CN205287615U - Stationary vane model aeroplane and model ship - Google Patents

Stationary vane model aeroplane and model ship Download PDF

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Publication number
CN205287615U
CN205287615U CN201620022478.9U CN201620022478U CN205287615U CN 205287615 U CN205287615 U CN 205287615U CN 201620022478 U CN201620022478 U CN 201620022478U CN 205287615 U CN205287615 U CN 205287615U
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CN
China
Prior art keywords
model
wing
fuselage
aeroplane
ship
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
Application number
CN201620022478.9U
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Chinese (zh)
Inventor
邓庆阳
郭占占
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
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Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
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Priority to CN201620022478.9U priority Critical patent/CN205287615U/en
Application granted granted Critical
Publication of CN205287615U publication Critical patent/CN205287615U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a stationary vane model aeroplane and model ship, including fuselage and wing, through the wing wing root string of a musical instrument and the fuselage axis fastener angle that changes model aeroplane and model ship to and the angle at the upper counterangle of model aeroplane and model ship, reach the lift when improving model aeroplane and model ship and taking off, the effect of relative energy consumption is reduced, and the unusual ability of aircraft automatic correction flight gesture can be strengthened, make flight performance more stable, fuselage and wing regard as the installation material with polypropylene foaming board, reach the purpose of the whole weight of reduction fuselage.

Description

A kind of fixed-wing model plane
Technical field
This utility model relates to a kind of model, particularly relates to a kind of fixed-wing model plane.
Background technology
Common fixed-wing fixed-wing model plane have that flying quality is not good, energy consumption is big, easy stall, and these are all exaggerated fixed-wing model plane manipulation difficulty and the probability that causes model plane surprisingly to be damaged increases.
The utility model discloses a kind of low energy consumption, the fixed-wing model plane that flying quality is stable.
Utility model content
The fixed-wing model plane that the technical problems to be solved in the utility model is to provide a kind of low energy consumption, flying quality is stable.
In order to solve above-mentioned technical problem; the technical solution adopted in the utility model is, a kind of fixed-wing model plane, including fuselage and wing; the wing wing root string of a musical instrument of described fixed-wing model plane and fuselage axis angle are 2 degree, and the described datum level of fixed-wing model plane wing and the angle of horizontal plane are 14 degree.
Above-described fixed-wing model plane, described fuselage and wing using polypropylene expanded plate as installation material.
This utility model has the advantage that
By changing the wing wing root string of a musical instrument and the fuselage axis angle of model plane, reach to improve lift when model plane take off, reduce the effect of relative energy consumption; By the angle at the upper counterangle of model plane, enhance aircraft and automatically revise the ability that flight attitude is abnormal so that flying quality is more stable; Fuselage and wing, using polypropylene expanded plate as installation material, have reached the purpose of the overall weight reducing fuselage.
Accompanying drawing explanation
Below in conjunction with the drawings and specific embodiments, the utility model is described in more detail.
Fig. 1 is front view of the present utility model.
Fig. 2 is top view of the present utility model.
Detailed description of the invention
This utility model embodiment; the structure of a kind of fixed-wing model plane is as depicted in figs. 1 and 2; including fuselage 1 and wing 2, the wing 2 wing root string of a musical instrument of described fixed-wing model plane and fuselage 1 axis angle are 2 degree, and the described datum level of fixed-wing model plane wing 2 and the angle of horizontal plane are 14 degree.
Above-described, described fuselage 1 and wing 2 are using polypropylene expanded plate as installation material.
The above; it is only this utility model preferably detailed description of the invention; but protection domain of the present utility model is not limited thereto; any those familiar with the art is in the technical scope that this utility model discloses; it is equal to replacement according to the technical solution of the utility model and inventive concept thereof or is changed, all should be encompassed within protection domain of the present utility model.

Claims (2)

1. fixed-wing model plane, including fuselage and wing, it is characterised in that the wing wing root string of a musical instrument of described fixed-wing model plane and fuselage axis angle are 2 degree, and the described datum level of fixed-wing model plane wing and the angle of horizontal plane are 14 degree.
2. fixed-wing model plane according to claim 1, it is characterised in that described fuselage and wing are using polypropylene expanded plate as installation material.
CN201620022478.9U 2016-01-12 2016-01-12 Stationary vane model aeroplane and model ship Expired - Fee Related CN205287615U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620022478.9U CN205287615U (en) 2016-01-12 2016-01-12 Stationary vane model aeroplane and model ship

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620022478.9U CN205287615U (en) 2016-01-12 2016-01-12 Stationary vane model aeroplane and model ship

Publications (1)

Publication Number Publication Date
CN205287615U true CN205287615U (en) 2016-06-08

Family

ID=56475638

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620022478.9U Expired - Fee Related CN205287615U (en) 2016-01-12 2016-01-12 Stationary vane model aeroplane and model ship

Country Status (1)

Country Link
CN (1) CN205287615U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107680470A (en) * 2017-11-07 2018-02-09 南昌启扬科技有限公司 Ba Sha wooden aircrafts are used in one kind teaching

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107680470A (en) * 2017-11-07 2018-02-09 南昌启扬科技有限公司 Ba Sha wooden aircrafts are used in one kind teaching
CN107680470B (en) * 2017-11-07 2020-03-27 南昌启扬科技有限公司 Bassa wood aircraft for teaching

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Legal Events

Date Code Title Description
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: 20160608

Termination date: 20180112