Invention Grant
- Patent Title: Throttle system
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Application No.: US16707567Application Date: 2019-12-09
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Publication No.: US11542883B2Publication Date: 2023-01-03
- Inventor: Mark Sheridan Hunter , Ronald J. Parker
- Applicant: Textron Aviation Inc.
- Applicant Address: US KS Wichita
- Assignee: Textron Aviation Inc.
- Current Assignee: Textron Aviation Inc.
- Current Assignee Address: US KS Wichita
- Agency: Avek IP, LLC
- Main IPC: F16H59/02
- IPC: F16H59/02 ; F02D41/14 ; F02D11/02 ; B64D31/04 ; B64D31/14 ; F02D11/10 ; F02D41/02 ; B64C27/57

Abstract:
Disclosed is a throttle quadrant arrangement utilizing a throttle lever mechanically connected to three Rotary Variable Differential Transformers (RVDTs). The signals from the RVDTs are monitored by a process where the processing component. More specifically, RVDT outputs are monitored by the engine control system to determine if they are outside a predetermined range of operability. If an RVDT is not operable, the engine control system establishes a thrust output using the signal from one of the functional two. If only one or none are within the range, the system moves on to a default mode.
Public/Granted literature
- US20200182177A1 THROTTLE SYSTEM Public/Granted day:2020-06-11
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