CN105999711A - Manipulable simulated helicopter - Google Patents
Manipulable simulated helicopter Download PDFInfo
- Publication number
- CN105999711A CN105999711A CN201610514634.8A CN201610514634A CN105999711A CN 105999711 A CN105999711 A CN 105999711A CN 201610514634 A CN201610514634 A CN 201610514634A CN 105999711 A CN105999711 A CN 105999711A
- Authority
- CN
- China
- Prior art keywords
- helicopter
- passenger
- steel wire
- high tower
- rotor
- 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
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63G—MERRY-GO-ROUNDS; SWINGS; ROCKING-HORSES; CHUTES; SWITCHBACKS; SIMILAR DEVICES FOR PUBLIC AMUSEMENT
- A63G31/00—Amusement arrangements
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
- G09B9/46—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer the aircraft being a helicopter
Landscapes
- Engineering & Computer Science (AREA)
- Theoretical Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Business, Economics & Management (AREA)
- Physics & Mathematics (AREA)
- Educational Administration (AREA)
- Educational Technology (AREA)
- General Physics & Mathematics (AREA)
- Toys (AREA)
Abstract
The invention relates to a manipulable simulated helicopter. The manipulable simulated helicopter mainly comprises a helicopter, a high tower, a steel wire, a pulley block and a clump weight. The manipulable simulated helicopter is characterized by only moving up and down under the limiting action of the high tower, the steel wire and the pulley block. The possibility that the helicopter is out of control is avoided. Due to arrangement of the clump weight, the simulated helicopter can ascend only by a tiny lift force. The simulated helicopter as mentioned above can move upwards and downwards under the control of a passenger, and also can rotate left and right under the control of the passenger. The manipulable simulated helicopter has the advantages that the simulated helicopter can only move up and down under the limiting action of the high tower, the steel wire and the pulley block, so that the possibility that the helicopter is out of control is avoided; due to arrangement of the clump weight, the simulated helicopter can ascend only by the tiny lift force.
Description
(1) technical field
The present invention relates to a kind of controllable simulation helicopter.
(2) background technology
Helicopter is the aircraft that a few peoples can drive.Technology requires height, and cost of use is high.
(3) summary of the invention
It is an object of the invention to design a kind of controllable simulation helicopter.Everybody can be allowed in safe and reliable feelings
Condition experience manipulation helicopter.
Technical scheme: a kind of controllable simulation helicopter.Main by helicopter, high tower, steel wire, cunning
Wheels, balancing weight form.Helicopter is connected to the steel wire on assembly pulley, and steel wire is furnished with pouring weight, and helicopter can taken advantage of
Upwards move downward under the control of member, it is also possible to left rotation and right rotation under the control of occupant.
The superiority of the present invention: owing to simulation helicopter is can only be upper and lower under, the restriction of high tower, steel wire, assembly pulley
Motion.Avoid the possibility that helicopter is out of control.Owing to being furnished with pouring weight simulation helicopter, to have only to minimum lift the most permissible
Rise.
(4) accompanying drawing explanation
Accompanying drawing 1 is the structural representation of the present invention；
Wherein: 1, assembly pulley, 2, high tower, 3, helicopter, 4, steel wire, 5, balancing weight.
(5) detailed description of the invention
As shown in drawings: controllable simulation helicopter, mainly by 1, assembly pulley, 2, high tower, 3, helicopter, 4,
Steel wire, 5, balancing weight composition.It is characterized in that: helicopter (3) be, high tower (2), steel wire (4), the restriction of assembly pulley (1)
Under can only move up and down.The rotor of helicopter (3) is by electromotor or motor-driven, and passenger controls electromotor or motor merit
Rate size just can be handled helicopter (3) and fly up and down.The left and right pedal that passenger controls helicopter (3) inner handles helicopter
(3) tail-rotor just can handle helicopter (3) left rotation and right rotation.
The above, be only presently preferred embodiments of the present invention, and the present invention not makees any pro forma restriction, all
It is based on any simple modification, equivalent variations and modification that above example is made by the technical spirit of the present invention, all still falls within
In the range of technical solution of the present invention.
Claims (7)
1. with controllable simulation helicopter mainly by 1, an assembly pulley, 2, high tower, 3, helicopter, 4, steel wire, 5, join
Pouring weight forms.
It is characterized in that: helicopter (3) is can only to move up and down under, the restriction of high tower (2), steel wire (4), assembly pulley (1).
The rotor of helicopter (3) is by electromotor or motor-driven, and passenger controls electromotor or motor power (output) size just can be handled
Helicopter (3) flies up and down.Passenger controls the tail-rotor of inner left and right pedal manipulation helicopter (3) of helicopter (3) and just may be used
Handle helicopter (3) left rotation and right rotation.
High tower the most according to claim 1 (2) can be by head tower, high building, building or any have height object constitute.
Helicopter the most according to claim 1 (3) be under, the restriction of high tower (2), steel wire (4), assembly pulley (1) only
Can move up and down.
The rotor of helicopter the most according to claim 1 (3) is controlled electromotor by electromotor or motor-driven, passenger
Or motor power (output) size just can handle helicopter (3) and fly up and down.
Passenger the most according to claim 1 controls the inner left and right pedal of helicopter (3) and handles the tail-rotor of helicopter (3)
Just can handle helicopter (3) left rotation and right rotation.
Helicopter the most according to claim 1 (3) has 2 steel wires to connect between balancing weight (5), plays security insurance and makees
With.
The small-sized balancing weight of polylith can be added on helicopter the most according to claim 1 (3).Counterweight can be carried out according to passenger size
To predetermined weight.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610514634.8A CN105999711A (en) | 2016-07-04 | 2016-07-04 | Manipulable simulated helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610514634.8A CN105999711A (en) | 2016-07-04 | 2016-07-04 | Manipulable simulated helicopter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105999711A true CN105999711A (en) | 2016-10-12 |
Family
ID=57107801
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610514634.8A Pending CN105999711A (en) | 2016-07-04 | 2016-07-04 | Manipulable simulated helicopter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105999711A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114310734A (en) * | 2022-03-14 | 2022-04-12 | 中国空气动力研究与发展中心低速空气动力研究所 | Airplane model sinking and floating supporting device and four-degree-of-freedom supporting device |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN86103436A (en) * | 1986-05-24 | 1988-06-01 | 僧全松 | Aeronautic amusement machine with flapping-and rotating wings |
| CN2045664U (en) * | 1988-07-14 | 1989-10-11 | 北京航空航天大学(原北京航空学院) | Manpower helicopter entertainment equipment |
| CN2357774Y (en) * | 1997-06-28 | 2000-01-12 | 刘勋 | Flying saucer game machine |
| CN1731124A (en) * | 2005-07-04 | 2006-02-08 | 浙江大学 | Test bench for testing flight performance of small-sized helicopter |
| CN201168431Y (en) * | 2007-11-26 | 2008-12-24 | 周德俊 | Helicopter simulating recreational and training dual-purpose system |
| JP2014238430A (en) * | 2013-06-06 | 2014-12-18 | 康郁 秋山 | Flying object piloting-training device |
-
2016
- 2016-07-04 CN CN201610514634.8A patent/CN105999711A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN86103436A (en) * | 1986-05-24 | 1988-06-01 | 僧全松 | Aeronautic amusement machine with flapping-and rotating wings |
| CN2045664U (en) * | 1988-07-14 | 1989-10-11 | 北京航空航天大学(原北京航空学院) | Manpower helicopter entertainment equipment |
| CN2357774Y (en) * | 1997-06-28 | 2000-01-12 | 刘勋 | Flying saucer game machine |
| CN1731124A (en) * | 2005-07-04 | 2006-02-08 | 浙江大学 | Test bench for testing flight performance of small-sized helicopter |
| CN201168431Y (en) * | 2007-11-26 | 2008-12-24 | 周德俊 | Helicopter simulating recreational and training dual-purpose system |
| JP2014238430A (en) * | 2013-06-06 | 2014-12-18 | 康郁 秋山 | Flying object piloting-training device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114310734A (en) * | 2022-03-14 | 2022-04-12 | 中国空气动力研究与发展中心低速空气动力研究所 | Airplane model sinking and floating supporting device and four-degree-of-freedom supporting device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| DD01 | Delivery of document by public notice | ||
| DD01 | Delivery of document by public notice |
Addressee: Lei Yi Document name: the First Notification of an Office Action |
|
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20161012 |