Patents by Inventor Michael Kriegel

Michael Kriegel 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).

  • Patent number: 11990472
    Abstract: Gate-all-around integrated circuit structures having pre-spacer-deposition cut gates are described. For example, an integrated circuit structure includes a first vertical arrangement of horizontal nanowires and a second vertical arrangement of horizontal nanowires. A first gate stack is over the first vertical arrangement of horizontal nanowires, and a second gate stack is over the second vertical arrangement of horizontal nanowires. An end of the second gate stack is spaced apart from an end of the first gate stack by a gap. The integrated circuit structure also includes a dielectric structure having a first portion forming a gate spacer along sidewalls of the first gate stack, a second portion forming a gate spacer along sidewalls of the second gate stack, and a third portion completely filling the gap, the third portion continuous with the first and second portions.
    Type: Grant
    Filed: September 23, 2020
    Date of Patent: May 21, 2024
    Assignee: Intel Corporation
    Inventors: Leonard P. Guler, Michael K. Harper, William Hsu, Biswajeet Guha, Tahir Ghani, Niels Zussblatt, Jeffrey Miles Tan, Benjamin Kriegel, Mohit K. Haran, Reken Patel, Oleg Golonzka, Mohammad Hasan
  • Patent number: 9637437
    Abstract: Benzene derivatives of the formula (I); wherein R1 and R2, are the same or different and independently are selected from the group consisting of hydrogen, alkyl, aralkyl, —CHO, —CH2OR3, —CH(OR4)(OR5) and —COOR6, wherein R3, R4 and R5 are the same or different and are selected from hydrogen, alkyl, aryl, alkaryl, aralkyl, alkylcarbonyl or arylcarbonyl, or wherein R4 and R5 together form an alkylene group and wherein R6 is selected from hydrogen, alkyl and aryl, are prepared in a process, which comprises: reacting a furan derivative of formula (II): wherein R1 and R2 have the meanings above, with ethylene under cycloaddition reaction conditions in the presence of an acid solvent to produce the benzene derivative, wherein the acid solvent is a carboxylic acid and is present in a weight ratio acid solvent to furan derivative from 1:1 to 250:1.
    Type: Grant
    Filed: October 22, 2013
    Date of Patent: May 2, 2017
    Assignees: FURANIX TECHNOLOGIES B.V., THE COCA-COLA COMPANY
    Inventors: Bing Wang, Gerardus Johannes Maria Gruter, Matheus Adrianus Dam, Robert Michael Kriegel
  • Publication number: 20160137579
    Abstract: Benzene derivatives of the formula (I); wherein R1 and R2, are the same or different and independently are selected from the group consisting of hydrogen, alkyl, aralkyl, —CHO, —CH2OR3, —CH(OR4)(OR5) and —COOR6, wherein R3, R4 and R5 are the same or different and are selected from hydrogen, alkyl, aryl, alkaryl, aralkyl, alkylcarbonyl or arylcarbonyl, or wherein R4 and R5 together form an alkylene group and wherein R6 is selected from hydrogen, alkyl and aryl, are prepared in a process, which comprises: reacting a furan derivative of formula (II): wherein R1 and R2 have the meanings above, with ethylene under cycloaddition reaction conditions in the presence of an acid solvent to produce the benzene derivative, wherein the acid solvent is a carboxylic acid and is present in a weight ratio acid solvent to furan derivative from 1:1 to 250:1.
    Type: Application
    Filed: October 22, 2013
    Publication date: May 19, 2016
    Inventors: Bing Wang, Gerardus Johannes Maria Gruter, Matheus Adrianus Dam, Robert Michael Kriegel
  • Publication number: 20150136897
    Abstract: The invention relates to an aircraft (1), preferably an unmanned aircraft (UAV), drone, or Unmanned Aerial System (UAS), comprising a rigid wing (2) which enables aerodynamic horizontal flight, and at least four rotors (4, 4?) which are driven by means of controllable electric motors (5) and which can be pivoted between a vertical starting position and a horizontal flight position by means of a pivoting mechanism (7), wherein all electric motors (5) and rotors (4) are arranged on the wing (2).
    Type: Application
    Filed: May 31, 2013
    Publication date: May 21, 2015
    Applicant: LOGO-TEAM UG (HAFTUNGSBESCHRANKT)
    Inventors: Florian Seibel, Michael Wohlfahrt, Michael Kriegel