CN107497123A - It is remotely controlled the attached wing construction of fixed-wing model of an airplane rotary stacked type - Google Patents
It is remotely controlled the attached wing construction of fixed-wing model of an airplane rotary stacked type Download PDFInfo
- Publication number
- CN107497123A CN107497123A CN201710993572.8A CN201710993572A CN107497123A CN 107497123 A CN107497123 A CN 107497123A CN 201710993572 A CN201710993572 A CN 201710993572A CN 107497123 A CN107497123 A CN 107497123A
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- CN
- China
- Prior art keywords
- wing
- attached
- steering wheel
- construction
- fixed
- 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.)
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Classifications
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
- A63H27/02—Model aircraft
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- Toys (AREA)
Abstract
It is a kind of imitative pinion recovery method to be remotely controlled fixed-wing model of an airplane rotary stacked type attached wing construction, is combined using rotation and folding, and rotation poststack is attached on fuselage, and shared horizontal space is small, the underslung attached wing construction of rotary stacked type.The attached wing construction of described rotary stacked type includes the inner wing and outer wing of the rotating shaft of two panels steering wheel 2 interconnection, the leading edge closing of inner wing, and trailing edge and outer rim leave gap, first screwed in outer wing in interior slot with remote controller control steering wheel 2；Connected between inner wing and fuselage by the rotating shaft of steering wheel 1；Steering wheel 1 is fixed on fuselage, and the rotating shaft of steering wheel 1 is fixed on hinge blade-rotating axle sleeve, and blade-rotating axle sleeve is fixed on inner wing, and described hinge folds up and down for inner wing, and fin maximum flip angle in limitation.Inner wing is folded downwardly together together with the outer wing in slot in screw-in with remote controller control steering wheel 1, is attached on fuselage.When needing to take off, with remote controller control steering wheel 1 inner wing and outer wing roll up come, then with remote controller control steering wheel 2 outer wing back-out expansion.
Description
Technical field
The invention belongs to model airplane field, and in particular to a kind of wing configuration of the fixed-wing model of an airplane, particularly energy
The horizontal perpendicular attached wing of the attached fixed-wing model of an airplane of exhibition constructs, particularly a kind of attached wing construction of rotary stacked type.
Background technology
Because the wing of fixed-wing aeromodelling airplane is wider, lateral dimension is excessive to influence storage and movement.It is not portable, often turn round
Bent even damage wing.Wing is once folded up as ship carrier aircraft uses, causes center of gravity to raise, stability declines.If machine
Revolve and withdraw after the sub-level of the wing one, can also take very big fuselage space.
The content of the invention
The imitative pinion recovery method of the present invention, there is provided one kind rotation poststack is attached on fuselage, and shared horizontal space is small, underslung
The attached wing construction of rotary stacked type.The attached wing construction of described rotary stacked type includes the inner wing and outer wing of the rotating shaft of two panels steering wheel 2 interconnection, interior
The leading edge closing of the wing, trailing edge and outer rim leave gap, with remote controller control steering wheel 2 by outer wing screw in in slot；Inner wing and machine
Connected between body by the rotating shaft of steering wheel 1；Steering wheel 1 is fixed on fuselage, and the rotating shaft of steering wheel 1 is fixed on hinge blade-rotating axle sleeve, blade-rotating
Axle sleeve is fixed on inner wing, and described hinge folds up and down for inner wing, and fin maximum flip angle in limitation.Controlled with remote controller
Steering wheel 1 folds inner wing together with the outer wing in slot in screw-in downwardly together, is attached on fuselage.When needing to take off, to wider
Wide place, first with remote controller control steering wheel 1 inner wing together with the outer flapwise both sides in slot in screw-in dig come, it is open and flat after again
Outer wing is screwed out with remote controller control steering wheel 2 and deployed.The present invention remarkable result be：The attached span has larger area, energy after opening
Enough provide compared with lift.Wing rotation poststack is attached on fuselage, reduces horizontal space.It is an object of the invention to provide a kind of machine
The wing withdraw after without the span, become the shell of aircraft.Empennage can also use this method to withdraw, and transverse width is greatly decreased.
Personal aircraft can also use this construction, can travel and park on road as automobile after withdrawing wing.
Brief description of the drawings
Fig. 1 is that rear top view is opened in the attached span of fixed-wing model of an airplane rotary stacked type.Fig. 2 is that fixed-wing model of an airplane rotary stacked type is attached
Top view after wing outer wing cycle.Fig. 3 is that the attached wing inner wing of fixed-wing model of an airplane rotary stacked type contains poststack top view under outer wing.Fig. 4 is
The attached wing inner wing side view containing outer wing of fixed-wing model of an airplane rotary stacked type.
Embodiment
Inner wing and outer wing are made as shown in Figure 1, inner wing are connected on fuselage with steering wheel 1 and hinge, steering wheel 1 is fixed on
On fuselage, the rotating shaft of steering wheel 1 is fixed on hinge blade-rotating axle sleeve, drives hinge to rotate, and has a switching channels control steering wheel 1, from
And inner wing is driven to transfer.Outer wing steering wheel 2 is connected on inner wing again, steering wheel 2 is fixed on inner wing, and the rotating disk of steering wheel 2 is fixed on
On outer wing, steering wheel 2 is controlled with a ratio passage, drives outer wing rotary expansion.
Claims (9)
1. it is a kind of folded wing of rotation in the attached wing construction of remote control fixed-wing model of an airplane rotary stacked type, it is characterized in that imitative pinion recovery side
Method, rotation poststack are attached on fuselage, and shared horizontal space is small, the attached wing construction of underslung rotary stacked type.
2. the attached wing construction of remote control fixed-wing model of an airplane rotary stacked type as claimed in claim 1, it is characterised in that described rotation is folded
The attached wing construction of formula includes the inner wing and outer wing being connected with each other with the rotating shaft of steering wheel 2, and inner wing is double-decker.
3. the attached wing construction of remote control fixed-wing model of an airplane rotary stacked type as claimed in claim 2, it is characterised in that described inner wing
Leading edge closing, trailing edge and outer rim leave gap, with remote controller control steering wheel 2 by outer wing screw in in slot.
4. the attached wing construction of remote control fixed-wing model of an airplane rotary stacked type as claimed in claim 2, it is characterised in that described inner wing
It is connected between fuselage by hinge, controls drive to spin upside down with steering wheel 1.
5. the attached wing construction of remote control fixed-wing model of an airplane rotary stacked type as claimed in claim 4, it is characterised in that described steering wheel 1
It is fixed on fuselage, the rotating shaft of steering wheel 1 is fixed on hinge blade-rotating axle sleeve, and blade-rotating axle sleeve is fixed on inner wing.
6. the attached wing construction of remote control fixed-wing model of an airplane rotary stacked type is characterized in that described hinge supplies as claimed in claim 4
Inner wing folds up and down, and fin maximum flip angle in limitation.
7. the attached wing construction of remote control fixed-wing model of an airplane rotary stacked type as claimed in claim 5, it is characterised in that with remote controller control
Steering wheel 1 processed folds inner wing together with the outer wing in slot in screw-in downwardly together, is attached on fuselage.
8. the attached wing construction of remote control fixed-wing model of an airplane rotary stacked type as claimed in claim 5, it is characterised in that when needs take off
When, first with remote controller control steering wheel 1 inner wing together with the outer flapwise both sides in slot in screw-in dig come, it is open and flat after again with shake control
Device controls steering wheel 2 that outer wing is screwed out and stretched out.
9. the attached wing construction of remote control fixed-wing model of an airplane rotary stacked type as claimed in claim 1, it is characterised in that after wing is withdrawn
Without the span, become the shell of aircraft, empennage can also use this method to withdraw, and transverse width be greatly decreased, personal aircraft
This construction can also be used, can travel and park on road as automobile after withdrawing wing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710993572.8A CN107497123A (en) | 2017-10-24 | 2017-10-24 | It is remotely controlled the attached wing construction of fixed-wing model of an airplane rotary stacked type |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710993572.8A CN107497123A (en) | 2017-10-24 | 2017-10-24 | It is remotely controlled the attached wing construction of fixed-wing model of an airplane rotary stacked type |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107497123A true CN107497123A (en) | 2017-12-22 |
Family
ID=60700686
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710993572.8A Withdrawn CN107497123A (en) | 2017-10-24 | 2017-10-24 | It is remotely controlled the attached wing construction of fixed-wing model of an airplane rotary stacked type |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107497123A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110104165A (en) * | 2019-05-14 | 2019-08-09 | 三亚学院 | It is fitted in longitudinal folding fixed wing in vertical take-off and landing drone |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4022403A (en) * | 1976-01-28 | 1977-05-10 | Louis Francois Chiquet | Convertible aircraft |
| US20060264146A1 (en) * | 2005-05-05 | 2006-11-23 | Steve Conrad | Toy airplane with foldable wings and a switch to activate a plane propeller |
| CN102616096A (en) * | 2012-04-24 | 2012-08-01 | 赵辉 | Solar flying automobile with folding wings |
| US20120280080A1 (en) * | 2011-05-03 | 2012-11-08 | Stark Aerospace, Inc. | Folding wing for aircraft |
| CN103129735A (en) * | 2013-03-08 | 2013-06-05 | 北京航空航天大学 | Three-section dual-folding wing |
| CN205707297U (en) * | 2016-04-19 | 2016-11-23 | 牛睿 | Fixed-wing unmanned plane |
-
2017
- 2017-10-24 CN CN201710993572.8A patent/CN107497123A/en not_active Withdrawn
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4022403A (en) * | 1976-01-28 | 1977-05-10 | Louis Francois Chiquet | Convertible aircraft |
| US20060264146A1 (en) * | 2005-05-05 | 2006-11-23 | Steve Conrad | Toy airplane with foldable wings and a switch to activate a plane propeller |
| US20120280080A1 (en) * | 2011-05-03 | 2012-11-08 | Stark Aerospace, Inc. | Folding wing for aircraft |
| CN102616096A (en) * | 2012-04-24 | 2012-08-01 | 赵辉 | Solar flying automobile with folding wings |
| CN103129735A (en) * | 2013-03-08 | 2013-06-05 | 北京航空航天大学 | Three-section dual-folding wing |
| CN205707297U (en) * | 2016-04-19 | 2016-11-23 | 牛睿 | Fixed-wing unmanned plane |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110104165A (en) * | 2019-05-14 | 2019-08-09 | 三亚学院 | It is fitted in longitudinal folding fixed wing in vertical take-off and landing drone |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20171222 |