Invention Application
- Patent Title: FORWARD PIVOTED FULL FLYING CONTROL TAIL BOOM
- Patent Title (中): 前进的全部飞行控制尾翼
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Application No.: PCT/US2005001350Application Date: 2005-01-18
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Publication No.: WO2006004570B1Publication Date: 2006-04-20
- Inventor: REYNOLDS ROSS STEVEN , SHULTZ DOUG ELLWOOD
- Applicant: NORTHROP GRUMMAN CORP , REYNOLDS ROSS STEVEN , SHULTZ DOUG ELLWOOD
- Assignee: NORTHROP GRUMMAN CORP,REYNOLDS ROSS STEVEN,SHULTZ DOUG ELLWOOD
- Current Assignee: NORTHROP GRUMMAN CORP,REYNOLDS ROSS STEVEN,SHULTZ DOUG ELLWOOD
- Priority: US77493204 2004-02-09
- Main IPC: B64C9/02
- IPC: B64C9/02 ; B64C9/08 ; B64C13/16 ; B64C39/10 ; B64C3/58
Abstract:
An aircraft motion control mechanism for regulating aircraft motion from a location remote from an aircraft body portion. The aircraft auxiliary control mechanism has at least one control surface support arm connected to and extending from the aircraft body portion, and an auxiliary flow control surface connected to the support arm. By pivotally controlling the movement of the support arm, the auxiliary flow control surface is operative to deflect airflow to regulate orientation of the aircraft. In addition, the auxiliary flow control surface may further deflect the airflow by deflecting about the support arm.
Public/Granted literature
- WO2006004570A3 Forward pivoted full flying control tail boom Public/Granted day:2006-05-11
Information query
