CN105771268A - Steady flight system for aircraft - Google Patents
Steady flight system for aircraft Download PDFInfo
- Publication number
- CN105771268A CN105771268A CN201410834822.XA CN201410834822A CN105771268A CN 105771268 A CN105771268 A CN 105771268A CN 201410834822 A CN201410834822 A CN 201410834822A CN 105771268 A CN105771268 A CN 105771268A
- Authority
- CN
- China
- Prior art keywords
- order
- blade
- uphold justice
- flight system
- aviation aircraft
- 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
Landscapes
- Toys (AREA)
Abstract
The invention discloses a steady flight system for an aircraft. The steady flight system comprises an aircraft driving shaft, and a rotating apparatus fixedly connected with the driving shaft, wherein the rotating apparatus comprises a pair of main blades and a pair of balance blades connected through a blade fixing apparatus. According to the steady flight system for the aircraft provided by the invention, the overall aircraft body can be automatically balanced in the steering process, so that the aircraft can be more steady and smooth in the flight process without being disassembled due to the fact that centrifugal force is out of control.
Description
Technical field
The present invention relates to a kind of aeromodelling airplane, especially relate to a kind of aeromodelling airplane that can automatically weigh and consider in order to uphold justice at the volley.
Background technology
The weighing and considering in order to uphold justice property of general aeromodelling airplane all armrest dynamic Control, therefore operationally have higher requirements, and for abecedarian, there is very big difficulty from strange to skilled.Simultaneously, the high speed rotating that aeromodelling airplane is all by propeller brings climbing power, the go to action of aeromodelling airplane is brought again acid test by this powerful centrifugal force, aeromodelling airplane is likely to because weigh and consider in order to uphold justice when turning to because powerful centrifugal action loses and fall out so that it is the safety of manipulator and body itself is on the hazard.Therefore automatically weigh and consider in order to uphold justice the endless pursuit with regard to Cheng Liaoge model plane manufacturer with airplane hobbyist.
Accordingly, it would be desirable to invent a kind of aeromodelling airplane that can automatically weigh and consider in order to uphold justice at the volley to solve the problems referred to above.
Summary of the invention
The present invention is directed to the deficiency that above-mentioned prior art exists, it is provided that the aviation aircraft smooth flight system of a kind of novel structure, make aeromodelling airplane can automatically keep weighing and considering in order to uphold justice of fuselage when flight, performance is safer.
The present invention, in order to realize above-mentioned technical purpose, adopts following technological means:
A kind of aviation aircraft smooth flight system, fixes, including aviation aircraft driving shaft, the tumbler being connected with described driving shaft, described tumbler includes the secondary primary blades connected by the fixing device of blade and a pair is weighed and consider in order to uphold justice blade.
Described head rest device of automatically weighing and considering in order to uphold justice also includes the moving block for connecting described driving shaft and described tumbler；In the middle part of the fixing device of described blade, side is provided with a slot down, is connected in the middle part of the fixing device of described blade in slot after two ends, described moving block left and right socket bearing.
Described moving block top middle portion is provided with strip groove, and its tail end is provided with the horizontal direction through hole for being connected by straight pin with described driving shaft.
A described secondary primary blades, a described pair weigh and consider in order to uphold justice blade, described in be set to the fixing device of blade and be arranged on same level, described in be set to be installed vertically on described blade after moving block is connected with described driving shaft head and the tail and fix the downside of device.
The fixing device of described blade is respectively arranged at the two ends with a vertical direction through hole for being bolted with described primary blades.
Described tumbler also includes the rod of weighing and considering in order to uphold justice being connected with the fixing device of described blade；Described blade of weighing and considering in order to uphold justice be arranged at described in weigh and consider in order to uphold justice rod two tops；A horizontal direction through hole for being connected it is additionally provided with described rod of weighing and considering in order to uphold justice in the middle part of the fixing device of described blade.
What described tumbler also included being sleeved on described driving shaft and be set to " ten " font acutangulates with horizontal plane " ten " shaped frame.
Described tumbler also include being arranged on described in weigh and consider in order to uphold justice at least one pair at rod two ends, left and right weigh and consider in order to uphold justice baseball shape overcoat, its one end be sleeved on described in weigh and consider in order to uphold justice on rod, the other end acutangulates with horizontal plane with described " ten " shaped frame is connected.
Described tumbler also includes described acutangulating with horizontal plane for connecting " ten " the break-in bar of shaped frame and described baseball shape overcoat of weighing and considering in order to uphold justice, its one end is connected with described baseball shape overcoat of weighing and considering in order to uphold justice, and the other end acutangulates with horizontal plane with described " ten " shaped frame is connected.
Aviation aircraft smooth flight system provided by the invention, due to be provided with the fixing device of blade, moving block, run through the fixing device of described blade and moving block weigh and consider in order to uphold justice rod and what horizontal plane acutangulated " ten " shaped frame, break-in bar, baseball shape overcoat of weighing and considering in order to uphold justice, integral body automatically can be weighed and consider in order to uphold justice in the process turned to, thus the sporting flying more steadily smoothness of aeromodelling airplane can be made, will not disintegrate because of the out of control of centrifugal force, it is ensured that the use safety of aviation aircraft itself and manipulator.
Accompanying drawing explanation
Fig. 1 is the decomposing schematic representation of a kind of aviation aircraft one embodiment of smooth flight system of the present invention；
Fig. 2 is the assembling schematic diagram of a kind of aviation aircraft one embodiment of smooth flight system of the present invention；
Fig. 3 is the blade fixture structure schematic diagram of a kind of aviation aircraft one embodiment of smooth flight system of the present invention.
Detailed description of the invention
With reference to Fig. 1, it is illustrated that the partition signal of a kind of embodiment of the present invention；With reference to Fig. 2, it is illustrated that the assembling schematic diagram of an embodiment；With reference to Fig. 3, it is illustrated that the upward view of the fixing device of the blade of an embodiment；In the present embodiment, automatically head rest device of weighing and considering in order to uphold justice includes aviation aircraft driving shaft 1, moving block 11, moving block bearing 111, moving block strip groove 112, straight pin 113, fixed via 114, tumbler 2, one secondary primary blades 20, primary blades bolt 201, primary blades nut 202, one pair is weighed and consider in order to uphold justice blade 21, weigh and consider in order to uphold justice blade bolt 211, weigh and consider in order to uphold justice blade nut 212, weigh and consider in order to uphold justice excellent 22, weigh and consider in order to uphold justice rod bearing 221, blade fixes device 23, blade fixes device slot 231, vertical through hole 232, horizontal through hole 233, counterweight set 24, hexagon socket head cap screw 241, acutangulate with horizontal plane " ten " shaped frame 25, weigh and consider in order to uphold justice baseball shape overcoat 26, spherical overcoat bolt 261, break-in bar 27, club 271, the connecting rod collar 272.
In this aviation aircraft smooth flight system, the fixed via 114 that moving block 11 is arranged by moving block 11 tail end with described driving shaft 1 is assigned after straight pin 113, and head and the tail connect, then is installed vertically on the downside of the fixing device 23 of described blade；Such as Fig. 3, blade is fixed and is provided with the fixing device slot 231 of blade on the downside of the middle part of device 23, connects in the fixing device slot 231 of blade after moving block about 11 two ends socket moving block bearing 111；Moving block 11 top middle portion offers moving block strip groove 112, and horizontal through hole 233 has also been offered in direction perpendicular with the fixing device slot 231 of blade in the middle part of the fixing device 23 of blade, when moving block 11 connects after in the fixing device slot 231 of blade, moving block strip groove 112 is overlapping in the same direction with horizontal through hole 233, in order to rod 22 of weighing and considering in order to uphold justice also cross the fixing device 23 of moving block 11 and blade；The fixing device 23 of blade is respectively arranged at the two ends with a vertical through hole 232 for passing through with described primary blades 20, and primary blades 20 is fixedly mounted on fixing device 23 two ends of blade by primary blades bolt 201, primary blades nut 202；Weighing and considering in order to uphold justice the rod 22 horizontal through hole 233 through the fixing devices 23 of blades, both sides are fixed on blade fix on device 23 with rod bearing 221 of weighing and considering in order to uphold justice rods 22 of will weighing and considering in order to uphold justice；One pair is installed symmetrically on excellent 22 both sides of weighing and considering in order to uphold justice weigh and consider in order to uphold justice blade 21, is fixedly mounted on 22 liang of tops of rod 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；Excellent 22 both sides of weighing and considering in order to uphold justice also are provided with a secondary counterweight set 24 symmetrically, are fixedly mounted on excellent 22 both sides of weighing and considering in order to uphold justice by hexagon socket head cap screw 241；Weigh and consider in order to uphold justice excellent 22 both sides near the fixing device 23 of blade positional symmetry a pair be installed weigh and consider in order to uphold justice baseball shape overcoat 26, weigh and consider in order to uphold justice baseball shape overcoat 26 one end be sleeved on weigh and consider in order to uphold justice rod 22, fixed by spherical overcoat bolt 261, the other end is provided with snap ring, it is connected to break-in bar 27, break-in bar 27 includes mutually threaded club 271, the connecting rod collar 272, can change connection state by regulating the rotation of screw thread therebetween；Break-in bar 27 one end is connected with baseball shape overcoat 26 of weighing and considering in order to uphold justice by club 271, the other end by the connecting rod collar 272 with acutangulate with horizontal plane " ten " shaped frame 25 is connected, acutangulate with horizontal plane " ten " shaped frame 25 is set to crosswise, each angle at four angles is both provided with spherical junctional complex, is connected with the connecting rod collar 272.
In the middle part of the described fixing device 23 of excellent 22 penetrating blades of weighing and considering in order to uphold justice and the notch 112 on moving block 11 top, also segmentation is fixed simultaneously, counterweight set 24, the fixing blade 21 of weighing and considering in order to uphold justice in baseball shape overcoat 26 two ends of weighing and considering in order to uphold justice so that it is the purpose of the body that reaches to weigh and consider in order to uphold justice.Described baseball shape overcoat 26 one end of weighing and considering in order to uphold justice is fixed on weighs and consider in order to uphold justice on rod 22, and the other end is connected on the pitch 25 of aeromodelling airplane with the connecting rod collar 272 so that it is turn to and the head frame assembly of body are synchronously performed.And the fixed center point of the primary blades 20 of head frame assembly, blade 21 of weighing and considering in order to uphold justice is all on the fixing device 23 of blade, what make aeromodelling airplane turns to the purpose having reached automatically to weigh and consider in order to uphold justice.
Aviation aircraft smooth flight system provided by the invention, due to be provided with the fixing device of blade, moving block, run through the fixing device of described blade and moving block weigh and consider in order to uphold justice rod and what horizontal plane acutangulated " ten " shaped frame, break-in bar, baseball shape overcoat of weighing and considering in order to uphold justice, integral body automatically can be weighed and consider in order to uphold justice in the process turned to, thus the sporting flying more steadily smoothness of aeromodelling airplane can be made, will not disintegrate because of the out of control of centrifugal force, it is ensured that the use safety of aviation aircraft itself and manipulator.
Above disclosed it is only the preferred embodiments of the present invention, certainly can not limit the interest field of the present invention, the equivalent variations therefore made according to the present patent application the scope of the claims with this, still belong to the scope that the present invention contains.
Claims (9)
1. an aviation aircraft smooth flight system, it is characterized in that: include aviation aircraft driving shaft and fix, with described aviation aircraft driving shaft, the tumbler being connected, described tumbler includes the secondary primary blades that connected by the fixing device of blade and a pair is weighed and consider in order to uphold justice blade.
2. aviation aircraft smooth flight system according to claim 1, it is characterised in that: described aviation aircraft smooth flight system also includes the moving block for connecting described driving shaft and described tumbler；In the middle part of the fixing device of described blade, side is provided with a slot down, is connected in the middle part of the fixing device of described blade in slot after two ends, institute's moving block left and right socket bearing.
3. aviation aircraft smooth flight system according to claim 2, it is characterised in that: described moving block top middle portion is provided with strip groove, and its tail end is provided with the horizontal direction through hole for being connected by straight pin with described driving shaft.
4. aviation aircraft smooth flight system according to claim 2, it is characterized in that: weigh and consider in order to uphold justice blade, the fixing device of described blade of a described secondary primary blades, a described pair is arranged on same level, and described moving block is installed vertically on described blade after being connected with described driving shaft head and the tail and fixes the downside of device.
5. aviation aircraft smooth flight system according to claim 1, it is characterised in that: the fixing device of described blade is respectively arranged at the two ends with the vertical direction through hole for being bolted with described primary blades.
6. aviation aircraft smooth flight system according to claim 1, it is characterised in that: described tumbler also includes the rod of weighing and considering in order to uphold justice being connected with the fixing device of described blade；Described blade of weighing and considering in order to uphold justice be arranged at described in weigh and consider in order to uphold justice rod two tops；The horizontal direction through hole for being connected it is additionally provided with described rod of weighing and considering in order to uphold justice in the middle part of the fixing device of described blade.
7. aviation aircraft smooth flight system according to claim 6, it is characterised in that: described tumbler also include being sleeved on described driving shaft set the horizontal of acute angle " ten " shaped frame.
8. aviation aircraft smooth flight system according to claim 8, it is characterized in that: described tumbler also include being arranged on described in weigh and consider in order to uphold justice at least one pair at rod two ends, left and right weigh and consider in order to uphold justice baseball shape overcoat, its one end weighs and consider in order to uphold justice on rod described in being sleeved on, and the other end acutangulates with horizontal plane with described " ten " shaped frame is connected.
9. aviation aircraft smooth flight system according to claim 8, it is characterized in that: described tumbler also includes described acutangulating with horizontal plane for connecting " ten " the break-in bar of shaped frame and described baseball shape overcoat of weighing and considering in order to uphold justice, its one end is connected with described baseball shape overcoat of weighing and considering in order to uphold justice, and the other end acutangulates with horizontal plane with described " ten " shaped frame is connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410834822.XA CN105771268A (en) | 2014-12-26 | 2014-12-26 | Steady flight system for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410834822.XA CN105771268A (en) | 2014-12-26 | 2014-12-26 | Steady flight system for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105771268A true CN105771268A (en) | 2016-07-20 |
Family
ID=56389104
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410834822.XA Pending CN105771268A (en) | 2014-12-26 | 2014-12-26 | Steady flight system for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105771268A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106621383A (en) * | 2015-11-04 | 2017-05-10 | 许美兰 | Aircraft stable flying system |
-
2014
- 2014-12-26 CN CN201410834822.XA patent/CN105771268A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106621383A (en) * | 2015-11-04 | 2017-05-10 | 许美兰 | Aircraft stable flying system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102862677A (en) | Double-wing type miniature bionic ornithopter | |
| CN105857628A (en) | Self-balancing anti-collision aircraft | |
| CN204380269U (en) | A kind of high-altitude flight toy balance control mechanism | |
| CN104787327A (en) | Axle distance-variable multi-rotor aircraft | |
| CN105620736B (en) | A kind of unmanned transporter | |
| CN106621383A (en) | Aircraft stable flying system | |
| CN105561604A (en) | Stable flight system for aviation aircraft | |
| CN105771268A (en) | Steady flight system for aircraft | |
| CN106706261B (en) | Balance measuring device for rolling rotation derivative experiment | |
| CN105771270A (en) | Aerial dynamic balance control device of high-altitude flight toy | |
| CN202848024U (en) | Propeller hub assembly used for small and medium-sized unmanned helicopters | |
| CN205022854U (en) | Deformable compound aircraft | |
| CN106516105B (en) | Aircraft oar face adjustment mechanism | |
| CN105797388A (en) | Air dynamic balance control device for high-altitude flying toy | |
| CN106669184A (en) | Model airplane switcher | |
| CN106669179A (en) | Smooth flight system of aircraft | |
| CN205469853U (en) | Self -balancing anticollision aircraft | |
| CN106693389A (en) | Smooth flight system of air vehicle | |
| CN107335237A (en) | A kind of dish-style flying toy | |
| CN109464812A (en) | Model plane with secondary blade control system of weighing and considering in order to uphold justice | |
| CN107149775A (en) | Switcher of model airplane remote controller | |
| CN109107179A (en) | A kind of aviation aircraft smooth flight system | |
| CN200987917Y (en) | Automatic balancing head stock device for model airplane | |
| CN108261777A (en) | A kind of toy airplane assembly with the microprocessor for assisting flight | |
| CN108607223A (en) | It is a kind of to can be used for waterborne and aerial photographing photographic aviation device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160720 |
|
| WD01 | Invention patent application deemed withdrawn after publication |