SU19465A1 - A device for shifting the wheel chassis of a seaplane - Google Patents
A device for shifting the wheel chassis of a seaplaneInfo
- Publication number
- SU19465A1 SU19465A1 SU65820A SU65820A SU19465A1 SU 19465 A1 SU19465 A1 SU 19465A1 SU 65820 A SU65820 A SU 65820A SU 65820 A SU65820 A SU 65820A SU 19465 A1 SU19465 A1 SU 19465A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- seaplane
- shifting
- chassis
- wheel chassis
- cylinder
- Prior art date
Links
Landscapes
- Motorcycle And Bicycle Frame (AREA)
Description
Изобретение касаетс устройства дл перестановки колесного шасси гидросамолета и имеет целью создание возможности посадки гидросамолетов на сухопутные аэродромы.The invention relates to a device for rearranging the wheeled chassis of a seaplane and aims at creating the possibility of landing seaplanes on land aerodromes.
На предлагаемом чертеже фиг. 1 изображает схематический вид на устройство спереди; фиг. 2-то же, вид сбоку.In the proposed drawing of FIG. 1 shows a schematic view of the device from the front; FIG. 2 is the same side view.
Конструкци устройства состоит из находШцейс внутри поплавка 7 рамы колесного шасси. Шасси 1 на своей оси 5 имеют колеса, каковые вход т в поплавки 7 шасси своим концом 6 к штоку поршн цилиндра 3 и вращаютс вокруг оси 2 рамы.The design of the device consists of a located inside the float 7 of the frame of the wheeled chassis. Chassis 1 on its axis 5 have wheels, which enter the floats 7 of the chassis with their end 6 to the piston rod of the cylinder 3 and rotate around the axis 2 of the frame.
Внутри рамы находитс качающийс вокруг пустотелой оси 4 цилиндр 3. Подъем и опускание колес производитс поступающим через пустотелую ось 4Inside the frame there is a cylinder 3 swinging around the hollow axis 4. The wheels are raised and lowered coming through the hollow axis 4
I в правую или левую сторону цилиндра о I сжатым воздухом, вследствие чего происходит перемещение поршн цилиндра I и св занного со штоком поршн шарнира 6 шасси 1. I to the right or left side of the cylinder O I with compressed air, as a result of which the piston of the cylinder I and the chassis 1 hinge 6 connected to the piston rod move.
IПредмет патент а.I Subject Patent a.
Устройство дл перестановки колесного I шасси гидросамолета, характеризующеес I тем, что колеса шасси внутри поплавков креп тс к раме 1, вращающейс вокруг оси 2 при помощи действи на другой конец этой рамы поршневого штока цилиндра 3, работающего сжатым воздухом, подводимым по специальной магистрали в правую или левую часть цилиндра в зависимости от направлени движени поршн через пустотелую ось 4, вокруг которой цилиндр может вращатьс .A device for rearranging the wheeled I chassis of a seaplane, characterized by the fact that the wheels of the chassis inside the floats are attached to the frame 1 rotating around axis 2 by acting on the other end of this frame of the piston rod of the cylinder 3 working with compressed air supplied through a special line to the right or the left side of the cylinder depending on the direction of movement of the piston through the hollow shaft 4 around which the cylinder can rotate.
фигfig
,.,
.i J v5frJ X7 75 y.i J v5frJ X7 75 y
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU65820A SU19465A1 (en) | 1930-04-01 | 1930-04-01 | A device for shifting the wheel chassis of a seaplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU65820A SU19465A1 (en) | 1930-04-01 | 1930-04-01 | A device for shifting the wheel chassis of a seaplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU19465A1 true SU19465A1 (en) | 1931-02-28 |
Family
ID=48339022
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU65820A SU19465A1 (en) | 1930-04-01 | 1930-04-01 | A device for shifting the wheel chassis of a seaplane |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU19465A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2364549C2 (en) * | 2007-10-19 | 2009-08-20 | Закрытое Акционерное Общество Научно-Производственное Объединение "Авиа Лтд" (Зао Нпо "Авиа Лтд") | Aircraft landing gear lifting mechanism |
-
1930
- 1930-04-01 SU SU65820A patent/SU19465A1/en active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2364549C2 (en) * | 2007-10-19 | 2009-08-20 | Закрытое Акционерное Общество Научно-Производственное Объединение "Авиа Лтд" (Зао Нпо "Авиа Лтд") | Aircraft landing gear lifting mechanism |
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