Invention Grant
- Patent Title: Prismatic-shaped vortex generators
- Patent Title (中): 棱柱形涡流发生器
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Application No.: US12606811Application Date: 2009-10-27
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Publication No.: US08210482B2Publication Date: 2012-07-03
- Inventor: Daniel N. Miller , Dan J. Baruzzini
- Applicant: Daniel N. Miller , Dan J. Baruzzini
- Applicant Address: US MD Bethesda
- Assignee: Lockheed Martin Corporation
- Current Assignee: Lockheed Martin Corporation
- Current Assignee Address: US MD Bethesda
- Agency: Bracewell & Giuliani LLP
- Main IPC: B64C9/00
- IPC: B64C9/00

Abstract:
A prismatic vortex generator for attenuating flow separation which occurs during supersonic flow of air over structure such as an aircraft airfoil, its fuselage, surfaces forming a part of a jet engine inlet, or similar surfaces subjected to supersonic airflow. A series of prismatic vortex generators are provided, each of which is configured to generate a vortex which attenuates flow separation and weight drag resulting from the supersonic airflow. Each prismatic vortex generator has a prismatic shape with a base, leading and trailing ends, and sidewalls that incline toward and join each other to form an apex. The leading end of each prismatic vortex generators is inclined away from the direction of flow.
Public/Granted literature
- US20110095135A1 PRISMATIC-SHAPED VORTEX GENERATORS Public/Granted day:2011-04-28
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