FIELD: testing equipment.
SUBSTANCE: present invention relates to testing equipment, specifically to equipment for high-speed track testing, and can be used in the design of a braking device used to brake rocket carriages. Brake shoe for missile carriage shoes contains a metal frame and a friction lining located on it, consisting of several separate elements with different friction coefficients. Friction lining elements with different friction coefficients are arranged sequentially on the metal frame to form a common working surface, part of the common working surface of the lining element with a high friction coefficient is initially smaller than the rest of the lining element with a lower friction coefficient. The overlays are made with a longitudinal section variable in thickness.
EFFECT: providing a smooth braking mode for rocket carriages with a brake mechanism drive based on powder pressure accumulators.
1 cl, 7 dwg
Title | Year | Author | Number |
---|---|---|---|
ROCKET CARRIAGE WITH CONTROLLED BRAKING | 2020 |
|
RU2739537C1 |
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RU2432511C2 |
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RU2225544C2 |
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RU2502901C1 |
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RU2557339C2 |
DRUM-SHOE BRAKE | 0 |
|
SU1250756A1 |
SHOE BRAKE | 0 |
|
SU821814A1 |
Authors
Dates
2022-08-22—Published
2022-04-19—Filed