亞洲知識產權資訊網為知識產權業界提供一個一站式網上交易平台,協助業界發掘知識產權貿易商機,並與環球知識產權業界建立聯繫。無論你是知識產權擁有者正在出售您的知識產權,或是製造商需要購買技術以提高操作效能,又或是知識產權配套服務供應商,你將會從本網站發掘到有用的知識產權貿易資訊。

Supersonic Thrust Vector Control for Jet Engines Using Staggered Flaps

技術優勢
Lower external profile Increased maneuverability Increased lift
技術應用
Supersonic, air-breathing engines
詳細技術說明
Since the late 1930s, jet engines have become ubiquitous in the aviation industry with turbojet and mixed-flow turbofan engines seeing particular use in highly maneuverable military aircraft. The application of turbojet engines for military use has further supported the development to vector aircraft engine thrust, providing advantages to aircraft that would be otherwise unavailable. Researchers at the University of California, Davis have developed a novel mechanism for vectoring the thrust of supersonic, air-breathing engines. The mechanism uses two asymmetrically staggered ramps; one placed at the throat of the engine nozzle, the other positioned at the exit lip of the nozzle. Thrust vector control (TVC) provides several advantages, such as increased lift and maneuverability.
*Abstract

Researchers at the University of California, Davis have developed a novel mechanism for vectoring the thrust of supersonic, air-breathing jet engines for aircraft applications.

*IP Issue Date
Dec 21, 2017
*Principal Investigation

Name: Roger Davis

Department:


Name: Carlos Montes

Department:

其他

Tech ID/UC Case

25977/2016-824-0


Related Cases

2016-824-0

國家/地區
美國

欲了解更多信息,請點擊 這裡
移動設備