CN107662712A - Take off disk - Google Patents
Take off disk Download PDFInfo
- Publication number
- CN107662712A CN107662712A CN201610673350.3A CN201610673350A CN107662712A CN 107662712 A CN107662712 A CN 107662712A CN 201610673350 A CN201610673350 A CN 201610673350A CN 107662712 A CN107662712 A CN 107662712A
- Authority
- CN
- China
- Prior art keywords
- rotating disk
- aircraft
- scale
- bevel gear
- scale rotating
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/04—Launching or towing gear
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Retarders (AREA)
Abstract
The present invention relates to aircraft circles, more particularly to take off disk.Process a large-scale rotating disk that can put down 2 to 4 airplanes, disk peripheral is higher than the middle part of rotating disk, a large-scale bevel gear is processed below rotating disk, as dynamic bevel gear, driving wheel uses 3 or 4 bevel gears, being evenly distributed to be engaged with dynamic bevel gear tooth, dynamic bevel gear drives large-scale rotating disk to rotate.Airplane tail group on large-scale rotating disk all utilizes pulling buckle aircraft pulling buckle on large-scale rotating disk, aircraft is when taking off, the power set of 3 or 4 drive bevel gears start simultaneously, aircraft also starts power set simultaneously, large-scale rotary speed is being accelerated, the power set of aircraft are also accelerating, make a concerted effort caused by gravitation caused by the centrifugal force and aircraft of large-scale rotating disk, the condition that aircraft can take off is reached, aircraft on large-scale rotating disk simultaneously unclamps pulling buckle, to being thrown off when aircraft is dished out by large-scale rotating disk, aircraft is flown in the air.
Description
Technical field：The present invention relates to aircraft circles, are directed to rotating disk, more particularly to take off disk.
Background technology：Take off and always taken off using runway, this mode of taking off is, it is necessary to which very long rising is run fast
Road, be not suitable for aircraft and taken off on aircraft carrier, be also not suitable for taking off on submarine.
The content of the invention：By the use of rotating disk as runway is taken off, drawn using the operating on centrifugal force of rotating disk with what is taken off
Power, generation are made a concerted effort, and aircraft is thrown in the air, while 2 to 4 airplanes that can take off.
Brief description of the drawings：
Fig. 1, it is placement schematic diagram of 3 airplanes on large-scale rotating disk.
Fig. 2, it is to take off disk schematic diagram.
Fig. 3, it is Bevel Gear Transmission schematic diagram.
1 in figure is large-scale rotating disk.2 be dynamic bevel gear.3 be drive bevel gear.4 be power set.5 be axle.6 be axle
Hold.7 be pulling buckle.8 be aircraft.
Embodiment：A large-scale rotating disk 1 that can put down 2 to 4 airplanes is processed, disk peripheral is higher than in rotating disk
Portion, a large-scale bevel gear is processed below rotating disk, as dynamic bevel gear 2, driving wheel uses 3 or 4 bevel gears, point
Cloth is uniformly engaged with the tooth of dynamic bevel gear, and transmission is combined with dynamic bevel gear.The power set of 3 or 4 drive bevel gears 3
4 starting times, the rotating speed of output was identical simultaneously, the center below large-scale rotating disk, was positioned using axle 5, and axle uses with large-scale rotating disk
Bearing 6 is connected, and dynamic bevel gear is arranged on below large-scale rotating disk, and dynamic bevel gear 2 engages with 3 or 4 drive bevel gears 3,
Engaged with the tooth of drive bevel gear, when drive bevel gear rotates, drive dynamic bevel gear to rotate, dynamic bevel gear drives large-scale turn
Disk rotates.When large-scale rotating disk reaches certain rotating speed, centrifugal force caused by large-scale rotating disk, the object on large-scale rotating disk can be made to dish out
Rotating disk.Aircraft is placed, at large-scale turn when being 3 airplane when being 2 airplane in standby for takeoff on large-scale rotating disk into 180 degree
Into 60 degree of placements on disk, into 45 degree of placements on large-scale rotating disk when being 4 airplane.The afterbody of aircraft 8 on large-scale rotating disk all utilizes
Aircraft pulling buckle on large-scale rotating disk, is prevented that aircraft is spilled over rotating disk to aircraft when being not reaching to the strength of flight by pulling buckle 7.Fly
When taking off, the power set of 3 or 4 drive bevel gears start machine simultaneously, and aircraft 8 also starts power set simultaneously, large-scale turn
Disk rotating speed is being accelerated, and the centrifugal force of large-scale rotating disk is increasing, and the power set of aircraft are also accelerating, and caused gravitation is also adding
Greatly, make a concerted effort caused by gravitation caused by the centrifugal force and aircraft of large-scale rotating disk, reached the condition that aircraft can take off, large-scale rotating disk
On aircraft pulling buckle is unclamped simultaneously, aircraft is dished out by large-scale rotating disk, and because the periphery of rotating disk is higher than the middle part of rotating disk, aircraft is big
To being thrown off when type rotating disk is dished out, along with lifting force caused by the wing of aircraft, making a concerted effort for aircraft flight is to produced,
Aircraft is flown in the air.
Beneficial effect：Take off and do not need runway, can reduce and take off the time, can take off 2 to 4 airplanes simultaneously,
It is adapted to take off on aircraft carrier, is also not suitable for taking off on submarine.
Claims (1)
1. the method taken off disk and taken off：Including rotating disk, transmission device, it is characterised in that：Processing one can put down 2 to 4
The large-scale rotating disk (1) of airplane, disk peripheral are higher than the middle part of rotating disk, and a large-scale bevel gear is processed below rotating disk,
As dynamic bevel gear (2), driving wheel uses 3 or 4 bevel gears, being evenly distributed to be engaged with dynamic bevel gear tooth, with quilt
Dynamic bevel gear combination transmission, power set (4) starting time of 3 or 4 drive bevel gears (3), the rotating speed of output was identical simultaneously,
Center below large-scale rotating disk, positioned using axle (5), axle is connected with large-scale rotating disk using bearing (6), and dynamic bevel gear is arranged on
Below large-scale rotating disk, dynamic bevel gear (2) engages with 3 or 4 drive bevel gears (3), is engaged with the tooth of drive bevel gear, main
When dynamic bevel gear rotates, dynamic bevel gear is driven to rotate, dynamic bevel gear drives large-scale rotating disk to rotate, and large-scale rotating disk reaches certain
Rotating speed when, centrifugal force caused by large-scale rotating disk, the object on large-scale rotating disk can be made to dish out rotating disk, aircraft in standby for takeoff,
Placed when being 2 airplane on large-scale rotating disk into 180 degree, be that 4 framves fly into 60 degree of placements on large-scale rotating disk when being 3 airplane
Placed during machine on large-scale rotating disk into 45 degree, aircraft (8) afterbody on large-scale rotating disk is all using pulling buckle (7) aircraft pulling buckle big
On type rotating disk, prevent that aircraft is spilled over rotating disk to aircraft when being not reaching to the strength of flight, aircraft is when taking off, 3 or 4 masters
The power set of dynamic bevel gear start simultaneously, and aircraft (8) also starts power set simultaneously, and large-scale rotary speed is being accelerated, large-scale
The centrifugal force of rotating disk is increasing, and the power set of aircraft are also accelerating, and caused gravitation is also increasing, the centrifugal force of large-scale rotating disk
With aircraft caused by make a concerted effort caused by gravitation, reached the condition that aircraft can take off, the aircraft on large-scale rotating disk is simultaneously pulling buckle
Unclamp, aircraft is dished out by large-scale rotating disk, and because the periphery of rotating disk is higher than the middle part of rotating disk, aircraft is upward when being dished out by large-scale rotating disk
Dish out, along with lifting force caused by the wing of aircraft, to produce making a concerted effort for aircraft flight, aircraft is flown in the air.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610673350.3A CN107662712A (en) | 2016-07-31 | 2016-07-31 | Take off disk |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610673350.3A CN107662712A (en) | 2016-07-31 | 2016-07-31 | Take off disk |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107662712A true CN107662712A (en) | 2018-02-06 |
Family
ID=61122509
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610673350.3A Pending CN107662712A (en) | 2016-07-31 | 2016-07-31 | Take off disk |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107662712A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112224433A (en) * | 2020-09-28 | 2021-01-15 | 北京二郎神科技有限公司 | Unmanned aerial vehicle helps and flies device and unmanned aerial vehicle system |
-
2016
- 2016-07-31 CN CN201610673350.3A patent/CN107662712A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112224433A (en) * | 2020-09-28 | 2021-01-15 | 北京二郎神科技有限公司 | Unmanned aerial vehicle helps and flies device and unmanned aerial vehicle system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180206 |