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MIL-B-8584C
BRAKE SYSTEMS, WHEEL, AIRCRAFT DESIGN OF
Organization:
NAVY - AS - Naval Air Systems Command
Year: 1970
Abstract: This specification covers the brake system design requirements for aircraft equipped with wheel-type landing gear.
The brake systems shall be either hydraulic or pneumatic; manually operated, power operated, manual-power operated; and shall be of the following types:
Type I - Manual pressure generating: The control unit generates pressure by manual actuation.
Type II - Power pressure generating: The control unit meters pressure from a power generating system.
Type III - Manual power pressure generating; Pressure is manually generated in a slave control unit which in turn operates the main control unit which meters fluid from a pressure generating system.
Type IV - Power-boosted manual pressure generating: The control unit generates pressure by manual actuation and, in addition, the manually generated pressure is boosted by pressure from a power generating system.
Type V - Power brake valve with emergency master cylinder: One part of the control unit meters pressure from a power generating system, and another part of the control unit serves as a standby manual pressure generating unit when the power system is inoperative. Intended Use: The design requirements specified herein are intended for use in the design of brake systems used on aircraft equipped with wheel-type landing gear.
The brake systems shall be either hydraulic or pneumatic; manually operated, power operated, manual-power operated; and shall be of the following types:
Type I - Manual pressure generating: The control unit generates pressure by manual actuation.
Type II - Power pressure generating: The control unit meters pressure from a power generating system.
Type III - Manual power pressure generating; Pressure is manually generated in a slave control unit which in turn operates the main control unit which meters fluid from a pressure generating system.
Type IV - Power-boosted manual pressure generating: The control unit generates pressure by manual actuation and, in addition, the manually generated pressure is boosted by pressure from a power generating system.
Type V - Power brake valve with emergency master cylinder: One part of the control unit meters pressure from a power generating system, and another part of the control unit serves as a standby manual pressure generating unit when the power system is inoperative. Intended Use: The design requirements specified herein are intended for use in the design of brake systems used on aircraft equipped with wheel-type landing gear.
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| contributor author | NAVY - AS - Naval Air Systems Command | |
| date accessioned | 2017-09-04T15:19:01Z | |
| date available | 2017-09-04T15:19:01Z | |
| date copyright | 08/12/1970 | |
| date issued | 1970 | |
| identifier other | MSAJDAAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/18749 | |
| description abstract | This specification covers the brake system design requirements for aircraft equipped with wheel-type landing gear. The brake systems shall be either hydraulic or pneumatic; manually operated, power operated, manual-power operated; and shall be of the following types: Type I - Manual pressure generating: The control unit generates pressure by manual actuation. Type II - Power pressure generating: The control unit meters pressure from a power generating system. Type III - Manual power pressure generating; Pressure is manually generated in a slave control unit which in turn operates the main control unit which meters fluid from a pressure generating system. Type IV - Power-boosted manual pressure generating: The control unit generates pressure by manual actuation and, in addition, the manually generated pressure is boosted by pressure from a power generating system. Type V - Power brake valve with emergency master cylinder: One part of the control unit meters pressure from a power generating system, and another part of the control unit serves as a standby manual pressure generating unit when the power system is inoperative. Intended Use: The design requirements specified herein are intended for use in the design of brake systems used on aircraft equipped with wheel-type landing gear. | |
| language | English | |
| title | MIL-B-8584C | num |
| title | BRAKE SYSTEMS, WHEEL, AIRCRAFT DESIGN OF | en |
| type | standard | |
| page | 13 | |
| status | Active | |
| tree | NAVY - AS - Naval Air Systems Command:;1970 | |
| contenttype | fulltext |