unmanned aerial vehicle
CN204507273U (en) A kind of agricultural unmanned vehicle spraying atomizing
CN104787324A (en) Lift force generator
CN103991541A (en) Small rotary ornithopter with springs
CN210852912U (en) Blade opening and closing mechanism based on rotary flapping wing vertical take-off and landing power device
CN203845008U (en) Unmanned ornithopter
CN203845010U (en) Small ornithopter
CN112407276A (en) Flapping rotor wing device capable of realizing upward half-rotation and downward horizontal operation
CN203845009U (en) Rotary ornithopter
CN101177168A (en) Rotor device with imitating flapping wings effect of windscreen

Legal Events

Date Code Title Description
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: 20160907