SU134060A1 - Device for remote separation of two elements of an object in flight during aerodynamic research - Google Patents
Device for remote separation of two elements of an object in flight during aerodynamic researchInfo
- Publication number
- SU134060A1 SU134060A1 SU657409A SU657409A SU134060A1 SU 134060 A1 SU134060 A1 SU 134060A1 SU 657409 A SU657409 A SU 657409A SU 657409 A SU657409 A SU 657409A SU 134060 A1 SU134060 A1 SU 134060A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- elements
- flight during
- remote separation
- during aerodynamic
- aerodynamic research
- Prior art date
Links
Landscapes
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Transmission Devices (AREA)
Description
Механические шариковые запоры наход т широкое применение .ч различных област х техники. В частности, известны устройства с инерционным грузом, освобождаюш,им замок, удерживаюш,ий элементы объекта, нанример, освобождающим в момент выстрела стонорный механизм взрывател .Mechanical ball locks are widely used in various fields of technology. In particular, devices are known with inertial load, releasing them, locking, holding, object elements, for example, freeing the stonor mechanism of the fuse at the moment of firing.
Описываемое устройство отличаетс от известных и предназначено дл того, чтобы система, состо ша из двух самосто тельных элементов , не разъедин лась при вылете из ствола, а разъедин лась только на нужном, наиеред заданном участке пути прм замедленном полете тел от сопротивлени воздуха. Достигнута эта особенность устройства тем, что инерционный груз, расположенный в канале его, выполнен в виде гильзы с калиброванным отверстием в донной части дл прохода воздуха при замедлении скорости полета, причем гильза перемещаетс вперед но каналу от действи инерционных сил.The described device differs from the known ones and is intended to ensure that the system consists of two independent elements, is not separated when departing from the barrel, and is separated only on the desired predetermined portion of the path of slow motion of the bodies from the air resistance. This feature of the device is achieved by the fact that the inertial load located in its channel is made in the form of a sleeve with a calibrated hole in the bottom part for the passage of air when the flight speed is slowed down, and the sleeve moves forward but to the channel from the action of inertial forces.
Подобное простое но конструкции устройство может быть использовано дл вы снени характера аэродинамического обтекани какоголибо тела, лет щего вслед за другим телом, а также и других подобных исследований.Such a simple device can be used to clarify the nature of the aerodynamic flow around any body flying after another body, as well as other similar studies.
На фиг. 1 показано устройство в положении заненленн ; на фиг. 2- то же, в положении расцеплени .FIG. 1 shows the device in the locked position; in fig. 2- the same in the unlocked position.
Система, состо ща из двух элементов / и 2 объекта, наход щегос в свободном полете, соединена при помощи устройства, состо щего из инерционного груза в внде гильзы 3 с калиброванным отверстием 4, перемещающейс в канале 5, и щариков 6, которые в собранном виде заперты гильзой 3.A system consisting of two elements / and 2 objects in free flight is connected by means of a device consisting of an inertial load in the liner 3 with a calibrated orifice 4 moving in channel 5 and balls 6 that are assembled. locked with a sleeve 3.
Работа устройства. При выстреле система из двух элементов / и 2, соединенных замком устройства, получает начальную скорость. По выходе из канала ствола оруди движение этой системы вследствие соThe operation of the device. When fired, a system of two elements / and 2, connected by a device lock, receives an initial velocity. Upon exiting the bore of the cannon, the movement of this system is due to
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU657409A SU134060A1 (en) | 1960-03-01 | 1960-03-01 | Device for remote separation of two elements of an object in flight during aerodynamic research |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU657409A SU134060A1 (en) | 1960-03-01 | 1960-03-01 | Device for remote separation of two elements of an object in flight during aerodynamic research |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU134060A1 true SU134060A1 (en) | 1960-11-30 |
Family
ID=48405046
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU657409A SU134060A1 (en) | 1960-03-01 | 1960-03-01 | Device for remote separation of two elements of an object in flight during aerodynamic research |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU134060A1 (en) |
-
1960
- 1960-03-01 SU SU657409A patent/SU134060A1/en active
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