CN104554714A - Splitting type undercarriage for helicopter model - Google Patents
Splitting type undercarriage for helicopter model Download PDFInfo
- Publication number
- CN104554714A CN104554714A CN201410730874.2A CN201410730874A CN104554714A CN 104554714 A CN104554714 A CN 104554714A CN 201410730874 A CN201410730874 A CN 201410730874A CN 104554714 A CN104554714 A CN 104554714A
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- China
- Prior art keywords
- helicopter
- support
- strut bar
- coupling link
- bracket
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Abstract
The invention relates to a splitting type undercarriage for a helicopter model. The splitting type undercarriage comprises a first bracket and a second bracket, wherein the bottom ends of the first bracket and the second bracket are fixedly connected with a connection ring; the connection ring is provided with a supporting rod; the supporting rod is in sleeve joint with the connection ring; the connection ring is provided with a fixing device for fixing the supporting rod in the connection ring; the first bracket and the second bracket are in bolt connection with a connection plate which is fixedly connected with a helicopter fuselage; a floating plate for promoting buoyancy force when a helicopter falls into the water is arranged in the connection plate; alarming lamps are fixedly connected with the two ends of the supporting rod and the supporting rod is internally provided with a power supply device for supplying power to the alarming lamps; and a pressure switch for controlling the alarming lamps to be turned on and off is arranged at the bottom of the supporting rod. The splitting type undercarriage for the helicopter model is provided with the connection plate with the floating plate and the automatic alarming lamps, so that the safety of the helicopter model is greatly improved.
Description
Technical field
The present invention relates to a kind of divided under carriage for helicopter model.
Background technology
Common helicopter model landing gear structure is simple, not to the passive connecting panel of fuselage, comparatively large to the damage of fuselage when helicopter rises and falls, and once helicopter drops in water, cannot provide enough buoyancy to helicopter, safety is poor; Warning light on common helicopter mostly is Non-follow control, cannot to rise and fall automatic switch along with helicopter, very inconvenient.
Summary of the invention
The technical problem to be solved in the present invention is: for solving above-mentioned Problems existing, provides a kind of divided under carriage for helicopter model, solves common alighting gear poor to helicopter protectiveness, cannot split and not have the problem of automatic alarm lamp.
The technical solution adopted for the present invention to solve the technical problems is: a kind of divided under carriage for helicopter model, comprise the first support and the second support, first support and the second support bottom are fixedly connected with coupling link, coupling link is provided with strut bar, strut bar and coupling link are socketed, coupling link offers the anchor fitting for strut bar being fixed on coupling link inside, first support is connected with the connecting panel for being fixedly connected with helicopter fuselage with the second bracket bolt, connecting panel inside is provided with falls in water for helicopter the kickboard promoting buoyancy, strut bar two ends are fixedly connected with Warning light, strut bar inside is provided with the supply unit of powering to Warning light, the pressure switch of closing for controlling Warning light is provided with bottom strut bar.
Further, connecting panel offers the through hole for alleviating connecting panel weight.
Further, coupling link inwall is provided with shock-absorbing protecting cover.
The invention has the beneficial effects as follows, of the present inventionly on the divided under carriage of helicopter model, be provided with the connecting panel and automatic alarm lamp with kickboard, greatly promote the safety of helicopter model.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the present invention is further described.
Fig. 1 is decomposition texture schematic diagram of the present invention.
Fig. 2 is structural representation of the present invention.
1. first supports, 2. the second support, 3. coupling link, 4. strut bar, 5. anchor fitting, 6. connecting panel, 7. Warning light, 8. through hole in figure.
Detailed description of the invention
In conjunction with the accompanying drawings, the present invention is further detailed explanation.These accompanying drawings are the schematic diagram of simplification, only basic structure of the present invention are described in a schematic way, and therefore it only shows the formation relevant with the present invention.
A kind of divided under carriage for helicopter model as depicted in figs. 1 and 2, comprise the first support 1 and the second support 2, first support 1 and the second support 2 bottom are fixedly connected with coupling link 3, coupling link 3 is provided with strut bar 4, strut bar 4 and coupling link 3 are socketed, coupling link 3 offers the anchor fitting 5 for strut bar 4 being fixed on coupling link 3 inside, first support 1 is connected with the connecting panel 6 for being fixedly connected with helicopter fuselage with the second support 2 bolt, connecting panel 6 inside is provided with falls in water for helicopter the kickboard promoting buoyancy, strut bar 4 two ends are fixedly connected with Warning light 7, strut bar 4 inside is provided with the supply unit of powering to Warning light 7, the pressure switch of closing for controlling Warning light 7 is provided with bottom strut bar 4, further, connecting panel 6 offers the through hole 8 for alleviating connecting panel 6 weight, further, coupling link 3 inwall is provided with shock-absorbing protecting cover, of the present inventionly on the divided under carriage of helicopter model, be provided with the connecting panel 6 and automatic alarm lamp 7 with kickboard, greatly promote the safety of helicopter model.
With above-mentioned according to desirable embodiment of the present invention for enlightenment, by above-mentioned description, relevant staff in the scope not departing from this invention technological thought, can carry out various change and amendment completely.The technical scope of this invention is not limited to the content on specification sheets, must determine its technical scope according to right.
Claims (3)
1. the divided under carriage for helicopter model, comprise the first support (1) and the second support (1), it is characterized in that: described the first support (1) and the second support (2) bottom are fixedly connected with coupling link (3), described coupling link (3) is provided with strut bar (4), described strut bar (4) and coupling link (3) are socketed, described coupling link (3) offer for strut bar (4) being fixed on the inner anchor fitting (5) of coupling link (3), described the first support (2) and the second support (3) bolt are connected with the connecting panel (6) for being fixedly connected with helicopter fuselage, described connecting panel (6) inside is provided with falls in water for helicopter the kickboard promoting buoyancy, described strut bar (4) two ends are fixedly connected with Warning light (7), strut bar (4) inside is provided with the supply unit of powering to Warning light (7), strut bar (4) bottom is provided with the pressure switch of closing for controlling Warning light (7).
2. the divided under carriage for helicopter model according to claim 1, is characterized in that: described connecting panel (6) offers the through hole (8) for alleviating connecting panel (6) weight.
3. the divided under carriage for helicopter model according to claim 1, is characterized in that: described coupling link (3) inwall is provided with shock-absorbing protecting cover.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410730874.2A CN104554714A (en) | 2014-12-05 | 2014-12-05 | Splitting type undercarriage for helicopter model |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410730874.2A CN104554714A (en) | 2014-12-05 | 2014-12-05 | Splitting type undercarriage for helicopter model |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104554714A true CN104554714A (en) | 2015-04-29 |
Family
ID=53071993
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410730874.2A Pending CN104554714A (en) | 2014-12-05 | 2014-12-05 | Splitting type undercarriage for helicopter model |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104554714A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107323665A (en) * | 2017-07-06 | 2017-11-07 | 上海复亚通信科技有限公司 | It is easy to the unmanned plane of salvage |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB294319A (en) * | 1927-05-17 | 1928-07-26 | Bert Hinkler | An improved undercarriage for aircraft |
| US5224669A (en) * | 1991-05-06 | 1993-07-06 | Aerospatiale Societe Nationale Industrielle | Landing gear for an aerodyne, with arches in composite material |
| CN1439578A (en) * | 2003-03-07 | 2003-09-03 | 孙学年 | Multifunctional airplane and application thereof |
| CN2687008Y (en) * | 2004-03-17 | 2005-03-23 | 李晓阳 | General float for hydroplane model |
| CN201457735U (en) * | 2009-06-29 | 2010-05-12 | 佛山市安尔康姆航拍科技有限公司 | Wheel-ski mixing type undercarriage for unmanned aerial vehicle |
| CN203461102U (en) * | 2013-09-13 | 2014-03-05 | 重庆金泰航空工业有限公司 | Undercarriage installation structure of agricultural unmanned aerial vehicle |
| CN104002961A (en) * | 2014-06-13 | 2014-08-27 | 韩世宇 | Miniature helicopter undercarriage |
-
2014
- 2014-12-05 CN CN201410730874.2A patent/CN104554714A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB294319A (en) * | 1927-05-17 | 1928-07-26 | Bert Hinkler | An improved undercarriage for aircraft |
| US5224669A (en) * | 1991-05-06 | 1993-07-06 | Aerospatiale Societe Nationale Industrielle | Landing gear for an aerodyne, with arches in composite material |
| CN1439578A (en) * | 2003-03-07 | 2003-09-03 | 孙学年 | Multifunctional airplane and application thereof |
| CN2687008Y (en) * | 2004-03-17 | 2005-03-23 | 李晓阳 | General float for hydroplane model |
| CN201457735U (en) * | 2009-06-29 | 2010-05-12 | 佛山市安尔康姆航拍科技有限公司 | Wheel-ski mixing type undercarriage for unmanned aerial vehicle |
| CN203461102U (en) * | 2013-09-13 | 2014-03-05 | 重庆金泰航空工业有限公司 | Undercarriage installation structure of agricultural unmanned aerial vehicle |
| CN104002961A (en) * | 2014-06-13 | 2014-08-27 | 韩世宇 | Miniature helicopter undercarriage |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107323665A (en) * | 2017-07-06 | 2017-11-07 | 上海复亚通信科技有限公司 | It is easy to the unmanned plane of salvage |
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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: 20150429 |