CN109107179A - A kind of aviation aircraft smooth flight system - Google Patents
A kind of aviation aircraft smooth flight system Download PDFInfo
- Publication number
- CN109107179A CN109107179A CN201710490065.2A CN201710490065A CN109107179A CN 109107179 A CN109107179 A CN 109107179A CN 201710490065 A CN201710490065 A CN 201710490065A CN 109107179 A CN109107179 A CN 109107179A
- Authority
- CN
- China
- Prior art keywords
- blade
- order
- aviation aircraft
- uphold justice
- fixed device
- 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
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Classifications
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- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
- A63H27/12—Helicopters ; Flying tops
Landscapes
- Toys (AREA)
Abstract
The invention discloses a kind of aviation aircraft smooth flight systems, and including aviation aircraft driving shaft, the rotating device being fixedly connected with the driving shaft, the rotating device includes to be weighed and consider in order to uphold justice blade by a secondary primary blades and a pair for the fixed device connection of blade；Aviation aircraft smooth flight system provided by the invention, integral body can weigh and consider in order to uphold justice automatically during steering, thus the sporting flying of aviation aircraft can be made more steady smooth, will not disintegrate because of the out of control of centrifugal force.
Description
Technical field
The present invention relates to a kind of aeromodelling airplanes, more particularly, to a kind of aeromodelling airplane that can be weighed and consider in order to uphold justice automatically during exercise.
Background technique
Weighing and considering in order to uphold justice property all armrest dynamic Controls of general aeromodelling airplane, therefore operationally have higher requirements, for beginner
For, from strange to skillfully in the presence of very big difficulty.Meanwhile aeromodelling airplane is all to bring rising by the high speed rotation of propeller
Power, this powerful centrifugal force bring acid test to the go to action of aeromodelling airplane again, aeromodelling airplane may also because of
It is fallen out due to powerful centrifugal force effect loses and weighs and consider in order to uphold justice when steering, the safety of its manipulator and body itself is made to be on the hazard.Cause
This just endless pursuit at Liao Ge model plane manufacturer and airplane hobbyist of weighing and considering in order to uphold justice automatically.
Therefore, it is necessary to invent a kind of aeromodelling airplane that can be weighed and consider in order to uphold justice automatically during exercise to solve the above problems.
Summary of the invention
The present invention in view of the deficiency of the prior art, provides a kind of aviation aircraft smooth flight of structure novel
System enables aeromodelling airplane to automatically keep weighing and considering in order to uphold justice for fuselage in flight, and performance is safer.
The present invention in order to achieve the above technical purposes, using following technological means:
A kind of aviation aircraft smooth flight system, what is be fixedly connected including aviation aircraft driving shaft, with the driving shaft turns
Dynamic device, the rotating device include to be weighed and consider in order to uphold justice blade by a secondary primary blades and a pair for the fixed device connection of blade.
Automatically the head rest device of weighing and considering in order to uphold justice further includes the rotating block for connecting the driving shaft Yu the rotating device；Institute
Stating the fixed device middle part of blade, side is provided with a slot downward, is connected to after the rotating block left and right ends socket bearing described
In the middle part of the fixed device of blade in slot.
The rotating block top middle portion is provided with strip groove, and tail end is provided with for passing through cylinder with the driving shaft
The horizontal direction through-hole of pin connection.
Weigh and consider in order to uphold justice blade, the fixed device of blade that is set as of the one secondary primary blades, a pair is arranged in same level
Face, the downside for being set as being installed vertically on the fixed device of the blade after rotating block is connect with the driving shaft head and the tail.
It is logical that the fixed device both ends of the blade are respectively provided with a vertical direction for being bolted with the primary blades
Hole.
The rotating device further includes having the stick of weighing and considering in order to uphold justice connecting with the fixed device of the blade；The blade of weighing and considering in order to uphold justice is set to
Two tops of the stick of weighing and considering in order to uphold justice；A level side for connecting with the stick of weighing and considering in order to uphold justice is additionally provided in the middle part of the fixed device of the blade
To through-hole.
The rotating device further includes being sleeved on to be set as the at an acute angle with horizontal plane of " ten " font on the driving shaft " ten "
Shaped frame.
The rotating device further includes that at least pairs of the stick left and right ends of weighing and considering in order to uphold justice is arranged in weigh and consider in order to uphold justice baseball shape housing,
One end be sleeved on it is described weigh and consider in order to uphold justice on stick, the other end with it is described at an acute angle with horizontal plane " ten " shaped frames are connected.
The rotating device further includes described at an acute angle with horizontal plane for connecting " ten " shaped frames and the stick of weighing and considering in order to uphold justice
The deflecting bar of spherical housing, one end are connect with the baseball shape housing of weighing and considering in order to uphold justice, and the other end and described and horizontal plane are at an acute angle "
The connection of ten " shaped frames.
Aviation aircraft smooth flight system provided by the invention, due to being provided with the fixed device of blade, rotating block, running through
The stick of weighing and considering in order to uphold justice and horizontal plane of the fixed device of the blade and rotating block are at an acute angle " ten " shaped frames, deflecting bar, baseball shape of weighing and considering in order to uphold justice
Housing, integral body can weigh and consider in order to uphold justice automatically during steering, thus the sporting flying of aeromodelling airplane can be made more steady smooth,
Will not disintegrate because of the out of control of centrifugal force, it is ensured that aviation aircraft itself and manipulator using safe.
Detailed description of the invention
Fig. 1 is a kind of decomposition diagram of aviation aircraft smooth flight system one embodiment of the present invention；
Fig. 2 is a kind of assembling schematic diagram of aviation aircraft smooth flight system one embodiment of the present invention；
Fig. 3 is a kind of blade fixture structure schematic diagram of aviation aircraft smooth flight system one embodiment of the present invention.
Specific embodiment
With reference to Fig. 1, a kind of partition signal of embodiment of the invention is illustrated；With reference to Fig. 2, one embodiment is illustrated
Assembling schematic diagram；With reference to Fig. 3, the bottom view of the fixed device of blade of one embodiment is illustrated；In the present embodiment, weigh and consider in order to uphold justice automatically
Head rest device includes aviation aircraft driving shaft 1, rotating block 11, rotating block bearing 111, rotating block strip groove 112, straight pin
113, the secondary primary blades 20 of fixed hole 114, rotating device 2, one, primary blades bolt 201, primary blades nut 202, a pair are weighed and consider in order to uphold justice leaf
Piece 21, blade bolt 211 of weighing and considering in order to uphold justice, blade nut of weighing and considering in order to uphold justice 212, stick 22 of weighing and considering in order to uphold justice, mandrel of weighing and considering in order to uphold justice hold 221, blade fixed device 23, leaf
Piece fixes device slot 231, vertical through hole 232, horizontal through hole 233, counterweight set 24, hexagon socket head cap screw 241 and horizontal plane Cheng Rui
Angle " ten " shaped frames 25, baseball shape housing 26 of weighing and considering in order to uphold justice, spherical housing bolt 261, deflecting bar 27, club 271, connecting rod lantern ring
272。
In this aviation aircraft smooth flight system, rotating block 11 and the driving shaft 1 are arranged by 11 tail end of rotating block
Fixed hole 114 assign into after straight pin 113, head and the tail connect, then are installed vertically on the downside of the fixed device 23 of the blade
Face；Such as Fig. 3, the middle part downside of the fixed device 23 of blade is provided with the fixed device slot 231 of blade, 11 left and right ends of rotating block set
It connects after switching through motion block bearing 111 into the fixed device slot 231 of blade；11 top middle portion of rotating block offers rotating block strip
Groove 112, and fixed 23 middle part of device of blade fixes the perpendicular direction of device slot 231 with blade and has also opened up horizontal through hole
233, after rotating block 11 is connected into the fixed device slot 231 of blade, rotating block strip groove 112 and horizontal through hole 233 are same
To overlapping, to stick 22 of weighing and considering in order to uphold justice also cross rotating block 11 and the fixed device 23 of blade；Fixed 23 both ends of device of blade are respectively provided with
One vertical through hole 232 for passing through with the primary blades 20, primary blades 20 pass through primary blades bolt 201, primary blades nut 202
It is fixedly mounted on fixed 23 both ends of device of blade；Stick 22 of weighing and considering in order to uphold justice passes through the horizontal through hole 233 of the fixed device 23 of blade, and two sides are to weigh
Flat mandrel is held 221 sticks 22 that will weigh and consider in order to uphold justice and is fixed on the fixed device 23 of blade；One secondary weighing apparatus is symmetrically installed on 22 both sides of stick of weighing and considering in order to uphold justice
Flat blade 21 is fixedly mounted on 22 liang of tops of stick of weighing and considering in order to uphold justice by blade bolt 211 of weighing and considering in order to uphold justice, blade nut of weighing and considering in order to uphold justice 212；Weigh and consider in order to uphold justice stick 22
Both sides are also symmetrically equipped with a secondary counterweight set 24, and 22 two sides of stick of weighing and considering in order to uphold justice are fixedly mounted on by hexagon socket head cap screw 241；Weigh and consider in order to uphold justice stick
22 both sides close to the fixed device 23 of blade positional symmetry a pair be installed weigh and consider in order to uphold justice baseball shape housing 26, baseball shape housing of weighing and considering in order to uphold justice
26 one end are sleeved on stick 22 of weighing and considering in order to uphold justice, fixed by spherical housing bolt 261, and the other end is provided with snap ring, is connected with deflecting bar 27,
Deflecting bar 27 includes the club 271 being mutually threadedly coupled, connecting rod lantern ring 272, can pass through the rotation of adjusting screw thread therebetween
Transfer change connection state；27 one end of deflecting bar is connect by club 271 with baseball shape housing 26 of weighing and considering in order to uphold justice, and the other end passes through connecting rod
Lantern ring 272 with it is at an acute angle with horizontal plane " ten " shaped frames 25 connect, at an acute angle with horizontal plane " ten " shaped frames 25 are set as
Crosswise is both provided with spherical attachment on each angle at four angles, is cooperatively connected with connecting rod lantern ring 272.
The notch 112 at 22 penetrating blade of stick of weighing and considering in order to uphold justice fixed device 23 middle part and 11 top of rotating block, while being also segmented
Fixed, counterweight set 24, the fixed blade 21 of weighing and considering in order to uphold justice in 26 both ends of baseball shape housing of weighing and considering in order to uphold justice reach the purpose for body of weighing and considering in order to uphold justice.It is described
26 one end of baseball shape housing of weighing and considering in order to uphold justice is fixed on and weighs and consider in order to uphold justice on stick 22, and the other end is connected to the inclination of aeromodelling airplane with connecting rod lantern ring 272
On disk 25, make the steering of its body is synchronous with head frame assembly to carry out.And the fixation of the primary blades 20 of head frame assembly, blade 21 of weighing and considering in order to uphold justice
Central point all on the fixed device 23 of blade, makes the steering of aeromodelling airplane achieve the purpose that weigh and consider in order to uphold justice automatically.
Aviation aircraft smooth flight system provided by the invention, due to being provided with the fixed device of blade, rotating block, running through
The stick of weighing and considering in order to uphold justice and horizontal plane of the fixed device of the blade and rotating block are at an acute angle " ten " shaped frames, deflecting bar, baseball shape of weighing and considering in order to uphold justice
Housing, integral body can weigh and consider in order to uphold justice automatically during steering, thus the sporting flying of aeromodelling airplane can be made more steady smooth,
Will not disintegrate because of the out of control of centrifugal force, it is ensured that aviation aircraft itself and manipulator using safe.
The above disclosure is only a preferred embodiment of the invention, cannot limit the right of the present invention with this certainly
Range, therefore according to equivalent variations made by scope of the present invention patent, it is still within the scope of the present invention.
Claims (6)
1. a kind of aviation aircraft smooth flight system, it is characterised in that: fly including aviation aircraft driving shaft, with the aviation
The rotating device that row device driving shaft is fixedly connected, the rotating device include the secondary primary blades by the fixed device connection of blade
Weigh and consider in order to uphold justice blade with a pair.
2. aviation aircraft smooth flight system according to claim 1, it is characterised in that: the aviation aircraft is steady
Flight system further includes the rotating block for connecting the driving shaft Yu the rotating device；Court in the middle part of the fixed device of the blade
Lower side is provided with a slot, and slot in the middle part of the fixed device of the blade is connected to after institute's rotating block left and right ends socket bearing
In.
3. aviation aircraft smooth flight system according to claim 2, it is characterised in that: the rotating block top middle portion
It is provided with strip groove, tail end is provided with the horizontal direction through-hole for passing through cylinder pin connection with the driving shaft.
4. aviation aircraft smooth flight system according to claim 2, it is characterised in that: described one secondary primary blades, institute
It states a pair and weighs and consider in order to uphold justice the fixed device setting of blade, the blade in same level, the rotating block connects with the driving shaft head and the tail
The downside of the fixed device of the blade is installed vertically on after connecing.
5. aviation aircraft smooth flight system according to claim 1, it is characterised in that: the fixed device two of the blade
End is respectively provided with the vertical direction through-hole for being bolted with the primary blades.
6. aviation aircraft smooth flight system according to claim 1, it is characterised in that: the rotating device further includes
There is the stick of weighing and considering in order to uphold justice connecting with the fixed device of the blade；The blade of weighing and considering in order to uphold justice is set to two tops of the stick of weighing and considering in order to uphold justice；The leaf
The horizontal direction through-hole for connecting with the stick of weighing and considering in order to uphold justice is additionally provided in the middle part of the fixed device of piece.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710490065.2A CN109107179A (en) | 2017-06-25 | 2017-06-25 | A kind of aviation aircraft smooth flight system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710490065.2A CN109107179A (en) | 2017-06-25 | 2017-06-25 | A kind of aviation aircraft smooth flight system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109107179A true CN109107179A (en) | 2019-01-01 |
Family
ID=64733544
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710490065.2A Pending CN109107179A (en) | 2017-06-25 | 2017-06-25 | A kind of aviation aircraft smooth flight system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109107179A (en) |
-
2017
- 2017-06-25 CN CN201710490065.2A patent/CN109107179A/en active Pending
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20190101 |
|
| WD01 | Invention patent application deemed withdrawn after publication |