CN101934152B - Vectoring nozzle model jet aircraft - Google Patents
Vectoring nozzle model jet aircraft Download PDFInfo
- Publication number
- CN101934152B CN101934152B CN2010101025173A CN201010102517A CN101934152B CN 101934152 B CN101934152 B CN 101934152B CN 2010101025173 A CN2010101025173 A CN 2010101025173A CN 201010102517 A CN201010102517 A CN 201010102517A CN 101934152 B CN101934152 B CN 101934152B
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- spout
- steering wheel
- nozzle
- steering gear
- manipulating wire
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Abstract
The invention relates to a vectoring nozzle model jet aircraft which comprises a body, a first nozzle, a second nozzle, a first steering gear, a second steering gear, a third steering gear, a first lifting operating steel wire, a second lifting operating steel wire, a first direction operating steel wire, a second direction operating steel wire and a three-fork rocker arm. The first nozzle and the second nozzle are respectively mounted on two sides of the tail part of the body, the first steering gear is arranged on the body positioned at the left part at the front end of the first nozzle, the second steering gear is arranged on the body positioned at the right part at the front end of the second nozzle, the third steering gear is arranged on the body at the middle part at the front ends of the first nozzle and the second nozzle, the three-fork rocker arm is mounted on the third steering gear, the first steering gear is connected with the first nozzle through the first lifting operating steel wire, the second steering gear is connected with the second nozzle through the second lifting operating steel wire, and the first nozzle and the second nozzle are respectively connected on the three-fork rocker arm through the first direction operating steel wire and the second direction operating steel wire and connected with the third steering gear.
Description
Technical field
The present invention relates to a kind of model of an airplane, refer more particularly to a kind of vector spray model jet airplane that can imitate the such up-down of true aircraft, lift-over and driftage.
Background technology
At present the type of the model of an airplane is very many, also is to be seen everywhere on the market with regard to the model of an airplane of jet power class.And the general type likelihood aircraft in moulding just of the being seen on the market at present model of an airplane, the model jet airplane of really accomplishing to resemble the similar action of the up-down of true aircraft, lift-over and driftage, also discovery on the market.And facts have proved the model of type likelihood aircraft more, doted on by the consumer more easily on the market.And the key technology of accomplishing to resemble up-down the true aircraft, lift-over and driftage is that also the spout of the model of an airplane turns to the control design.So designing spout that a key technology that can imitate the model of an airplane that resembles up-down the true aircraft, lift-over and driftage also is how to design the control aircraft, to turn to technology be the vector spray technology.
Summary of the invention
The object of the invention just provides a kind of vector spray model jet that can imitate the such up-down of true aircraft, lift-over and driftage.
A kind of vector spray model jet airplane, it comprises a fuselage, one first spout, one second spout, one first steering wheel, one second steering wheel, one the 3rd steering wheel, one first up-down manipulating wire, one second up-down manipulating wire, a first direction manipulating wire, a second direction manipulating wire, a trident rocking arm.
This first spout, second spout are installed in the two sides of tail of this fuselage respectively; This first steering wheel is arranged on the fuselage of left-hand portion of front end of this first spout; This second steering wheel is arranged on the fuselage at position, right side of front end of this second spout; The 3rd steering wheel is arranged on the fuselage of middle part of front end of this first, second spout; This trident rocking arm is installed on the 3rd steering wheel; Be connected through the first up-down manipulating wire between this first steering wheel and first spout, the second up-down manipulating wire is connected between this second steering wheel and second spout, and this first spout, second spout are connected on the trident rocking arm through first direction manipulating wire, second direction manipulating wire respectively and are connected with the 3rd steering wheel.
The invention has the advantages that: it controls the up-down that can control aircraft that swings up and down of first spout, second spout through the up-down manipulating wire that is connected between first steering wheel, second steering wheel and first spout, second spout; Through the up-down manipulating wire that is connected between first steering wheel, second steering wheel and first spout, second spout control first spout upwards swing, second spout to lower swing or control first spout can be controlled lift-over from aircraft to the upwards swing of lower swing, second spout; Directional control steel wire through being connected between the 3rd steering wheel and first spout, second spout is controlled the left and right sides yawed flight that swinging of first spout, second spout can be controlled aircraft; Can reach through the present invention design and to make this model of an airplane resemble the up-down of true aircraft, lift-over and driftage, to satisfy the consumer's who likes the aircraft that uses a model the demand that plays greatly.
Description of drawings
Fig. 1 is the structural representation of vector spray model jet of the present invention.
The specific embodiment
Please refer to Fig. 1; A kind of vector spray model jet, it comprises a fuselage 1, one first spout 2, one second spout 3, one first steering wheel 4, one second steering wheel 5, one the 3rd steering wheel 6, one first up-down manipulating wire 7, one second up-down manipulating wire 8, a first direction manipulating wire 9, a second direction manipulating wire 10, a trident rocking arm 11.
This first spout 2, second spout 3 are installed in the afterbody of this fuselage 1 respectively; This first steering wheel 4 is arranged on the fuselage 1 of left-hand portion of front end of this first spout 2; This second steering wheel 5 is arranged on the fuselage 1 at position, right side of front end of this second spout 3; The 3rd steering wheel 6 is arranged on the fuselage 1 of middle part of front end of this first, second spout 2,3; This trident rocking arm 11 is installed on the 3rd steering wheel 6; Be connected through the first up-down manipulating wire 7 between this first steering wheel 4 and first spout 2, the second up-down manipulating wire 8 is connected between this second steering wheel 5 and second spout 3, and this first spout 2, second spout 3 are connected on the trident rocking arm 11 through first direction manipulating wire 9, second direction manipulating wire 10 respectively and are connected with the 3rd steering wheel 6.
Operation principle of the present invention is following: start this model of an airplane; And driving the running of three steering wheels, it controls the up-down that can control aircraft that swings up and down of first spout, second spout through the up-down manipulating wire that is connected between first steering wheel, second steering wheel and first spout, second spout; Through the up-down manipulating wire that is connected between first steering wheel, second steering wheel and first spout, second spout control first spout upwards swing, second spout simultaneously to lower swing or control first spout can be controlled rolling flight from aircraft to the upwards swing of lower swing, second spout; Directional control steel wire through being connected between the 3rd steering wheel and first spout, second spout is controlled the left and right sides yawed flight that swinging of first spout, second spout can be controlled aircraft.
Explain: every interior any simple modification, equivalent variations and modification of perhaps according to technical spirit of the present invention above scheme being done that does not break away from technical scheme of the present invention all still belongs within the protection domain of the present invention.
Claims (1)
1. vector spray model jet airplane, it is characterized in that: it comprises a fuselage, one first spout, one second spout, one first steering wheel, one second steering wheel, one the 3rd steering wheel, one first up-down manipulating wire, one second up-down manipulating wire, a first direction manipulating wire, a second direction manipulating wire, a trident rocking arm; This first spout, second spout are installed in the two sides of tail of this fuselage respectively; This first steering wheel is arranged on the fuselage of left-hand portion of front end of this first spout; This second steering wheel is arranged on the fuselage at position, right side of front end of this second spout; The 3rd steering wheel is arranged on the fuselage of middle part of front end of this first, second spout; This trident rocking arm is installed on the 3rd steering wheel; Be connected through the first up-down manipulating wire between this first steering wheel and first spout, the second up-down manipulating wire is connected between this second steering wheel and second spout, and this first spout, second spout are connected on the trident rocking arm through first direction manipulating wire, second direction manipulating wire respectively and are connected with the 3rd steering wheel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010101025173A CN101934152B (en) | 2010-01-25 | 2010-01-25 | Vectoring nozzle model jet aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010101025173A CN101934152B (en) | 2010-01-25 | 2010-01-25 | Vectoring nozzle model jet aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN101934152A CN101934152A (en) | 2011-01-05 |
| CN101934152B true CN101934152B (en) | 2012-01-25 |
Family
ID=43387866
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010101025173A Expired - Fee Related CN101934152B (en) | 2010-01-25 | 2010-01-25 | Vectoring nozzle model jet aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101934152B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107389296B (en) * | 2015-10-28 | 2019-09-13 | 中国航空工业集团公司沈阳飞机设计研究所 | A kind of model aircraft for wind-tunnel |
| CN108910057B (en) * | 2018-06-10 | 2024-03-29 | 东莞理工学院 | Flying wing unmanned aerial vehicle with multiple engines |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3796005A (en) * | 1973-02-23 | 1974-03-12 | Mattel Inc | Simulated jet airplane toy |
| CN2447030Y (en) * | 2000-07-13 | 2001-09-12 | 贵阳本生新产品研究所 | Model plane |
| CN200970477Y (en) * | 2006-11-23 | 2007-11-07 | 深圳市艾特电子技术有限公司 | Artificial plane model |
| CN200973981Y (en) * | 2006-11-23 | 2007-11-14 | 深圳市艾特电子技术有限公司 | Simulated airplane model |
| GB2455145A (en) * | 2007-11-30 | 2009-06-03 | Ping-Sung Chang | Toy aeroplane powered by hydraulic power |
-
2010
- 2010-01-25 CN CN2010101025173A patent/CN101934152B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3796005A (en) * | 1973-02-23 | 1974-03-12 | Mattel Inc | Simulated jet airplane toy |
| CN2447030Y (en) * | 2000-07-13 | 2001-09-12 | 贵阳本生新产品研究所 | Model plane |
| CN200970477Y (en) * | 2006-11-23 | 2007-11-07 | 深圳市艾特电子技术有限公司 | Artificial plane model |
| CN200973981Y (en) * | 2006-11-23 | 2007-11-14 | 深圳市艾特电子技术有限公司 | Simulated airplane model |
| GB2455145A (en) * | 2007-11-30 | 2009-06-03 | Ping-Sung Chang | Toy aeroplane powered by hydraulic power |
Also Published As
| Publication number | Publication date |
|---|---|
| CN101934152A (en) | 2011-01-05 |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120125 Termination date: 20130125 |