CN107487448A - Lead to aircraft in disc - Google Patents
Lead to aircraft in disc Download PDFInfo
- Publication number
- CN107487448A CN107487448A CN201610461204.4A CN201610461204A CN107487448A CN 107487448 A CN107487448 A CN 107487448A CN 201610461204 A CN201610461204 A CN 201610461204A CN 107487448 A CN107487448 A CN 107487448A
- Authority
- CN
- China
- Prior art keywords
- disc
- lead
- aircraft
- engine
- thrust engine
- 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
- 230000000149 penetrating effect Effects 0.000 claims description 2
- 238000009434 installation Methods 0.000 claims 3
- 230000033001 locomotion Effects 0.000 abstract description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008450 motivation 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; 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
-
- 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
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0045—Fuselages characterised by special shapes
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
One kind can be vertically moved up or down, also can the horizontal sliding disc-shaped flying device for running landing.It is made up of passage, vertical thrust engine, horizontal thrust engine, trishores undercarriage in disc shell, setting etc..Horizontal thrust engine can be enabled when taking off or landing slide and run landing, lead in can also enabling and erect vertical thrust engine Vertical Dynamic lifting is provided, 360 degree of rotations can be carried out during flight in the air, u-turn, rotation stop, be vertically moved up or down etc., and various motion is integrated.
Description
Technical field：
Also horizontal slide can be vertically moved up or down the present invention relates to one kind and runs landing aircraft, in specifically a kind of collar plate shape
It is logical to be vertically moved up or down also horizontal sliding race landing aircraft.
Background technology：
At present, known helicopter is to provide lifting power by the big vane rotation of back, and the small vane of its fuselage is big,
Fuselage interior space is small, and take-off weight is small, and fly is influenceed by weather and steric requirements, and the rate of climb is slow, and lifting height is limited.
The content of the invention：
In order to overcome the big vane fuselage of existing helicopter small, fuselage interior space is small, and take-off weight is small, fly by
Weather and steric requirements influence, and the rate of climb is slow, the limited phenomenon of lifting height, and the present invention provides Tong Kechui in a kind of collar plate shape
Going straight up to drop also can horizontal sliding race landing aircraft.
The present invention solves the technical scheme that its technical problem uses：By passage, normal thrust in disc shell, setting
Engine, horizontal thrust engine, trishores undercarriage etc. form.Horizontal thrust engine can be enabled when taking off or landing
It is sliding to run landing, lead in can also enabling and vertical thrust engine offer Vertical Dynamic lifting is provided.360 can be carried out during flight in the air
The various motions such as degree rotates, reversed end for end, rotation stops, is vertically moved up or down are integrated.
The beneficial effects of the invention are as follows：Race landing can be slided also to be vertically moved up or down, 360 degree of rotations can be carried out during flight in the air
Turn, u-turn, rotation the various motion such as stop, be vertically moved up or downs and being integrated, the increase of its inner space, take-off weight increase, flying height increasing
High, flying speed is speeded.
Brief description of the drawings：
The present invention is further described with reference to the accompanying drawings and examples.
Fig. 1：Plan.
Fig. 2：Profile.
In figure：1st, shell on collar plate shape, 2, collar plate shape lower casing, 3, collar plate shape drain pan, 4, air inlet, 5, gas outlet, 6,
Erect engine, 7, horizontal engine, 8, trishores undercarriage, 9, vertical air guide vane can be transferred.
Embodiment：
It is that circle penetrating up and down is empty (4) in Fig. 1, among circular housing (1), normal thrust hair is installed in circular cavity
Motivation (6) provides vertical lift power, its aircraft is vertically moved up or down or is suspended in the air.
In Fig. 1, circular housing (1) both sides respectively install a horizontal thrust engine (7) and provide horizontal thrust, make its flight
Device can horizontally advance or fly.
In Fig. 2, vertical air guide vane (9) can be transferred, vertical air is can adjust when vertical engine starts and is oriented to
Blade angle, its aircraft is set to rotate, reverse end for end in the air.
Claims (5)
1. lead to aircraft in a kind of disc, by shell, collar plate shape lower casing, collar plate shape drain pan, air inlet, outlet on collar plate shape
Mouthful, erect engine, horizontal engine, trishores undercarriage, can transfer vertical air guide vane composition, it is characterized in that：
Disc shell.
2. lead to aircraft in disc according to claim 1, it is characterized in that：Penetrating circle above and below among disc shell
Empty passage.
3. lead to aircraft in disc according to claim 1, it is characterized in that：Installation vertically pushes away among circular empty passage
Force engine.
4. lead to aircraft in disc according to claim 1, it is characterized in that：Each installation one in disc shell both sides
Horizontal thrust engine.
5. lead to aircraft in disc according to claim 1, it is characterized in that：Vertical thrust engine air inlet installation is adjustable
Dynamic air guide vane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610461204.4A CN107487448A (en) | 2016-06-12 | 2016-06-12 | Lead to aircraft in disc |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610461204.4A CN107487448A (en) | 2016-06-12 | 2016-06-12 | Lead to aircraft in disc |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107487448A true CN107487448A (en) | 2017-12-19 |
Family
ID=60642088
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610461204.4A Pending CN107487448A (en) | 2016-06-12 | 2016-06-12 | Lead to aircraft in disc |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107487448A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN86105611A (en) * | 1986-07-23 | 1988-03-30 | 海斯塔航天发展公司 | Aircraft |
| CN1080253A (en) * | 1992-01-29 | 1994-01-05 | 飞盘操作有限公司 | Flight instruments |
| CN1121021A (en) * | 1994-10-15 | 1996-04-24 | 吴德滨 | Two-purpose flying vehicle |
| CN202295287U (en) * | 2011-09-06 | 2012-07-04 | 雷佳振 | Disc-shaped aircraft |
| CN105366053A (en) * | 2015-11-19 | 2016-03-02 | 唐若权 | Disk shaped vehicle |
-
2016
- 2016-06-12 CN CN201610461204.4A patent/CN107487448A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN86105611A (en) * | 1986-07-23 | 1988-03-30 | 海斯塔航天发展公司 | Aircraft |
| CN1080253A (en) * | 1992-01-29 | 1994-01-05 | 飞盘操作有限公司 | Flight instruments |
| CN1121021A (en) * | 1994-10-15 | 1996-04-24 | 吴德滨 | Two-purpose flying vehicle |
| CN202295287U (en) * | 2011-09-06 | 2012-07-04 | 雷佳振 | Disc-shaped aircraft |
| CN105366053A (en) * | 2015-11-19 | 2016-03-02 | 唐若权 | Disk shaped vehicle |
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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 |
Application publication date: 20171219 |
|
| WD01 | Invention patent application deemed withdrawn after publication |