CN203540064U - Non-gluing wing deck of airplane model - Google Patents
Non-gluing wing deck of airplane model Download PDFInfo
- Publication number
- CN203540064U CN203540064U CN201320277099.0U CN201320277099U CN203540064U CN 203540064 U CN203540064 U CN 203540064U CN 201320277099 U CN201320277099 U CN 201320277099U CN 203540064 U CN203540064 U CN 203540064U
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- wing
- model
- airplane
- adhesive type
- platform
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- Expired - Lifetime
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Abstract
The utility model relates to a non-gluing wing deck of an airplane model. An airplane body installation surface matching with the shape of an airplane body joint is arranged on one side of the non-gluing wing deck, and the airplane body is directly connected with the airplane body installation surface. left wing and right installation surfaces corresponding to the respective dihedral angles of left and right wings are arranged on the other side of the non-gluing wing deck, wherein the left wing and right installation surfaces are sectioned and respectively pass through the central line of the non-gluing wing deck. Insertion gaps are arranged on the installation portions of the left and right wings corresponding to the non-gluing wing deck, and the left and right wings are installed on the left and right wing installation surfaces on the non-gluing wing deck after insertion installation. The non-gluing wing deck is fixed on the airplane body through fixing rubber bands and wing pressing sheets.
Description
Technical field
The utility model belongs to during model airplane wing is connected with fuselage, and one has accurate location, the accessory of non-gluing quick connection.
Background technology
In universal model airplane activity, fan is children fan wood model plane particularly in analogue formation aircraft especially, often because model airplane wing is connected and will uses glue with each assembling parts of fuselage, the careless slightly injury just having caused children in bonding process, serious until seek medical advice to hospital.Because the universal model airplane activity of above-mentioned reason especially wood model plane activity is difficult to extensively carry out in children.
Summary of the invention
The utility model object is exactly the problem existing for the above-mentioned model of an airplane, designed targetedly the non-adhesive type wing of a model of an airplane being connected with fuselage for model airplane wing platform, make children fan can complete fast and accurately an accurate positioning, the model of an airplane of assembling standard, has significantly expanded in children's model fan and has carried out model scope of activities.
The utility model is realized object by the following method: on a face of the non-adhesive type wing of model of an airplane platform, output a fuselage installed surface consistent with fuselage junction shape, fuselage is directly connected with this installed surface.On another face of the non-adhesive type wing of model of an airplane platform, segmentation is outputed respectively through the non-adhesive type wing of model of an airplane platform center line, the port wing starboard wing installed surface of the each upper counterangle of corresponding port wing starboard wing angle.Port wing starboard wing and the corresponding mounting portion of the non-adhesive type wing of model of an airplane platform are outputed and are referred to insert breach, and port wing starboard wing is arranged on the port wing starboard wing installed surface of the non-adhesive type wing of model of an airplane platform after referring to insert.Use fixing elastic by wing compressing tablet, port wing starboard wing and the non-adhesive type wing of model of an airplane platform to be fixed on fuselage.Because held the upper counterangle angle of port wing starboard wing successfully on the non-adhesive type wing of this model of an airplane platform, so not be used in, remeasure location in installation, save time to realize fast and accurately and install.Simultaneously because the port wing starboard wing installed surface of the non-adhesive type wing of this model of an airplane platform has passed the center line of the non-adhesive type wing of model of an airplane platform, so lengthened the arm of force length of the mounting portion of model of an airplane port wing starboard wing, thus the fastness of the fixing port wing starboard wing of fixing elastic played to effective reinforcement.
Accompanying drawing explanation
The general assembly drawing of Fig. 1 model of an airplane
The non-adhesive type wing of Fig. 2 model of an airplane platform figure
The non-adhesive type wing of Fig. 3 model of an airplane platform scheme of installation
The non-adhesive type wing of the sectionally assembled model of an airplane of Fig. 4 platform figure
The non-adhesive type wing of the sectionally assembled model of an airplane of Fig. 5 platform combination schematic diagram
Number description
1, fuselage
2, starboard wing
3, port wing
4, tailplane
5, vertical tail
6, port wing installed surface
7, starboard wing installed surface
8, fuselage installed surface
9, compressing tablet
10, fixing elastic
11, the non-adhesive type wing of model of an airplane platform
13, the non-adhesive type wing of sectionally assembled model of an airplane platform
14, the non-adhesive type wing of sectionally assembled model of an airplane platform fuselage installed surface
15, the non-adhesive type wing of sectionally assembled model of an airplane platform wing installed surface
embodiment
By accompanying drawing, describe embodiment of the present utility model in detail.First by fuselage installed surface (8), non-model of an airplane adhesive type wing platform (11) is arranged on fuselage (1), after again the finger plug part of port wing (3) starboard wing (2) being referred to insert, be arranged on the port wing installed surface (6) and starboard wing installed surface (7) of the non-adhesive type wing of model of an airplane platform (11), with compressing tablet (9), push down the finger plug part of port wing (3) starboard wing (2), then with fixing elastic (10) non-model of an airplane adhesive type wing platform (11) port wing (3) starboard wing (2) compressing tablet (9) binding is fixed on fuselage (1), such one easy for installation, structure relatively firmly reasonable non-gluing wing completed with being just connected of fuselage.
Claims (2)
1. the non-adhesive type wing of model of an airplane platform, it is characterized in that the port wing installed surface (6) and starboard wing installed surface (7) of the non-adhesive type wing of model of an airplane platform (11), that segmentation is respectively through the center line of the non-adhesive type wing of model of an airplane platform (11), open on (11) faces of the non-adhesive type wing of the model of an airplane platform port wing installed surface (6) and the established angle of having held respectively corresponding port wing (3) starboard wing (2) upper counterangle on starboard wing installed surface (7) successfully.
2. according to the non-adhesive type wing of claim 1 model of an airplane platform, it is characterized in that the non-adhesive type wing of model of an airplane platform (11) can make by more than 2 sections number combinations together, the non-adhesive type wing of sectionally assembled model of an airplane platform (13), the every section of non-adhesive type wing of sectionally assembled model of an airplane platform (13) is at least opened more than one quantity, the non-adhesive type wing of sectionally assembled model of an airplane platform wing installed surface (15) according to the upper counterangle of port wing (3) starboard wing (2).
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201320277099.0U CN203540064U (en) | 2013-05-21 | 2013-05-21 | Non-gluing wing deck of airplane model |
EP13184627.1A EP2805752B1 (en) | 2013-05-21 | 2013-09-16 | A non-adhesive wing connector for aircraft models |
US14/282,528 US9138654B2 (en) | 2013-05-21 | 2014-05-20 | Non-adhesive wing connector for aircraft models |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201320277099.0U CN203540064U (en) | 2013-05-21 | 2013-05-21 | Non-gluing wing deck of airplane model |
Publications (1)
Publication Number | Publication Date |
---|---|
CN203540064U true CN203540064U (en) | 2014-04-16 |
Family
ID=50458235
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201320277099.0U Expired - Lifetime CN203540064U (en) | 2013-05-21 | 2013-05-21 | Non-gluing wing deck of airplane model |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN203540064U (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104174171A (en) * | 2013-05-21 | 2014-12-03 | 李文奇 | Model airplane non-adhesive wing table |
CN106669180A (en) * | 2016-12-27 | 2017-05-17 | 常州大学 | Fixed wing aircraft folded wing device |
CN107757863A (en) * | 2017-09-12 | 2018-03-06 | 江西洪都航空工业集团有限责任公司 | A kind of small aircraft wing body list bandage attachment structure |
-
2013
- 2013-05-21 CN CN201320277099.0U patent/CN203540064U/en not_active Expired - Lifetime
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104174171A (en) * | 2013-05-21 | 2014-12-03 | 李文奇 | Model airplane non-adhesive wing table |
CN104174171B (en) * | 2013-05-21 | 2016-04-20 | 李文奇 | The model of an airplane non-adhesive type wing platform |
CN106669180A (en) * | 2016-12-27 | 2017-05-17 | 常州大学 | Fixed wing aircraft folded wing device |
CN106669180B (en) * | 2016-12-27 | 2019-12-06 | 常州大学 | Flap aligning device of fixed-wing aircraft |
CN107757863A (en) * | 2017-09-12 | 2018-03-06 | 江西洪都航空工业集团有限责任公司 | A kind of small aircraft wing body list bandage attachment structure |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
AV01 | Patent right actively abandoned |
Granted publication date: 20140416 Effective date of abandoning: 20160420 |
|
C25 | Abandonment of patent right or utility model to avoid double patenting |