3742813

Information

• Patent Grant
• 3742813

• References
• Source

• Patent Number

  3,742,813

• Date Filed

  Not available

• Date Issued

  Tuesday, July 3, 1973
  51 years ago

• CPC

  • F41F3/052 - Means for securing the rocket in the launching apparatus
  • F15B11/076 - with pneumatic drive or displacement and speed control or stopping by hydraulic braking
  • F15B15/226 - having elastic elements
  • F15B15/261 - using positive interengagement
  • F41F3/042 - the launching apparatus being used also as a transport container for the rocket
  • F15B2211/2053 - Type of pump
  • F15B2211/212 - the pressure sources being accumulators
  • F15B2211/30505 - Non-return valves
  • F15B2211/30525 - Directional control valves
  • F15B2211/327 - electrically or electronically
  • F15B2211/40507 - with constant throttles or orifices
  • F15B2211/40584 - the flow control means arranged in parallel with a check valve
  • F15B2211/41527 - being connected to an output member and a directional control valve
  • F15B2211/41536 - being connected to multiple ports of an output member
  • F15B2211/428 - actuated by fluid pressure
  • F15B2211/45 - Control of bleed-off flow
  • F15B2211/455 - Control of flow in the feed line
  • F15B2211/46 - Control of flow in the return lin
  • F15B2211/473 - without restriction in the reverse direction
  • F15B2211/50554 - the pressure control means controlling a pressure downstream of the pressure control means
  • F15B2211/6336 - representing a state of the output member
  • F15B2211/665 - Methods of control using electronic components
  • F15B2211/71 - Multiple output members
  • F15B2211/72 - having locking means
  • F15B2211/755 - Control of acceleration or deceleration of the output member
  • F15B2211/783 - Sequential control
  • F15B2211/8855 - Compressible fluids

• US Classifications

  • 089 - Ordnance