Khorrami
Behrooz V. Khorrami, Livingston, NJ US
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20140275709 | METHODS AND SYSTEMS FOR DETERMINING THE DISTRIBUTION OF RADIATION DOSE AND RESPONSE - A system, method and computer program product to determine radiation dose from radionuclides used to treat a patient in need thereof. The present invention allows users to visualize and understand the impact of radionuclide choice, distribution of activity in the cell, distribution of activity among the cells, cell dimensions, cell separation distance, cluster size, and radiobiological response parameters on the capacity to kill populations of cells. All of these parameters can play a substantial role in determining the surviving fraction of cells. Accordingly, this system, method and computer program product can assist in designing treatment plans for therapeutic radiopharmaceuticals suited to individual needs. | 09-18-2014 |
Farshad Khorrami, Brooklyn, NY US
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20100025261 | CONTROL APPARATUS, SYSTEM, AND METHOD FOR REDUCTION AND/OR PREVENTION OF SPACE WEATHER INDUCED CORROSION - An apparatus, system, method and computer program product directed to controlling corrosion, particularly space weather induced corrosion, of a conductive structure in contact with a corrosive environment and coated with a semiconductive coating, where the corrosion is controlled by a controllable filter and a corresponding electronic control unit configured to process and adjust the controllable filter in response to at least one measured parameter associated with space weather effects on the conductive structure. | 02-04-2010 |
Fereshteh Khorrami, San Diego, CA US
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20130141500 | FIXER COMPOSITION - A fixer composition is disclosed herein. An example of the fixer composition includes from about 5 wt % to about 25 wt % of a co-solvent, from about 1 wt % to about 20 wt % of a calcium salt, from about 0.01 wt % to about 0.6 wt % of a sulfonated chelating agent, and a balance of water. | 06-06-2013 |
20140300673 | INK COMPOSITION - An ink composition is disclosed herein. The ink composition includes from about 5 wt % to about 25 wt % of a co-solvent; from about 0.025 wt % to about 0.2 wt % of i) a chelating agent represented by formula 1, wherein R′ is a carboxylic acid functional group or a carboxylate salt functional group and n>2; ii) a chelating agent represented by formula 2:, wherein R is a carboxylic acid functional group or a carboxylate salt functional group, m is greater than or equal to 1, x is greater than or equal to 2, y is greater than or equal to 1, and z is greater than or equal to 2; iii) a chelating agent represented by formula 3, wherein any of r, s, t, or u is a sulfonic acid functional group or a sulfonate functional group; or iv) combinations of any of i, ii, and iii. The ink composition also includes a balance of water. | 10-09-2014 |
Mehdi R. Khorrami, Norfolk, VA US
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20120097791 | Autonomous Slat-Cove-Filler Device for Reduction of Aeroacoustic Noise Associated with Aircraft Systems - A slat cove filler is utilized to reduce airframe noise resulting from deployment of a leading edge slat of an aircraft wing. The slat cove filler is preferably made of a super elastic shape memory alloy, and the slat cove filler shifts between stowed and deployed shapes as the slat is deployed. The slat cove filler may be configured such that a separate powered actuator is not required to change the shape of the slat cove filler from its deployed shape to its stowed shape and vice-versa. The outer contour of the slat cove filler preferably follows a profile designed to maintain accelerating flow in the gap between the slat cove filler and wing leading edge to provide for noise reduction. | 04-26-2012 |
20120153086 | Elastically Deformable Side-Edge Link for Trailing-Edge Flap Aeroacoustic Noise Reduction - A system is provided for reducing aeroacoustic noise generated by an aircraft having wings equipped with trailing-edge flaps. The system includes a plurality of elastically deformable structures. Each structure is coupled to and along one of the side edges of one of the trailing-edge flaps, and is coupled to a portion of one of the wings that is adjacent to the one of the side edges. The structures elastically deform when the trailing-edge flaps are deployed away from the wings. | 06-21-2012 |
20120261517 | Multi-Element Airfoil System - A multi-element airfoil system includes an airfoil element having a leading edge region and a skin element coupled to the airfoil element. A slat deployment system is coupled to the slat and the skin element, and is capable of deploying and retracting the slat and the skin element. The skin element substantially fills the lateral gap formed between the slat and the airfoil element when the slat is deployed. The system further includes an uncoupling device and a sensor to remove the skin element from the gap based on a critical angle-of-attack of the airfoil element. The system can alternatively comprise a trailing edge flap, where a skin element substantially fills the lateral gap between the flap and the trailing edge region of the airfoil element. In each case, the skin element fills a gap between the airfoil element and the deployed flap or slat to reduce airframe noise. | 10-18-2012 |
Mohammad A. Khorrami, Ypsilanti, MI US
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20100021262 | FASTENER RETAINER - A fastener retainer is provided capable of retaining a fastener to a part prior to and during assembly. A first portion engages a fastener flange while leaving a fastener head exposed for assembly tool access. A second portion has flanges that engage the edges of the part. | 01-28-2010 |
20120237314 | FASTENER RETAINER - A fastener retainer is provided capable of retaining a fastener to a part prior to and during assembly. A first portion engages a fastener flange while leaving a fastener head exposed for assembly tool access. A second portion has flanges that engage the edges of the part. | 09-20-2012 |
Morteza Khorrami, Tehran IR
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20100234491 | METHOD AND MATERIAL FOR MANUFACTURING FIBER CEMENT BOARD - The various embodiments herein provide a method and materials to produce non-asbestos Fiber Cement Board (FCB). According to one embodiment herein, a new material including Cement (60%-75% by weight), Acrylic fiber (1%-4% by weight), Nano silicate (1%-4% by weight), slake lime stone powder (5%-20% by weight), waste cardboard pulp paper (3%-12% by weight) and some polymeric additives are used to make FCB in the Hatcheck process. In another embodiment, a method to make FCB using this method in the Hatcheck process, only some small changes are needed. According to another embodiment, the FCB produced in this method can be used for cladding, internal wall and external walls. | 09-16-2010 |