Invention Grant
- Patent Title: Structural dynamic stability for an aircraft
- Patent Title (中): 飞机的结构动态稳定性
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Application No.: US13323471Application Date: 2011-12-12
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Publication No.: US08376270B2Publication Date: 2013-02-19
- Inventor: John Baker
- Applicant: John Baker
- Applicant Address: US OK Guthrie
- Assignee: Calvin Burgess
- Current Assignee: Calvin Burgess
- Current Assignee Address: US OK Guthrie
- Agency: Hall Estill Attorneys at Law
- Agent Daniel P. Dooley
- Main IPC: B64C17/00
- IPC: B64C17/00 ; B64C5/00

Abstract:
An improvement and method for improved structural dynamic stability for 20 and 30 Series Learjets are disclosed. The improvement includes a redistribution of the elevator mass balance to uncouple the elevator rotational motion from the stabilizer translation motion for the higher order horizontal frequencies having node lines in the proximity of the mass outboard counterbalance weights. The original tail section includes a rudder, and a horizontal stabilizer supporting an elevator mounted adjacent the rudder. The elevator includes a proximal end adjacent the rudder and a distal end that includes a counterbalance portion. The improvement includes replacement of an original mass counterbalance weight from within the counterbalance portion with a new mass counterbalance weight of less mass, and the inclusion of additional mass counterbalance weights disposed within the elevator and interposed between the proximal end and the counterbalance portion.
Public/Granted literature
- US20120091268A1 Structural Dynamic Stability For An Aircraft Public/Granted day:2012-04-19
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