CN107754342A - The Novel noise-reduction model of an airplane - Google Patents
The Novel noise-reduction model of an airplane Download PDFInfo
- Publication number
- CN107754342A CN107754342A CN201610675792.1A CN201610675792A CN107754342A CN 107754342 A CN107754342 A CN 107754342A CN 201610675792 A CN201610675792 A CN 201610675792A CN 107754342 A CN107754342 A CN 107754342A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- flank
- airplane
- reduction model
- undercarriage
- 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
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
- A63H27/02—Model aircraft
Landscapes
- Toys (AREA)
Abstract
The invention discloses a kind of Novel noise-reduction model of an airplane, including fuselage(4), vertical tail(5)Installed in fuselage(4)End, tailplane(6)Installed in vertical tail(5)Both sides, flank(7)Installed in fuselage(4), undercarriage(3)Installed in fuselage(4)On the downside of leading portion, engine(1)Installed in fuselage(4)Front end, propeller(2)On head, undercarriage(3)Wheel is installed below(8), bloop(9)Installed in flank(7)It is internal.The beneficial effects of the invention are as follows:The setting of rubber wheels is added, the vibrations triggered due to Uneven road can be mitigated, jolted.The vibrations that flank is sent when the design of snubber block can reduce flight.The noise that wing is sent when the design of bloop can reduce aircraft flight, environmental protection.
Description
Technical field
The present invention relates to aircraft field, more particularly, to a kind of Novel noise-reduction model of an airplane.
Background technology
Aircraft refers to that the power set with a tool or more tool engines produce the thrust advanced or pulling force, by consolidating for fuselage
Determine wing and produce lift, in the airborne vehicle for overweighting air of endoatmosphere flight.Aircraft is a kind of most common fixed-wing aviation
Device.The engine type used according to it can be divided into jet airplane and propeller aeroplane again.
The content of the invention
The present invention provides a kind of Novel noise-reduction model of an airplane, including fuselage, vertical end for this to solve present problems
The wing is arranged on tail cone, and tailplane is arranged on vertical tail both sides, and flank is arranged on fuselage, before undercarriage is arranged on fuselage
Section downside, engine are arranged on front fuselage, and propeller is arranged on head, and wheel, bloop installation is installed below in undercarriage
Inside flank.
Preferably, the wheel outer surface is quality of rubber materials.
The beneficial effects of the invention are as follows:
The setting of rubber wheels is added, the vibrations triggered due to Uneven road can be mitigated, jolted.The design of snubber block can subtract
The vibrations that flank is sent during few flight.The noise that wing is sent when the design of bloop can reduce aircraft flight, environmental protection.
Brief description of the drawings
Examples of the present invention will be described by way of reference to the accompanying drawings, wherein:
Fig. 1 is the front view of the present invention.
Embodiment
All features disclosed in this specification, or disclosed all methods or during the step of, except mutually exclusive
Feature and/or step beyond, can combine in any way.
Any feature disclosed in this specification, unless specifically stated otherwise, can be equivalent by other or with similar purpose
Alternative features are replaced.I.e., unless specifically stated otherwise, each feature is an example in a series of equivalent or similar characteristics
.
As shown in Fig. 1 a kind of Novel noise-reduction model of an airplane, including fuselage, vertical tail are arranged on tail cone, water
The horizontal tail wing is arranged on vertical tail both sides, and flank is arranged on fuselage, and undercarriage is arranged on the downside of nosing, and engine is arranged on
Front fuselage, propeller are arranged on head, and wheel is installed below in undercarriage, and bloop is arranged on inside flank.
Preferably, the wheel outer surface is quality of rubber materials.
The beneficial effects of the invention are as follows:
The setting of rubber wheels is added, the vibrations triggered due to Uneven road can be mitigated, jolted.The design of snubber block can subtract
The vibrations that flank is sent during few flight.The noise that wing is sent when the design of bloop can reduce aircraft flight, environmental protection.
The invention is not limited in foregoing embodiment.The present invention, which expands to, any in this manual to be disclosed
New feature or any new combination, and disclose any new method or process the step of or any new combination.
Claims (2)
1. a kind of Novel noise-reduction model of an airplane, it is characterised in that including fuselage(4), vertical tail(5)Installed in fuselage(4)End
End, tailplane(6)Installed in vertical tail(5)Both sides, flank(7)Installed in fuselage(4), undercarriage(3)Installed in fuselage
(4)On the downside of leading portion, engine(1)Installed in fuselage(4)Front end, propeller(2)On head, undercarriage(3)Pacify below
Fill wheel(8), bloop(9)Installed in flank(7)It is internal.
2. the Novel noise-reduction model of an airplane according to claim 1, it is characterized in that:The wheel(8)Outer surface is rubber
Material.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610675792.1A CN107754342A (en) | 2016-08-17 | 2016-08-17 | The Novel noise-reduction model of an airplane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610675792.1A CN107754342A (en) | 2016-08-17 | 2016-08-17 | The Novel noise-reduction model of an airplane |
Publications (1)
Publication Number | Publication Date |
---|---|
CN107754342A true CN107754342A (en) | 2018-03-06 |
Family
ID=61259851
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201610675792.1A Pending CN107754342A (en) | 2016-08-17 | 2016-08-17 | The Novel noise-reduction model of an airplane |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN107754342A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108721912A (en) * | 2018-08-13 | 2018-11-02 | 江阴市翔诺电子科技有限公司 | A kind of model of an airplane |
-
2016
- 2016-08-17 CN CN201610675792.1A patent/CN107754342A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108721912A (en) * | 2018-08-13 | 2018-11-02 | 江阴市翔诺电子科技有限公司 | A kind of model of an airplane |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180306 |
|
WD01 | Invention patent application deemed withdrawn after publication |