![hydromechanical flight control system hydromechanical flight control system](http://www.aero-mechanic.com/wp-content/uploads/2009/08/5-1.gif)
The CCS is normally designed to be balanced such that such that without pilot intervention, the cyclic stick centers to a position called “trim position”. The mechanical characteristic of a CCS are typically summarized as the effective forces perceived by the pilot through the cyclic stick as the pilot manipulates the cyclic stick. B64C27/59- Transmitting means mechanicalĪ CCS is often described as having particular mechanical characteristics.B64C27/54- Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g.B64C27/00- Rotorcraft Rotors peculiar thereto.B64C13/343- Transmitting means without power amplification or where power amplification is irrelevant mechanical overriding of personal controls with automatic return to inoperative position.B64C13/28- Transmitting means without power amplification or where power amplification is irrelevant mechanical.B64C13/26- Transmitting means without power amplification or where power amplification is irrelevant.B64C13/00- Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers.238000006011 modification reaction Methods 0.000 description 1.230000018109 developmental process Effects 0.000 description 1.125000004122 cyclic group Chemical group 0.000 claims description 55.238000011144 upstream manufacturing Methods 0.000 claims abstract description 17.Application granted granted Critical Publication of US7890222B1 publication Critical patent/US7890222B1/en Publication of US20110036940A1 publication Critical patent/US20110036940A1/en Status Active legal-status Critical Current Anticipated expiration legal-status Critical Links ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: WALKER, TODD, ARJUNAN, SAM, FENNY, CARLOS A., SHULTZ, PETER M.
![hydromechanical flight control system hydromechanical flight control system](https://www.insidescience.org/sites/default/files/2020-05/laser-sail.jpg)
reassignment BELL HELICOPTER TEXTRON INC. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.) Filing date Publication date Priority to US66466407A priority Critical Application filed by Textron Innovations Inc filed Critical Textron Innovations Inc Priority to US12/684,411 priority patent/US7890222B1/en Assigned to BELL HELICOPTER TEXTRON INC. Original Assignee Textron Innovations 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.) Fenny Todd Walker Sam Arjunan Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.) Active Application number US12/684,411 Other versions US20110036940A1
Hydromechanical flight control system pdf#
Google Patents Mechanical flight control auxiliary power assist systemĭownload PDF Info Publication number US7890222B1 US7890222B1 US12/684,411 US68441110A US7890222B1 US 7890222 B1 US7890222 B1 US 7890222B1 US 68441110 A US68441110 A US 68441110A US 7890222 B1 US7890222 B1 US 7890222B1 Authority US United States Prior art keywords control system cyclic control cyclic ccs aircraft according Prior art date Legal status (The legal status is an assumption and is not a legal conclusion. Google Patents US7890222B1 - Mechanical flight control auxiliary power assist system US7890222B1 - Mechanical flight control auxiliary power assist system