SU491260A1 - TIP HANDLEBATE FOR AIR LAUNCH OF AIRCRAFT ENGINE - Google Patents
TIP HANDLEBATE FOR AIR LAUNCH OF AIRCRAFT ENGINEInfo
- Publication number
- SU491260A1 SU491260A1 SU1857756/23A SU1857756A SU491260A1 SU 491260 A1 SU491260 A1 SU 491260A1 SU 1857756/23 A SU1857756/23 A SU 1857756/23A SU 1857756 A SU1857756 A SU 1857756A SU 491260 A1 SU491260 A1 SU 491260A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- piston
- tip
- sleeve
- aircraft engine
- handlebate
- Prior art date
Links
Abstract
Наконечник раздаточного рукава для воздушного запуска двигателя летательного аппарата, содержащий корпус с шариковым замком для крепления наконечника к бортовому штуцеру и рукоятку, отличающийся тем, что, с целью снижения сопротивления проточной части наконечника, снаружи на корпусе закреплен неподвижный поршень, перед которым в корпусе выполнены отверстия и установлена с возможностью продольного перемещения гильза, один конец которой расположен на корпусе и служит запирающим устройством шарикового замка, а другой конец расположен на поршне, при этом между поршнем и внутренним выступом гильзы установлены пружина и втулка с заплечиком, расположенная позади поршня и соединенная шарнирными звеньями с рычагами рукоятки, причем конец гильзы, расположенный на поршне, имеет наружный выступ, на который опирается буртик стакана, между дном которого и заплечиком втулки установлены пружины, суммарное усилие предварительного обжатия которых несколько больше, чем усилие предварительного обжатия пружины поршня.The tip of the distributing sleeve for the air starting of the aircraft engine, comprising a housing with a ball lock for fastening the tip to the onboard fitting and a handle, characterized in that, in order to reduce the resistance of the flowing part of the tip, there is a fixed piston outside the housing, in front of which and installed with the possibility of longitudinal movement of the sleeve, one end of which is located on the body and serves as a locking device of the ball lock, and the other end is a piston, while between the piston and the inner protrusion of the liner there is a spring and sleeve with a shoulder located behind the piston and connected by hinge links to the lever arms, the end of the liner located on the piston having an outer protrusion on which the bead of the glass rests, between the bottom of which and the bushings of the bush are fitted with springs, the total force of the preliminary compression of which is somewhat greater than the force of the preliminary compression of the piston spring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU1857756/23A SU491260A1 (en) | 1972-12-15 | 1972-12-15 | TIP HANDLEBATE FOR AIR LAUNCH OF AIRCRAFT ENGINE |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU1857756/23A SU491260A1 (en) | 1972-12-15 | 1972-12-15 | TIP HANDLEBATE FOR AIR LAUNCH OF AIRCRAFT ENGINE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU491260A1 true SU491260A1 (en) | 2004-11-20 |
Family
ID=60518066
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU1857756/23A SU491260A1 (en) | 1972-12-15 | 1972-12-15 | TIP HANDLEBATE FOR AIR LAUNCH OF AIRCRAFT ENGINE |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU491260A1 (en) |
-
1972
- 1972-12-15 SU SU1857756/23A patent/SU491260A1/en active
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