CN205598645U - Can assist radiating stationary vane model aeroplane and model ship aircraft parachuting mechanism - Google Patents
Can assist radiating stationary vane model aeroplane and model ship aircraft parachuting mechanism Download PDFInfo
- Publication number
- CN205598645U CN205598645U CN201620333905.5U CN201620333905U CN205598645U CN 205598645 U CN205598645 U CN 205598645U CN 201620333905 U CN201620333905 U CN 201620333905U CN 205598645 U CN205598645 U CN 205598645U
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- Prior art keywords
- axle
- parachuting
- aircraft
- model
- support shaft
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- 238000009434 installation Methods 0.000 claims abstract description 10
- 230000017525 heat dissipation Effects 0.000 claims description 10
- 235000017166 Bambusa arundinacea Nutrition 0.000 abstract 2
- 235000017491 Bambusa tulda Nutrition 0.000 abstract 2
- 241001330002 Bambuseae Species 0.000 abstract 2
- 235000015334 Phyllostachys viridis Nutrition 0.000 abstract 2
- 239000011425 bamboo Substances 0.000 abstract 2
- 210000001331 Nose Anatomy 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 206010022114 Injury Diseases 0.000 description 1
- 230000003139 buffering Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000035800 maturation Effects 0.000 description 1
- 230000001681 protective Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
Abstract
The utility model provides a can assist radiating stationary vane model aeroplane and model ship aircraft parachuting mechanism, includes aircraft body, install engine and back shaft on aircraft body's the aircraft nose. The cover is equipped with section of thick bamboo axle on the back shaft, the epaxial the propeller blades that installs of a section of thick bamboo. A set seat is installed on the back shaft top, install radome fairing, descending pack and installation axle on the dish seat, installation off -axial end position is in the fixed orifices that the radome fairing set up, it is equipped with the catapult to install epaxial cover, the descending pack lies in the radome fairing, back shaft, dish seat and installation axle all are provided with air vent coaxial and mutual intercommunication, back shaft the inner is connected with the jet -propelled pipe that is linked together with the air vent, the jet -propelled pipe other end is towards the engine. Can assist radiating stationary vane model aeroplane and model ship aircraft parachuting mechanism can open the parachute at the aircraft foremost, when making the condition such as the aircraft breaks down, can slowly land, prevents to pound the pedestrian because of the crash, avoids causing the incident.
Description
Technical field
This utility model relates to a kind of aeromodelling airplane, a kind of can the fixed-wing aeromodelling airplane parachuting machine of auxiliary heat dissipation
Structure.
Background technology
Along with the raising of material life, the maturation of model plane product, increasing people purchases aeromodelling airplane and carries out amusement and leisure.Mesh
Front people play aeromodelling airplane place and are concentrated mainly on park, vacant lot, community, but these local pedestrians are more, when aeromodelling airplane flies
During break down, fall, be very easy to pound pedestrian, cause security incident.And starting due to aeromodelling airplane
The parts such as machine, controller are all located at fore-body, aeromodelling airplane run out of steam crash time, can land crash by head, electromotor,
The parts such as controller can directly damage, and causes bigger economic loss.
Utility model content
The deficiency that this utility model exists for above-mentioned prior art, propose a kind of can the fixed-wing aeromodelling airplane umbrella of auxiliary heat dissipation
Descending mechanism.
Of the present utility model can the fixed-wing aeromodelling airplane parachuting mechanism of auxiliary heat dissipation, including airframe, described airframe
Head on electromotor and support shaft are installed.
It is set with an axle in described support shaft, described cylinder axle is provided with propeller blade.
Described support shaft top is provided with dish seat, described dish seat is provided with trousers, landing pack and installs axle, described installation
Axle outer end is positioned in the fixing hole that trousers is arranged, and described installation axle is set with ejector, and described landing pack is positioned at trousers
In；
Described support shaft, dish seat and installation axle are both provided with passage that is coaxial and that be interconnected, and described support shaft the inner connects to be had
The air jet pipe being connected with passage, the described air jet pipe other end is towards electromotor.
Being provided with controller in described airframe, described controller electrically connects with ejector.
Described cylinder axle the inner is provided with travelling gear, and the main shaft of described electromotor is provided with driving gear, described driving gear and biography
Moving gear engages.
Preferably, the inner end edge of told trousers is tangent with cylinder axle outer wall.
Preferably, described travelling gear is to be arranged on the internal gear that an axle is inner.
The beneficial effects of the utility model are: can the fixed-wing aeromodelling airplane parachuting mechanism of auxiliary heat dissipation can at aircraft foremost
Release a parachute, when making the situations such as aircraft breaks down, it is possible to slowly land, prevent from pounding pedestrian because crashing, it is to avoid cause peace
Full accident.Will also result in body injury owing to the aeromodelling airplane of parachuting lands, parachute is arranged on foremost, after opening, makes boat
During mould aircraft parachuting, head upward, makes tail first contact to earth, it is to avoid the vitals such as electromotor receive damage, makes model plane
Aircraft only need to repairing simple to afterbody can recover to use again.Parachute is arranged on fixing dish seat, it is to avoid parachute along with
Propeller rotates, and when preventing aeromodelling airplane from normally using, parachute is excited by mistake, also prevents from rotating during parachuting, it is ensured that parachuting
Journey falls steadily.Trousers protection landing pack, concurrently forms flow-guiding structure, and tangent with cylinder axle, it is ensured that model plane are overall
Aerodynamic demands.The many-section desiccation hole being connected and air jet pipe, it is to avoid air-flow, energy are blocked in front end in whole parachuting mechanism
Enough introduce the stream in body, for engine radiating, reduce temperature during electromotor work, it is ensured that electromotor can be grown
Time steady operation, does not results in again the change of whole aeromodelling airplane aerodynamic structures, it is ensured that the stability of flight simultaneously.
Accompanying drawing explanation
Accompanying drawing 1 is originally can the structural representation of fixed-wing aeromodelling airplane parachuting mechanism of auxiliary heat dissipation.
Detailed description of the invention
In order to be able to further appreciate that structure of the present utility model, feature and other purpose, in conjunction with appended preferred embodiment specifically
Bright as follows, illustrated preferred embodiment is merely to illustrate the technical solution of the utility model, and non-limiting this utility model.
Detailed description of the invention of the present utility model is as follows:
As shown in Figure 1, it is possible to the fixed-wing aeromodelling airplane parachuting mechanism of auxiliary heat dissipation includes airframe 1, airframe 1
Electromotor 2 and support shaft 3 are installed on head.
Being set with an axle 4 in support shaft 3, support shaft 3 is fixed, and cylinder axle 4 rotates in support shaft 3.It is provided with on cylinder axle 4
Propeller blade 5, forms propeller.
Support shaft 3 top is provided with dish seat 6, dish seat 6 is provided with trousers 7, landing pack 8 and installs axle 10.Install
Axle outer end is positioned in the fixing hole that trousers 7 is arranged, and installs and is set with ejector 8 on axle, and landing pack 8 is positioned at trousers 7
In.
The inner end edge of trousers 7 is tangent with cylinder axle 4 outer wall, not only acts as the effect of a protective cover, protects landing therein
Pack 8 and ejector 9, also guide result, the aerodynamic structures that composition aircraft is overall as an air-flow.
Support shaft 3, dish seat 6 and installation axle 10 are both provided with passage that is coaxial and that be interconnected, have support shaft 3 inner connection
The air jet pipe 13 being connected with passage, air jet pipe 13 other end is towards electromotor 2.The air-flow of aeromodelling airplane front end passes sequentially through
Axle 10, dish seat 6 and the passage of support shaft 3 are installed, spray to electromotor 2 finally by air jet pipe 13, lower the temperature for electromotor 2
Heat radiation.
Being provided with controller in airframe 1, controller electrically connects with ejector 9, controls ejector 9 by trousers 7 from dish
Flick on seat 6.
Cylinder axle 4 the inner is provided with travelling gear 11, and the main shaft of electromotor 2 is provided with driving gear 12, drives gear 12 and passes
Moving gear 11 engages, and makes electromotor 2 drive the propeller of cylinder axle 4 and propeller blade 5 composition to rotate, provides for aircraft flight
Power.
For avoiding drive mechanism to affect the aerodynamic structures that aeromodelling airplane is overall, travelling gear 11 is inner for being arranged on an axle 4
Internal gear, drive mechanism is hidden into inside.
When electromotor 2 breaks down, aeromodelling airplane stops, cylinder axle 4 and the dead stick of propeller blade 5 composition.Logical
Crossing remote controller and send instruction to controller, controller controls ejector 9 and is flicked from dish seat 6 by trousers 7, and land pack 8
Outside being exposed to, due to the effect of air-flow, deployment, draw whole aeromodelling airplane and carry out slow fall.
During slow fall, the head of airframe is upward, tail-down.When contacting to earth, tail first lands, when buffering is landed further
Impact, protection is positioned at head and the various electronic equipments of airframe front portion and other parts.
Claims (3)
1. one kind can the fixed-wing aeromodelling airplane parachuting mechanism of auxiliary heat dissipation, it is characterised in that include airframe (1), the head of described airframe (1) be provided with electromotor (2) and support shaft (3),
It is set with an axle (4) in described support shaft (3), described cylinder axle (4) is provided with propeller blade (5)；
Described support shaft (3) top is provided with dish seat (6), trousers (7), landing pack (8) are installed on described dish seat (6) and axle (10) is installed, described installation axle outer end is positioned in the fixing hole that trousers (7) is arranged, being set with ejector (9) on described installation axle, described landing pack (8) is positioned at trousers (7)；
Described support shaft (3), dish seat (6) and installation axle (10) are both provided with passage that is coaxial and that be interconnected, there is the air jet pipe (13) being connected with passage described support shaft (3) inner connection, and described air jet pipe (13) other end is towards electromotor (2)；
Being provided with controller in described airframe (1), described controller electrically connects with ejector (9)；
Described cylinder axle (4) the inner is provided with travelling gear (11), the main shaft of described electromotor (2) is provided with driving gear (12), and described driving gear (12) is engaged with travelling gear (11).
The most according to claim 1 can the fixed-wing aeromodelling airplane parachuting mechanism of auxiliary heat dissipation, it is characterised in that the inner end edge of told trousers (7) is tangent with cylinder axle (4) outer wall.
The most according to claim 1 can the fixed-wing aeromodelling airplane parachuting mechanism of auxiliary heat dissipation, it is characterised in that described travelling gear (11) is to be arranged on the internal gear that an axle (4) is inner.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620333905.5U CN205598645U (en) | 2016-04-20 | 2016-04-20 | Can assist radiating stationary vane model aeroplane and model ship aircraft parachuting mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620333905.5U CN205598645U (en) | 2016-04-20 | 2016-04-20 | Can assist radiating stationary vane model aeroplane and model ship aircraft parachuting mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205598645U true CN205598645U (en) | 2016-09-28 |
Family
ID=56973630
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620333905.5U Active CN205598645U (en) | 2016-04-20 | 2016-04-20 | Can assist radiating stationary vane model aeroplane and model ship aircraft parachuting mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205598645U (en) |
-
2016
- 2016-04-20 CN CN201620333905.5U patent/CN205598645U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170919 Address after: 266000 Shandong Province, Qingdao city Chengyang District Chunyang Road No. 88 building room 311 business days of the digital city Patentee after: Qingdao Haotian Xiangyu Aviation Technology Co. Ltd. Address before: 101.102, 266000, SME incubator building, 1 Kam Yip Road, Qingdao hi tech Industrial Development Zone, Shandong, China Patentee before: QINGDAO HAOTIANXIANG INTELLIGENT TECHNOLOGY CO., LTD. |
|
| TR01 | Transfer of patent right |