CN201227539Y - Helicopter simulated flight system - Google Patents
Helicopter simulated flight system Download PDFInfo
- Publication number
- CN201227539Y CN201227539Y CNU2007203001459U CN200720300145U CN201227539Y CN 201227539 Y CN201227539 Y CN 201227539Y CN U2007203001459 U CNU2007203001459 U CN U2007203001459U CN 200720300145 U CN200720300145 U CN 200720300145U CN 201227539 Y CN201227539 Y CN 201227539Y
- Authority
- CN
- China
- Prior art keywords
- helicopter
- push rod
- pedestal
- mandril
- casing
- 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.)
- Expired - Fee Related
Links
Abstract
The utility model relates to a helicopter flight simulation system which can do rotation and revolution motions, belongs to the recreation facility field and comprises a hydraulic pedestal, a mandril and helicopter casings. The scale frame type mandril is connected to the elevating hydraulic pedestal, both ends of the mandril are respectively connected with one helicopter casing, the airscrews of the helicopter casings are connected with common gasoline engines, the tail rotor of a helicopter comprises a common fan which is connected with a storage battery, the airscrews are controlled by a navigation space, and the hydraulic pedestal is connected with a main control system.
Description
Technical field
The utility model relates to the recreational facilities field, is a kind of helicopter simulated flight system that does rotation and revolution.
Technical background
At present, society enters into the aircraft epoch by bicycle epoch, motorcycle epoch, auto age, can fly is one of main dream human over millions upon millions of years, but can't fly by the self-condition restriction mankind, so take the important alternatives that flight tool becomes human flight, but be subjected to time, economy, meteorological effect, most of people can't participate in, and have the factor of aspect such as safety, this activity can not be popularized.
Summary of the invention
This practical purpose provides a kind of helicopter casing that is erected on the pedestal, takes to people, by the lifting of pedestal and the rotation and the revolution motion of helicopter casing, simulates helicopter flight.
The utility model is achieved in that and is connecting push rod on the Liftable hydraulic pedestal.Connect the helicopter casing on the push rod.The screw of going straight up to casing connects the regular gasoline machine, and the tail-rotor of helicopter is made up of conventional fan, and fan connects battery, and screw is controlled by driver's cabin, and hydraulic base connects main control system.
Because adopt such scheme, the utility model can be simulated the helicopter lifting, hovers in the air and flies.Be not subjected to the influence of time, economy, meteorology yet, can use throughout the year, both safe and reliable, can experience the enjoyment that helicopt is flown aloft again.
Description of drawings:
Fig. 1 is a front view of the present utility model
In the drawings: 1, helicopter; 2, hydraulic base; 3, push rod; 4, motor; 5, gasoline engine; 6, battery; 7, tail-rotor; 8, main control system; 9, screw; 10, driver's cabin.
The specific embodiment
Below in conjunction with drawings and Examples the utility model is further described:
In Fig. 1: go up connection push rod (3) at Liftable hydraulic pedestal (2), push rod (3) is gone up and is connected helicopter shell (1), the screw of helicopter casing (9) connects gasoline engine (5), the tail-rotor (7) of helicopter (1) is made up of the common electrical fan, holding storage battery (6) in the helicopter, fan is by battery (6) power supply, and screw (9) is controlled by driver's cabin.Push rod (3) is driven by motor (4) and rotates on pedestal.Hydraulic support (2) is controlled by main control system (8).
Lifting by main control system control hydraulic support, produce helicopter lifting effect, driving screw by gasoline engine rotates, the rotation of electric fan and the rotation of motor, make the helicopter casing produce the effect of spiraling, flying, the helicopter casing is done 360 ° of rotations on push rod under the driving of tail-rotor, the Motor Drive push rod rotates around support, makes the helicopter casing produce the effect of doing 360 ° of revolution around hydraulic base.So the occupant produces a kind of amusement sensation of flight aloft.
Claims (1)
1, helicopter simulated flight system, it is characterized in that: go up a connection day flatrack push rod (3) at Liftable hydraulic support (2), push rod (3) is gone up two ends and is respectively connected a helicopter shell (1), the screw of helicopter casing (9) connects gasoline engine motor (5), helicopter (1) connects tail-rotor (7), holding storage battery (6) in the helicopter, and tail-rotor (7) connects battery (6), push rod (3) is driven by motor (4) and rotates on pedestal, and hydraulic support (2) is controlled by main control system (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007203001459U CN201227539Y (en) | 2007-12-17 | 2007-12-17 | Helicopter simulated flight system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007203001459U CN201227539Y (en) | 2007-12-17 | 2007-12-17 | Helicopter simulated flight system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201227539Y true CN201227539Y (en) | 2009-04-29 |
Family
ID=40632499
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2007203001459U Expired - Fee Related CN201227539Y (en) | 2007-12-17 | 2007-12-17 | Helicopter simulated flight system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201227539Y (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8979660B2 (en) | 2010-10-26 | 2015-03-17 | Aba Science Play Ltd. | Helicopter amusement apparatus |
-
2007
- 2007-12-17 CN CNU2007203001459U patent/CN201227539Y/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8979660B2 (en) | 2010-10-26 | 2015-03-17 | Aba Science Play Ltd. | Helicopter amusement apparatus |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN202728572U (en) | Multi-rotor aircraft | |
| CN206502014U (en) | A kind of single duct engine | |
| CN206494123U (en) | A kind of aircraft | |
| CN204279919U (en) | For folding oar pull-type before motor glider | |
| CN206358362U (en) | A kind of manned flapping-wing machine | |
| CN208915439U (en) | Adjustable wing swallow shape simulation type unmanned plane | |
| CN201227539Y (en) | Helicopter simulated flight system | |
| CN207292407U (en) | A kind of two rotor personal aircrafts of new cross-arranging type | |
| CN203220761U (en) | Multi-rotor aircraft | |
| CN205554566U (en) | Innovative small -size unmanned vehicles | |
| CN2392582Y (en) | Sport-composition type 3D space freedom model helicopter | |
| CN107284165A (en) | A kind of coaxial double-rotary wing land and air double-used aircraft | |
| CN208963310U (en) | It is a kind of can VTOL vert the fixed-wing unmanned plane of quadrotor | |
| CN217170962U (en) | Bionic bird capable of automatically folding wing | |
| CN106005412B (en) | Flying disk type VTOL high speed electromagnetic aircraft | |
| CN2423940Y (en) | Romoto-control electric aeroplane | |
| CN102336271A (en) | Butterfly-shaped aircraft | |
| CN202128907U (en) | Multifunctional intelligent kite | |
| CN205060007U (en) | Four portable rotor unmanned aerial vehicle | |
| CN201101893Y (en) | Telecontrolled model helicopter | |
| CN206394895U (en) | Oil electric mixed dynamic rotor manned aircraft | |
| CN201179335Y (en) | Cable car type riding system of helicopter | |
| CN206265298U (en) | A kind of manned travelling waterborne is tethered at multi-rotor aerocraft | |
| CN205055430U (en) | But differential steering's high mobility model propeller aircraft | |
| CN205554587U (en) | Solar energy power rogallo |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20090429 Termination date: 20101217 |