|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/204; 244/209; 244/210|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 12 인용 특허 : 11|
The present invention relates to a reconfigurable porous technology for fluid flow control system and more particularly to reconfigurable porosity fluid flow control system for vehicles such as aircraft, missiles, ground and water vehicles to improve the performance of such vehicles. The present invention further relates to a method of operating the reconfigurable fluid flow control system.In one embodiment, the present invention includes a reconfigurable porosity system for fluid flow control on the surface of an aircraft, missile, water-craft or ground...
1. A reconfigurable porosity system for fluid flow control on the surface of an aircraft missile, watercraft or ground vehicle comprisinga porous outer skin comprising individual pores; individually addressable valves corresponding and connected individual pores for opening and closing the pores; a pneumatic system for connecting the pores; a sensor having an output, the output being used at least in part to estimate or determine the high and low pressure areas of the porous outer skin, and a closed loop control system far opening and closing the individ...