CN104083876A - Rear vertical tail used for toy plane - Google Patents
Rear vertical tail used for toy plane Download PDFInfo
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- CN104083876A CN104083876A CN201410361300.2A CN201410361300A CN104083876A CN 104083876 A CN104083876 A CN 104083876A CN 201410361300 A CN201410361300 A CN 201410361300A CN 104083876 A CN104083876 A CN 104083876A
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- China
- Prior art keywords
- support
- rear vertical
- vertical tail
- connecting rod
- plane
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Abstract
The invention relates to a rear vertical tail used for a toy plane. The rear vertical tail comprises a support, two through holes used for reducing the weight of the support are formed in the support, two connecting rods are arranged on the left side of the support, the connecting rods and the side wall of the support are provided with nine connecting holes used for being in threaded connection with an outer decorative sheet, and four threaded holes which correspond to one another and are used for being connected with a plane body are formed in the connecting rods. The rear vertical tail used for the toy plane is provided with the connecting holes for being connected with the decorative sheet and the threaded holes for being connected with the plane body, so that playability of the plane and the freedom degree of modification are enhanced greatly.
Description
Technical field
The present invention relates to a kind of rear vertical tail for toy airplane.
Background technology
After common toy airplane, empennage mostly is and aircraft integrative-structure, causes toy airplane manufacturing cost high, and rear vertical tail cannot be changed, and playability is low, and cannot be according to the style pattern of empennage decorative panel after user preferences self-changeable, and the free degree is very poor.
Summary of the invention
The technical problem to be solved in the present invention is: for solving the problem of above-mentioned existence, provide a kind of rear vertical tail for toy airplane, solve conventional airplane and can play the poor and low problem of the repacking free degree.
The technical solution adopted for the present invention to solve the technical problems is: a kind of rear vertical tail for toy airplane, comprise support, on support, offer two for reducing the through hole of weight support frame, support left side has two connecting rods, connecting rod with on rack side wall, offer nine for the connecting hole of the balustrade exterior panelling that is threaded, on connecting rod, offer four corresponding screws that are connected with fuselage that are useful on.
Support is hollow structure support.
Connecting rod is hollow structure connecting rod.
The invention has the beneficial effects as follows, on the rear vertical tail for toy airplane of the present invention, be provided with the connecting hole and the screw being connected with fuselage that connect decorative panel, greatly strengthen playability and the repacking free degree of aircraft.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the present invention is further described.
Fig. 1 is structural representation of the present invention.
Fig. 2 is the structure enlarged diagram of connecting rod.
1. supports in figure, 2. through hole, 3. connecting rod, 4. connecting hole, 5. screw.
The specific embodiment
In conjunction with the accompanying drawings, the present invention is further detailed explanation.These accompanying drawings are the schematic diagram of simplification, basic structure of the present invention is only described in a schematic way, so it only show the formation relevant with the present invention.
A kind of rear vertical tail for toy airplane as depicted in figs. 1 and 2, comprise support 1, on support 1, offer two for reducing the through hole 2 of weight support frame, support 1 left side has two connecting rods 3, connecting rod 3 with on support 1 sidewall, offer nine for the connecting hole 4 of the balustrade exterior panelling that is threaded, on connecting rod 3, offer four corresponding screws 5 that are connected with fuselage that are useful on.
Support 1 is hollow structure support.
Connecting rod 3 is hollow structure connecting rod.
The above-mentioned foundation desirable embodiment of the present invention of take is enlightenment, and by above-mentioned description, relevant staff can, within not departing from the scope of this invention technological thought, carry out various change and modification completely.The technical scope of this invention is not limited to the content on description, must determine its technical scope according to claim scope.
Claims (3)
1. the rear vertical tail for toy airplane, comprise support (1), it is characterized in that: on described support (1), offer two for reducing the through hole (2) of support (1) weight, support (1) left side has two connecting rods (3), described connecting rod (3) offers nine connecting holes for the balustrade exterior panelling that is threaded (4) with on support (1) sidewall, offers four corresponding screws (5) that are connected with fuselage that are useful on described connecting rod (3).
2. the rear vertical tail for toy airplane according to claim 1, is characterized in that: described support (1) is hollow structure support.
3. the rear vertical tail for toy airplane according to claim 1, is characterized in that: described connecting rod (3) is hollow structure connecting rod.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410361300.2A CN104083876A (en) | 2014-07-28 | 2014-07-28 | Rear vertical tail used for toy plane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410361300.2A CN104083876A (en) | 2014-07-28 | 2014-07-28 | Rear vertical tail used for toy plane |
Publications (1)
Publication Number | Publication Date |
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CN104083876A true CN104083876A (en) | 2014-10-08 |
Family
ID=51631695
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201410361300.2A Pending CN104083876A (en) | 2014-07-28 | 2014-07-28 | Rear vertical tail used for toy plane |
Country Status (1)
Country | Link |
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CN (1) | CN104083876A (en) |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2030879A (en) * | 1978-10-05 | 1980-04-16 | Walton J | A toy aircraft |
US5525087A (en) * | 1993-09-16 | 1996-06-11 | Chin-Lin; Hsu | Toy aeroplane |
DE19827392A1 (en) * | 1998-06-19 | 1999-12-23 | Uli Streich | Model air-worthy helicopter with drive mechanism |
CN2848314Y (en) * | 2005-08-12 | 2006-12-20 | 罗之洪 | Oil driven toy helicopter |
CN2889423Y (en) * | 2005-11-30 | 2007-04-18 | 梁钟铭 | Tail structure of toy aircraft |
US20070178798A1 (en) * | 2006-01-27 | 2007-08-02 | Aling Lai | Model helicopter |
CN201073553Y (en) * | 2007-07-18 | 2008-06-18 | 杜大森 | Tail transmission structure improvement of toy helicopter |
-
2014
- 2014-07-28 CN CN201410361300.2A patent/CN104083876A/en active Pending
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2030879A (en) * | 1978-10-05 | 1980-04-16 | Walton J | A toy aircraft |
US5525087A (en) * | 1993-09-16 | 1996-06-11 | Chin-Lin; Hsu | Toy aeroplane |
DE19827392A1 (en) * | 1998-06-19 | 1999-12-23 | Uli Streich | Model air-worthy helicopter with drive mechanism |
CN2848314Y (en) * | 2005-08-12 | 2006-12-20 | 罗之洪 | Oil driven toy helicopter |
CN2889423Y (en) * | 2005-11-30 | 2007-04-18 | 梁钟铭 | Tail structure of toy aircraft |
US20070178798A1 (en) * | 2006-01-27 | 2007-08-02 | Aling Lai | Model helicopter |
CN201073553Y (en) * | 2007-07-18 | 2008-06-18 | 杜大森 | Tail transmission structure improvement of toy helicopter |
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Legal Events
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C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20141008 |