CN208746229U - A kind of Novel model airplane aircraft - Google Patents

A kind of Novel model airplane aircraft Download PDF

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Publication number
CN208746229U
CN208746229U CN201821238742.8U CN201821238742U CN208746229U CN 208746229 U CN208746229 U CN 208746229U CN 201821238742 U CN201821238742 U CN 201821238742U CN 208746229 U CN208746229 U CN 208746229U
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CN
China
Prior art keywords
head
fuselage
fixed link
fixing groove
forebody
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
CN201821238742.8U
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Chinese (zh)
Inventor
郭志兴
苏文乐
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
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Filing date
Publication date
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Priority to CN201821238742.8U priority Critical patent/CN208746229U/en
Application granted granted Critical
Publication of CN208746229U publication Critical patent/CN208746229U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model provides a kind of Novel model airplane aircraft, the head of model plane is flexibly connected with fuselage, head is equipped with head fixed link, fuselage is equipped with head fixing groove corresponding with head fixed link position, head fixed link is mounted in head fixing groove, and spring is equipped between head fixed link and head fixing groove;Head two sides are additionally provided with auxiliary stopper bar, are connected with the auxiliary stopper slot being arranged on fuselage.The forebody and rear body of the utility model are detachable, and recoverability is strong, save the cost;In addition, being equipped with spring between head and forebody, the probability that head is damaged is reduced.

Description

A kind of Novel model airplane aircraft
Technical field
The utility model belongs to model plane technical field, and in particular to a kind of Novel model airplane aircraft.
Background technique
Aeromodelling airplane usually reduces actual airplane by a certain percentage, is fabricated to the lesser model of an airplane.Aeromodelling airplane master It is used to popularize popular science knowledge, in addition aeromodelling airplane is also largely used to the simulated experiment that airplane design produces early period.Aeromodelling airplane Generally as manned aircraft, mainly by including wing, empennage, fuselage, undercarriage, engine and control system etc. six Point.
Model plane in use, often due to misoperation, cause aeromodelling airplane to be easy to hit ground, due to speed Fastly, impact force is big, often hits curved by the head of aeromodelling airplane or even severs.Prevent although having just install additional before the handpiece in the prior art The technology of collision block, but the anticollison block installed additional in front of head is affected to the globality of aircraft, streamline and center of gravity, causes to navigate The manipulation difficulty of mould aircraft becomes larger, and flying speed reduces, and increases the probability that aeromodelling airplane falls.
Utility model content
The utility model provides a kind of Novel model airplane aircraft, is to solve the problems, such as that aeromodelling airplane head is easy to break. For this purpose, the utility model adopts the following technical solution:
A kind of Novel model airplane aircraft, the aeromodelling airplane include head, fuselage, wing, vertical tail, tailplane, spiral shell Rotation paddle and undercarriage, the head of the model plane are flexibly connected with fuselage, and head is equipped with head fixed link, and fuselage is equipped with and machine The corresponding head fixing groove in head fixed link position, head fixed link are mounted in head fixing groove, and head fixed link and head are solid Determine to be equipped with spring between slot;Head two sides are additionally provided with auxiliary stopper bar, are connected with the auxiliary stopper slot being arranged on fuselage.
Further, the fuselage is divided into forebody and rear body, and the wing of model plane is fixed on rear body, the preceding machine It is equipped with fuselage fixed link with it, the corresponding position of rear body is equipped with fuselage fixing groove, and head fixed link is mounted on fuselage and fixes It is fixedly connected in slot and using rivet.
Further, the top of the fuselage fixing groove is equipped with the location hole of rectangle, and location hole is connected with fuselage fixing groove It is logical;Head fixed link has fluting in the corresponding position with location hole, and positioning hole is equipped with for fixing forebody and rear body Locating piece.
Further, the head fixed link and fuselage fixing groove are multiple.
The utility model has the beneficial effects that: forebody and rear body are detachable, broken in the forebody of aeromodelling airplane After, only needing to change forebody can be used continuously, and recoverability is strong, save the cost;In addition, being equipped between head and forebody Spring plays certain buffer function when head hits ground, reduces the probability that head is damaged.
Detailed description of the invention
Fig. 1 is the schematic perspective view of the utility model;
Fig. 2 is the structural front view of the utility model;
Fig. 3 is the structural side view of the utility model;
Fig. 4 is the structural schematic diagram of the utility model head;
Fig. 5 is the partial enlarged view in the portion I in Fig. 3;
In figure: 1- head, 2- fuselage, 201- forebody, 202- rear body, 3- wing, 4- vertical tail, the horizontal tail of 5- The wing, 6- propeller, 7- undercarriage, 8- head fixed link, 9- head fixing groove, 10- spring, 11- auxiliary stopper bar, 12- auxiliary Limiting slot, 13- fuselage fixed link, 14- fuselage fixing groove, 15- locating piece, 16- location hole.
Specific embodiment
The utility model is described in further detail with reference to the accompanying drawing:
As shown in Figures 1 to 5, a kind of Novel model airplane aircraft, the aeromodelling airplane include head 1, fuselage 2, wing 3, hang down Straight tail 4, tailplane 5, propeller 6 and undercarriage 7, fuselage 2 include forebody 201 and rear body 202.Aeromodelling airplane Wing 3 is fixed on rear body 202, and the fuselage fixed link 13 there are two rectangle is set on the forebody 201, rear body 202 Corresponding position is equipped with the fuselage fixing groove 14 of rectangle, and the top of fuselage fixing groove 14 is equipped with the positioning of the vertical fuselage 2 of rectangle Hole 16, location hole 16 are connected with fuselage fixing groove 14;There is fluting in the corresponding position of head fixed link 13 and location hole 16, fixed Position is equipped in hole 16 for fixing 202 locating piece 15 of forebody 201 and rear body.
The head 1 of aeromodelling airplane is flexibly connected with forebody 201, and head 1 is equipped with the head fixed link 8 of rectangle, preceding machine Body 201 is equipped with head fixing groove 9 corresponding with 8 position of head fixed link, and head fixed link 8 is mounted in head fixing groove 9, Spring 10 is equipped between head fixed link 8 and head fixing groove 9;1 two sides of head are additionally provided with auxiliary stopper bar 11, with forebody The auxiliary stopper slot 12 being arranged on 201 is connected.
The working principle of the utility model is as follows:
It is flexibly connected between head 1 and forebody 201 by piston cylinder operator, and spring 10 is set in-between, so that When hitting ground, head 1 is moved along auxiliary stopper slot 12 to the inside the head 1 of model plane, and spring 10 is compressed, and spring can 10 To play certain buffer function, the risk that head 1 is damaged is reduced.
In addition, according to statistics, the probability highest that 201 position of forebody of aeromodelling airplane is damaged, therefore, the utility model Middle forebody 201 and rear body 202 are flexibly connected using card slot type, after forebody 201 is broken, only need to change forebody 201 aeromodelling airplanes can restore to use.

Claims (4)

1. a kind of Novel model airplane aircraft, the aeromodelling airplane includes head (1), fuselage (2), wing (3), vertical tail (4), water The horizontal tail wing (5), propeller (6) and undercarriage (7), which is characterized in that the head (1) of the model plane is flexibly connected with fuselage (2), Head (1) is equipped with head fixed link (8), and fuselage (2) is equipped with head fixing groove corresponding with head fixed link (8) position (9), head fixed link (8) is mounted in head fixing groove (9), and bullet is equipped between head fixed link (8) and head fixing groove (9) Spring (10);Head (1) two sides are additionally provided with auxiliary stopper bar (11), are connected with the auxiliary stopper slot (12) being arranged on fuselage (2).
2. a kind of Novel model airplane aircraft according to claim 1, which is characterized in that the fuselage (2) is divided into forebody (201) it is fixed on rear body (202) with rear body (202), the wing (3) of model plane, the forebody (201) is equipped with fuselage The corresponding position of fixed link (13), rear body (202) is equipped with fuselage fixing groove (14), and head fixed link (8) is mounted on fuselage It is fixedly connected in fixing groove (14) and using rivet.
3. a kind of Novel model airplane aircraft according to claim 2, which is characterized in that the top of the fuselage fixing groove (14) Location hole (16) equipped with rectangle, location hole (16) are connected with fuselage fixing groove (14);Head fixed link (8) with location hole (16) corresponding position is equipped with fluting, is equipped in location hole (16) for fixing determining for forebody (201) and rear body (202) Position block (15).
4. a kind of Novel model airplane aircraft according to claim 1, which is characterized in that the head fixed link (8) and fuselage Fixing groove (14) is multiple.
CN201821238742.8U 2018-08-02 2018-08-02 A kind of Novel model airplane aircraft Expired - Fee Related CN208746229U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821238742.8U CN208746229U (en) 2018-08-02 2018-08-02 A kind of Novel model airplane aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821238742.8U CN208746229U (en) 2018-08-02 2018-08-02 A kind of Novel model airplane aircraft

Publications (1)

Publication Number Publication Date
CN208746229U true CN208746229U (en) 2019-04-16

Family

ID=66058598

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821238742.8U Expired - Fee Related CN208746229U (en) 2018-08-02 2018-08-02 A kind of Novel model airplane aircraft

Country Status (1)

Country Link
CN (1) CN208746229U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111806683A (en) * 2020-06-04 2020-10-23 仿翼(北京)科技有限公司 Aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111806683A (en) * 2020-06-04 2020-10-23 仿翼(北京)科技有限公司 Aircraft
CN111806683B (en) * 2020-06-04 2022-06-14 仿翼(北京)科技有限公司 Aircraft

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20190416

Termination date: 20210802

CF01 Termination of patent right due to non-payment of annual fee