Patents by Inventor Binyamin Rubin

Binyamin Rubin has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Publication number: 20160289819
    Abstract: Methods of lowering the absorption losses of optical coatings at wavelengths shorter than 350 nm. During a deposition process of a metal oxide optical coating, dissociated hydroxide ion is added to the deposition process. The hydroxide ion source can be, for example, water vapor. By adding the hydroxide ion, a decrease in impurities and defects/dislocations in the optical coating is achieved.
    Type: Application
    Filed: April 2, 2015
    Publication date: October 6, 2016
    Inventors: Ove Lyngnes, Binyamin Rubin
  • Patent number: 9447779
    Abstract: A low power hall thruster is provided that is effective for micro-spacecrafts and nano-spacecrafts as well as mini-spacecrafts. The hall thruster comprises a co-axial acceleration channel capable of being applied with predominantly-radial magnetic field and a co-axial anode within a cavity capable of being applied with substantially longitudinal magnetic field. A cathode-compensator is placed beyond the acceleration channel and magnetic system is provided capable of generating the radial magnetic field within the co-axial acceleration channel and the longitudinal magnetic field within the co-axial anode. An electrically isolated gas distributor is also provided.
    Type: Grant
    Filed: November 11, 2007
    Date of Patent: September 20, 2016
    Inventors: Alexander Kapulkin, Mauricio Moshe Guelman, Vladimir Balabanov, Binyamin Rubin
  • Publication number: 20100107596
    Abstract: A low power hall thruster is provided that is effective for micro-spacecrafts and nano-spacecrafts as well as mini-spacecrafts. The hall thruster comprises a co-axial acceleration channel capable of being applied with predominantly-radial magnetic field and a co-axial anode within a cavity capable of being applied with substantially longitudinal magnetic field. A cathode-compensator is placed beyond the acceleration channel and magnetic system is provided capable of generating the radial magnetic field within the co-axial acceleration channel and the longitudinal magnetic field within the co-axial anode. An electrically isolated gas distributor is also provided.
    Type: Application
    Filed: November 11, 2007
    Publication date: May 6, 2010
    Applicant: Technion Research & Development Foundation Ltd.
    Inventors: Alexander Kapulkin, Mauricio Moshe Guelman, Vladimir Balabanov, Binyamin Rubin