CN205055437U - Undercarriage system of model aeroplane and model ship aircraft - Google Patents
Undercarriage system of model aeroplane and model ship aircraft Download PDFInfo
- Publication number
- CN205055437U CN205055437U CN201520638924.4U CN201520638924U CN205055437U CN 205055437 U CN205055437 U CN 205055437U CN 201520638924 U CN201520638924 U CN 201520638924U CN 205055437 U CN205055437 U CN 205055437U
- Authority
- CN
- China
- Prior art keywords
- wheel
- model
- support
- shaft
- wheel cover
- 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
Links
Landscapes
- Toys (AREA)
Abstract
The utility model discloses an undercarriage system of model aeroplane and model ship aircraft, including support, shaft, wheel and wheel casing, the support mounting is on fuselage bottom, shaft fixed mounting is on the support bottom, the wheel sets up at the wheel epaxially, the wheel casing movable sleeve is established at the wheel epaxially. This undercarriage system is epaxial through establishing the wheel casing movable sleeve at the wheel, and is epaxial rather than fixing at the wheel for the wheel casing runs into the upon impact at model aeroplane and model ship aircraft descending in -process, and the wheel casing can rotate round the shaft in the twinkling of an eye unconstrainedly, thereby reaches the effect of the power of unloading, avoids the wheel casing to damage.
Description
Technical field
The utility model relates to aeromodelling airplane technical field, particularly relates to a kind of Landing Gear System of aeromodelling airplane.
Background technology
Undercarriage be airborne vehicle bottom for take off landing or ground taxi time support the accessories apparatus of airborne vehicle, wheel cover is normally fixed on undercarriage support with wheel shaft by the Landing Gear System of tradition aeromodelling airplane, because aeromodelling airplane tilts to land because of flight attitude in descent, wheel cover usually directly encounters ground, or run into barrier, wheel cover is generally made up of glass steel material, is easily damaged, and aeromodelling airplane even can be caused to overturn crash.
Summary of the invention
In order to overcome above-mentioned the deficiencies in the prior art, the utility model provides a kind of Landing Gear System of aeromodelling airplane, and it is not changing environmental protection wheel house material, when not increasing cost, reduces the damage of wheel cover and fuselage.
The utility model solves the technical scheme that its technical problem adopts:
A Landing Gear System for aeromodelling airplane, comprises support, wheel shaft, wheel and wheel cover, and described support installing is on fuselage bottom, and described wheel shaft is fixedly mounted on support bottom, and described wheel is arranged on wheel shaft, and described wheel cover is movably set on wheel shaft.
As the improvement of technique scheme, described wheel portions is placed in the cavity of wheel cover, and left and right two sidewalls of described wheel cover all lay respectively at the arranged on left and right sides of wheel through wheel shaft.
As the improvement of technique scheme, described wheel shaft is set to stay bolt, described stay bolt comprises head, not threaded polished rod and is with externally threaded screw rod, and described screw rod is by being fixedly connected with support with nut screw connection, and sidewall and the wheel of described wheel cover are arranged on polished rod.
As the improvement of technique scheme, described polished rod is also provided with limited block in position between the sidewall and wheel of wheel cover.
The beneficial effects of the utility model have:
This Landing Gear System is by being movably set on wheel shaft by wheel cover, instead of being fixed on wheel shaft, when wheel being covered on run into collision in aeromodelling airplane descent, wheel cover can rotate around wheel shaft moment without restrictions, thus reach the effect of the power of unloading, avoid wheel cover to damage.
Accompanying drawing explanation
Below in conjunction with drawings and the specific embodiments, the utility model is described in further detail, wherein:
Fig. 1 is the structural representation of the utility model embodiment;
Fig. 2 is the part-structure schematic diagram of the utility model embodiment.
Detailed description of the invention
See Fig. 1, the Landing Gear System of a kind of aeromodelling airplane of the present utility model, comprise support 1, wheel shaft 2, wheel 3 and wheel cover 4, support 1 is arranged on fuselage bottom, wheel shaft 2 is fixedly mounted on support 1 bottom, wheel 3 is arranged on wheel shaft 2, wheel 3 part is placed in the cavity of wheel cover 4, wheel cover 4 is movably set on wheel shaft 2, a left side for wheel cover 4, right two sidewalls all lay respectively at the left side of wheel 3 through wheel shaft 2, right both sides, when making wheel cover 4 run into collision in aeromodelling airplane descent, wheel cover 4 can rotate around wheel shaft 2 moment without restrictions, thus reach the effect of the power of unloading, avoid the damage of wheel cover 4.
With further reference to Fig. 2, wheel shaft 2 is set to a stay bolt, stay bolt comprises head 21, not threaded polished rod 22 and is with externally threaded screw rod 23, screw rod 23 is by being fixedly connected with support 1 with nut screw connection, the sidewall of wheel cover 4 and wheel 3 are arranged on polished rod 22, and between the sidewall and wheel 3 of wheel cover 4, position be also provided with limited block 5 at polished rod 22, prevent wheel 3 from sliding axially on polished rod 22, also play the effect preventing wheel 3 and the mutual frictional influence of wheel cover 4.
The above, just better embodiment of the present utility model, but the utility model is not limited to above-described embodiment, as long as it reaches technique effect of the present utility model with any same or similar means, all should belong to protection domain of the present utility model.
Claims (4)
1. the Landing Gear System of an aeromodelling airplane, comprise support (1), wheel shaft (2), wheel (3) and wheel cover (4), described support (1) is arranged on fuselage bottom, it is characterized in that: described wheel shaft (2) is fixedly mounted on support (1) bottom, described wheel (3) is arranged on wheel shaft (2), and described wheel cover (4) is movably set on wheel shaft (2).
2. the Landing Gear System of a kind of aeromodelling airplane according to claim 1, it is characterized in that: described wheel (3) part is placed in the cavity of wheel cover (4), left and right two sidewalls of described wheel cover (4) all lay respectively at the arranged on left and right sides of wheel (3) through wheel shaft (2).
3. the Landing Gear System of a kind of aeromodelling airplane according to claim 2, it is characterized in that: described wheel shaft (2) is set to stay bolt, described stay bolt comprises head (21), not threaded polished rod (22) and the externally threaded screw rod of band (23), described screw rod (23) is by being fixedly connected with support (1) with nut screw connection, sidewall and the wheel (3) of described wheel cover (4) are arranged on polished rod (22).
4. the Landing Gear System of a kind of aeromodelling airplane according to claim 3, is characterized in that: described polished rod (22) is positioned at position between the sidewall of wheel cover (4) and wheel (3) and is also provided with limited block (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520638924.4U CN205055437U (en) | 2015-08-21 | 2015-08-21 | Undercarriage system of model aeroplane and model ship aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520638924.4U CN205055437U (en) | 2015-08-21 | 2015-08-21 | Undercarriage system of model aeroplane and model ship aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205055437U true CN205055437U (en) | 2016-03-02 |
Family
ID=55382041
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520638924.4U Expired - Fee Related CN205055437U (en) | 2015-08-21 | 2015-08-21 | Undercarriage system of model aeroplane and model ship aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205055437U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114802721A (en) * | 2022-05-27 | 2022-07-29 | 江西冠一通用飞机有限公司 | Fairing of strut type landing gear and mounting method thereof |
-
2015
- 2015-08-21 CN CN201520638924.4U patent/CN205055437U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114802721A (en) * | 2022-05-27 | 2022-07-29 | 江西冠一通用飞机有限公司 | Fairing of strut type landing gear and mounting method thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104787309A (en) | Landing gear of rotor unmanned aerial vehicle (UAV) | |
| CN106394882B (en) | A kind of chute-type unmanned plane skid jack | |
| KR101822386B1 (en) | Wireless charging system of drone | |
| CN104596729A (en) | Test method for ditching towing tank of fixed-wing airplane model | |
| CN202657252U (en) | Vehicle-mounted flying frame | |
| CN205273843U (en) | Many rotor unmanned aerial vehicle's multi -functional undercarriage | |
| CN101973393A (en) | High-strength cage-type undercarriage of unmanned helicopter | |
| WO2018122842A3 (en) | Universal flying terrain vehicle | |
| CN103963986A (en) | Undercarriage faulty airplane safe landing gear | |
| CN205055437U (en) | Undercarriage system of model aeroplane and model ship aircraft | |
| CN205554569U (en) | Aerospace's undercarriage is exclusively used in | |
| CN204623827U (en) | A kind of rotor wing unmanned aerial vehicle alighting gear | |
| CN207466962U (en) | A kind of rotor wing unmanned aerial vehicle damping undercarriage | |
| CN106586010A (en) | Inspection device based on quadrotor unmanned aerial vehicle | |
| CN203428026U (en) | Small duct-type aircraft | |
| CN205770131U (en) | A kind of light-duty slide type undercarriage | |
| CN203780794U (en) | Lightweight wing tip structure for protecting wing | |
| CN204279927U (en) | There is with elastic ball the rotor craft alighting gear of rotor protected effect | |
| CN204998757U (en) | Undercarriage that topples is prevented to many rotor crafts | |
| CN204473127U (en) | Rear bikini aerial survey fixed-wing unmanned plane tail-pulley device | |
| CN211033000U (en) | Unmanned aerial vehicle with safeguard function | |
| US2696957A (en) | Landing and launching system for aircraft | |
| CN203996879U (en) | A kind of unmanned plane head helps and falls structure | |
| CN203497168U (en) | Front camera bin of unmanned plane | |
| CN104548616A (en) | Remote control aircraft |
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: 20160302 Termination date: 20200821 |