238000006073 displacement reaction Methods 0.000 description 24.Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.) Filing date Publication date Application filed by Honeywell Inc filed Critical Honeywell Inc Priority to US269209A priority Critical patent/US2770428A/en Application granted granted Critical Publication of US2770428A publication Critical patent/US2770428A/en Anticipated expiration legal-status Critical Status Expired - Lifetime legal-status Critical Current Links Original Assignee Honeywell Inc Priority date (The priority date is an assumption and is not a legal conclusion.
Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.) Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.) Expired - Lifetime Application number US269209A Inventor Clarence E Vogel Current Assignee (The listed assignees may be inaccurate.
Airspeed switchies pdf#
Google Patents Automatic steering mechanismÄownload PDF Info Publication number US2770428A US2770428A US269209A US26920952A US2770428A US 2770428 A US2770428 A US 2770428A US 269209 A US269209 A US 269209A US 26920952 A US26920952 A US 26920952A US 2770428 A US2770428 A US 2770428A Authority US United States Prior art keywords motor slider resistor rudder network Prior art date Legal status (The legal status is an assumption and is not a legal conclusion. Google Patents US2770428A - Automatic steering mechanism Guidelines for ranges are given in the pressure range section of the specifications on page 2.US2770428A - Automatic steering mechanism Pressure ranges for each channel can be specified by the customer. An optional barometer can be installed for display in the front panel or as a separate channel. In the Ps / Pt version the airspeed / airspeed rate channel is a calculated channel. It can be configured as a single channel altitude / altitude rate indicator, (Ps only) a single channel airspeed / airspeed rate indicator (Qc only) or it can be a dual channel unit configured as Ps / Pt or Ps / Qc.
Functional Flexibility The CPA2501 can be configured with an altitude channel and an airspeed channel consisting of Ps / Pt or Ps / Qc. Applied wherever there is a need for a high level of accuracy in an avionics indicator or calibration device.