scholarly journals High efficiency low power rectifier design using zero bias schottky diodes

Author(s):  
Aya Mabrouki ◽  
Mohamed Latrach ◽  
Vincent Lorrain
Author(s):  
Aya Mabrouki ◽  
Mohamed Latrach

This chapter proposes an overview of microwave energy harvesting with focuses on the design of high efficiency low power rectifying circuits. A background survey of RF energy harvesting techniques is presented first. Then, the performances of conventional rectifier topologies are analyzed and discussed. A review of the most efficient rectenna designs, from the state of the art, is also presented. Design considerations for low power rectifier operations are detailed and new high efficient rectifying circuits are designed and evaluated in both GSM and ISM bands under low power constraints.


1997 ◽  
Vol 33 (2) ◽  
pp. 160 ◽  
Author(s):  
Y. Muramoto ◽  
K. Kato ◽  
A. Kozen ◽  
M. Ueki ◽  
K. Noguchi ◽  
...  

Author(s):  
Raphaella Luiza Resende da Silva ◽  
Sandro Trindade Mordente Gonçalves ◽  
Christian Vollaire ◽  
Arnaud Bréard ◽  
Gláucio Lopes Ramos ◽  
...  

2011 ◽  
Vol 324 ◽  
pp. 449-452 ◽  
Author(s):  
Vlad Marian ◽  
Salah Eddine Adami ◽  
Christian Vollaire ◽  
Bruno Allard ◽  
Jacques Verdier

This paper presents several RF-to-DC converter topologies and compares their performances based on measurements made on fabricated prototypes. A medium range wireless low power transmission experiment is presented. A low power DC-DC boost converter designed rectenna-generated energy conditioning is also discussed.


2021 ◽  
Vol 11 (14) ◽  
pp. 6549
Author(s):  
Hui Liu ◽  
Ming Zeng ◽  
Xiang Niu ◽  
Hongyan Huang ◽  
Daren Yu

The microthruster is the crucial device of the drag-free attitude control system, essential for the space-borne gravitational wave detection mission. The cusped field thruster (also called the High Efficiency Multistage Plasma Thruster) becomes one of the candidate thrusters for the mission due to its low complexity and potential long life over a wide range of thrust. However, the prescribed minimum of thrust and thrust noise are considerable obstacles to downscaling works on cusped field thrusters. This article reviews the development of the low power cusped field thruster at the Harbin Institute of Technology since 2012, including the design of prototypes, experimental investigations and simulation studies. Progress has been made on the downscaling of cusped field thrusters, and a new concept of microwave discharge cusped field thruster has been introduced.


Author(s):  
Hyung-Soo Kim ◽  
Jae-Sang Lee ◽  
Byung-Hee Son ◽  
Su-Jin Jeon ◽  
Seok-Ho Hong ◽  
...  
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