Patents by Inventor Ozan Uluc
Ozan Uluc 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).
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Patent number: 9617007Abstract: A system for controlling a cooling system comprises an operating state detection unit adapted to detect operating signals characteristic of the operating state of the cooling system and/or the operating state of a plurality of cooling energy consumers to be supplied with cooling energy by the cooling system and a database in which priority data dependent on the operating state and characteristic of the priority to be given to the cooling energy consumers in terms of the cooling energy to be supplied in various operating states of the cooling system and/or of the cooling energy consumers, is stored for a plurality of cooling energy consumers to be supplied with cooling energy by the cooling system.Type: GrantFiled: March 29, 2012Date of Patent: April 11, 2017Assignee: Airbus Operations GmbHInventors: Marc Hoelling, Werner Rothammer, Jan Dittmar, Carsten Colberg, Wilson Willy Casas Noriega, Ozan Uluc, Sebastian Roering, Holger Wolf
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Patent number: 9315272Abstract: A system for cooling and/or heating aircraft devices to be cooled and/or heated includes a first individual cooling and/or heating system associated with a first aircraft device to be cooled and/or heated, a second individual cooling and/or heating system associated with a second aircraft device to be cooled and/or heated, a cooling and/or heating energy supply apparatus adapted to supply cooling and/or heating energy generated by the first and/or the second individual cooling and/or heating system to the first and/or the second aircraft device to be cooled and/or heated, a control device adapted to receive and process signals characteristic of the cooling and/or heating requirements of the first and/or the second aircraft device to be cooled and/or heated and of the load condition of the first and/or the second individual cooling and/or heating system.Type: GrantFiled: March 28, 2012Date of Patent: April 19, 2016Assignee: AIRBUS OPERATIONS GMBHInventors: Marc Hoelling, Werner Rothammer, Jan Dittmar, Carsten Colberg, Wilson Willy Casas Noriega, Ozan Uluc, Sebastian Roering, Holger Wolf
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Patent number: 9167720Abstract: The invention relates to an improved aircraft electronics cooling system for an aircraft having a liquid cooling system, the aircraft electronics cooling system providing a thermal coupling between an electronic device to be cooled and the liquid cooling system of the aircraft. A coolant delivered by the liquid cooling system may flow through a board of the electronic device, through a heat sink on which the electronic device is arranged and/or through a housing in which the electronic device is arranged. The coolant may be permanently in the liquid state in a cooling circuit. The coolant may vaporize at least partially while cooling the electronic device.Type: GrantFiled: March 18, 2013Date of Patent: October 20, 2015Assignee: Airbus Operations GmbHInventors: Ozan Uluc, Ahmet Kayihan Kiryaman, Andreas Frey
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Publication number: 20130215572Abstract: The invention relates to an improved aircraft electronics cooling system for an aircraft having a liquid cooling system, the aircraft electronics cooling system providing a thermal coupling between an electronic device to be cooled and the liquid cooling system of the aircraft. A coolant delivered by the liquid cooling system may flow through a board of the electronic device, through a heat sink on which the electronic device is arranged and/or through a housing in which the electronic device is arranged. The coolant may be permanently in the liquid state in a cooling circuit. The coolant may vaporize at least partially while cooling the electronic device.Type: ApplicationFiled: March 18, 2013Publication date: August 22, 2013Applicant: AIRBUS OPERATIONS GMBHInventors: Ozan Uluc, Ahmet Kayihan Kiryaman, Andreas Frey
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Publication number: 20130075055Abstract: A system for cooling and/or heating aircraft devices to be cooled and/or heated includes a first individual cooling and/or heating system associated with a first aircraft device to be cooled and/or heated, a second individual cooling and/or heating system associated with a second aircraft device to be cooled and/or heated, a cooling and/or heating energy supply apparatus adapted to supply cooling and/or heating energy generated by the first and/or the second individual cooling and/or heating system to the first and/or the second aircraft device to be cooled and/or heated, a control device adapted to receive and process signals characteristic of the cooling and/or heating requirements of the first and/or the second aircraft device to be cooled and/or heated and of the load condition of the first and/or the second individual cooling and/or heating system.Type: ApplicationFiled: March 28, 2012Publication date: March 28, 2013Applicant: AIRBUS OPERATIONS GMBHInventors: Marc HOELLING, Werner ROTHAMMER, Jan DITTMAR, Carsten COLBERG, Wilson WIlly CASAS NORIEGA, Ozan ULUC, Sebastian ROERING, Holger WOLF
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Patent number: 8336329Abstract: A system (10) for cooling freight goods on board an aircraft comprises a refrigerating apparatus and a cooling station (14) to which cooling energy generated by said refrigerating apparatus is fed by means of a refrigerating medium and which is connected to an air infeed line (29) of an air-conditioning installation of the aircraft, wherein an air outlet aperture (16) of the cooling station (14) is connectable to a freight compartment (24) of the aircraft in order to discharge into said freight compartment (24) air which has been cooled down to a desired temperature.Type: GrantFiled: March 25, 2008Date of Patent: December 25, 2012Assignee: Airbus Operations GmbHInventors: Ozan Uluc, Andreas Frey, Sven Reisbach, Frank Bliemeister
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Patent number: 8331093Abstract: The invention relates to an improved aircraft electronics cooling system for an aircraft having a liquid cooling system (2), the aircraft electronics cooling system providing a thermal coupling between an electronic device (40a, 40b, 40c, 40d, 42, 44) to be cooled and the liquid cooling system (2) of the aircraft. A coolant delivered by the liquid cooling system (2) may flow through a board of the electronic device (40a, 40b, 40c, 40d), through a heat sink on which the electronic device (42) is arranged and/or through a housing in which the electronic device (44) is arranged. The coolant may be permanently in the liquid state in a cooling circuit. The coolant may vaporize at least partially while cooling the electronic device.Type: GrantFiled: February 28, 2011Date of Patent: December 11, 2012Assignee: Airbus Operations GmbHInventors: Ozan Uluc, Ahmet Kayihan Kiryaman, Andreas Frey
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Patent number: 8315053Abstract: The invention relates to an improved aircraft electronics cooling system for an aircraft having a liquid cooling system (2), the aircraft electronics cooling system providing a thermal coupling between an electronic device (40a, 40b, 40c, 40d, 42, 44) to be cooled and the liquid cooling system (2) of the aircraft. A coolant delivered by the liquid cooling system (2) may flow through a board of the electronic device (40a, 40b, 40c, 40d), through a heat sink on which the electronic device (42) is arranged and/or through a housing in which the electronic device (44) is arranged. The coolant may be permanently in the liquid state in a cooling circuit. The coolant may vaporize at least partially while cooling the electronic device.Type: GrantFiled: February 28, 2011Date of Patent: November 20, 2012Assignee: Airbus Operations GmbHInventors: Ozan Uluc, Ahmet Kayihan Kiryaman, Andreas Frey
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Publication number: 20120279680Abstract: A system for controlling a cooling system comprises an operating state detection unit adapted to detect operating signals characteristic of the operating state of the cooling system and/or the operating state of a plurality of cooling energy consumers to be supplied with cooling energy by the cooling system and a database in which priority data dependent on the operating state and characteristic of the priority to be given to the cooling energy consumers in terms of the cooling energy to be supplied in various operating states of the cooling system and/or of the cooling energy consumers, is stored for a plurality of cooling energy consumers to be supplied with cooling energy by the cooling system.Type: ApplicationFiled: March 29, 2012Publication date: November 8, 2012Inventors: Marc Hoelling, Werner Rothammer, Jan Dittmar, Carsten Colberg, Wilson Willy Casas Noriega, Ozan Uluc, Sebastian Roering, Holger Wolf
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Patent number: 8225622Abstract: A system for cooling items of freight on board an aircraft includes a refrigerating device and also a cooling station to which cooling energy generated by the refrigerating device is supplied by a refrigerant medium. The cooling station is capable of being connected to a freight compartment of the aircraft or to a freight container on board the aircraft, in order to lead the cooling energy supplied to the cooling station away into the freight compartment or into the freight container. A freight container for receiving items of freight designated for transportation on board an aircraft is capable of being connected to a cooling station of a system for cooling items of freight on board an aircraft, so that the cooling energy supplied to the cooling station is capable of being led away into the freight container.Type: GrantFiled: April 11, 2007Date of Patent: July 24, 2012Assignee: Airbus Deutschland GmbHInventors: Ozan Uluc, Kayihan Ahmet Kiryaman, Matthias Witschke
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Publication number: 20110216505Abstract: The invention relates to an improved aircraft electronics cooling system for an aircraft having a liquid cooling system (2), the aircraft electronics cooling system providing a thermal coupling between an electronic device (40a, 40b, 40c, 40d, 42, 44) to be cooled and the liquid cooling system (2) of the aircraft. A coolant delivered by the liquid cooling system (2) may flow through a board of the electronic device (40a, 40b, 40c, 40d), through a heat sink on which the electronic device (42) is arranged and/or through a housing in which the electronic device (44) is arranged. The coolant may be permanently in the liquid state in a cooling circuit. The coolant may vaporize at least partially while cooling the electronic device.Type: ApplicationFiled: February 28, 2011Publication date: September 8, 2011Applicant: AIRBUS OPERATIONS GMBHInventors: Ozan Uluc, Ahmet Kayihan Kiryaman, Andreas Frey
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Publication number: 20110170263Abstract: The invention relates to an improved aircraft electronics cooling system for an aircraft having a liquid cooling system (2), the aircraft electronics cooling system providing a thermal coupling between an electronic device (40a, 40b, 40c, 40d, 42, 44) to be cooled and the liquid cooling system (2) of the aircraft. A coolant delivered by the liquid cooling system (2) may flow through a board of the electronic device (40a, 40b, 40c, 40d), through a heat sink on which the electronic device (42) is arranged and/or through a housing in which the electronic device (44) is arranged. The coolant may be permanently in the liquid state in a cooling circuit. The coolant may vaporize at least partially while cooling the electronic device.Type: ApplicationFiled: February 28, 2011Publication date: July 14, 2011Applicant: AIRBUS OPERATIONS GMBHInventors: Ozan Uluc, Ahmet Kayihan Kiryaman, Andreas Frey
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Publication number: 20110149517Abstract: The invention relates to an improved aircraft electronics cooling system for an aircraft having a liquid cooling system (2), the aircraft electronics cooling system providing a thermal coupling between an electronic device (40a, 40b, 40c, 40d, 42, 44) to be cooled and the liquid cooling system (2) of the aircraft. A coolant delivered by the liquid cooling system (2) may flow through a board of the electronic device (40a, 40b, 40c, 40d), through a heat sink on which the electronic device (42) is arranged and/or through a housing in which the electronic device (44) is arranged. The coolant may be permanently in the liquid state in a cooling circuit. The coolant may vaporize at least partially while cooling the electronic device.Type: ApplicationFiled: February 28, 2011Publication date: June 23, 2011Applicant: AIRBUS OPERATIONS GMBHInventors: Ozan Uluc, Ahmet Kayihan Kiryaman, Andreas Frey
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Patent number: 7920382Abstract: The invention relates to an improved aircraft electronics cooling system for an aircraft having a liquid cooling system (2), the aircraft electronics cooling system providing a thermal coupling between an electronic device (40a, 40b, 40c, 40d, 42, 44) to be cooled and the liquid cooling system (2) of the aircraft. A coolant delivered by the liquid cooling system (2) may flow through a board of the electronic device (40a, 40b, 40c, 40d), through a heat sink on which the electronic device (42) is arranged and/or through a housing in which the electronic device (44) is arranged. The coolant may be permanently in the liquid state in a cooling circuit. The coolant may vaporize at least partially while cooling the electronic device.Type: GrantFiled: February 19, 2010Date of Patent: April 5, 2011Assignee: Airbus Operations GmbHInventors: Ozan Uluc, Ahmet Kayihan Kiryaman, Andreas Frey
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Publication number: 20100202108Abstract: The invention relates to an improved aircraft electronics cooling system for an aircraft having a liquid cooling system (2), the aircraft electronics cooling system providing a thermal coupling between an electronic device (40a, 40b, 40c, 40d, 42, 44) to be cooled and the liquid cooling system (2) of the aircraft. A coolant delivered by the liquid cooling system (2) may flow through a board of the electronic device (40a, 40b, 40c, 40d), through a heat sink on which the electronic device (42) is arranged and/or through a housing in which the electronic device (44) is arranged. The coolant may be permanently in the liquid state in a cooling circuit. The coolant may vaporize at least partially while cooling the electronic device.Type: ApplicationFiled: February 19, 2010Publication date: August 12, 2010Applicant: AIRBUS OPERATIONS GMBHInventors: Ozan Uluc, Ahmet Kayihan Kiryaman, Andreas Frey
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Publication number: 20100101262Abstract: A system (10) for cooling freight goods on board an aircraft comprises a refrigerating apparatus and a cooling station (14) to which cooling energy generated by said refrigerating apparatus is fed by means of a refrigerating medium and which is connected to an air infeed line (29) of an air-conditioning installation of the aircraft, wherein an air outlet aperture (16) of the cooling station (14) is connectable to a freight compartment (24) of the aircraft in order to discharge into said freight compartment (24) air which has been cooled down to a desired temperature.Type: ApplicationFiled: March 25, 2008Publication date: April 29, 2010Inventors: Ozan Uluc, Andreas Frey, Sven Reisbach, Frank Bliemeister
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Patent number: 7697292Abstract: The invention relates to an improved aircraft electronics cooling system for an aircraft having a liquid cooling system (2), the aircraft electronics cooling system providing a thermal coupling between an electronic device (40a, 40b, 40c, 40d, 42, 44) to be cooled and the liquid cooling system (2) of the aircraft. A coolant delivered by the liquid cooling system (2) may flow through a board of the electronic device (40a, 40b, 40c, 40d), through a heat sink on which the electronic device (42) is arranged and/or through a housing in which the electronic device (44) is arranged. The coolant may be permanently in the liquid state in a cooling circuit. The coolant may vaporize at least partially while cooling the electronic device.Type: GrantFiled: September 6, 2007Date of Patent: April 13, 2010Assignee: Airbus Deutschland GmbHInventors: Ozan Uluc, Ahmet Kayihan Kiryaman, Andreas Frey
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Publication number: 20090193835Abstract: A system (10, 10?) for cooling items of freight on board an aircraft includes a refrigerating device and also a cooling station (14, 14?) to which cooling energy generated by the refrigerating device is supplied by means of a refrigerant medium. The cooling station (14, 14?) is capable of being connected to a freight compartment (24) of the aircraft or to a freight container (26?) on board the aircraft, in order to lead the cooling energy supplied to the cooling station (14, 14?) away into the freight compartment (24) or into the freight container (26?). A freight container (26?) for receiving items of freight designated for transportation on board an aircraft is capable of being connected to a cooling station (14?) of a system (10?) for cooling items of freight on board an aircraft, so that the cooling energy supplied to the cooling station (14?) is capable of being led away into the freight container (26?).Type: ApplicationFiled: April 11, 2007Publication date: August 6, 2009Applicant: AIRBUS DEUTSCHLAND GMBHInventors: Ozan Uluc, Kayihan Ahmet Kiryaman, Matthias Witschke
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Publication number: 20080055852Abstract: The invention relates to an improved aircraft electronics cooling system for an aircraft having a liquid cooling system (2), the aircraft electronics cooling system providing a thermal coupling between an electronic device (40a, 40b, 40c, 40d, 42, 44) to be cooled and the liquid cooling system (2) of the aircraft. A coolant delivered by the liquid cooling system (2) may flow through a board of the electronic device (40a, 40b, 40c, 40d), through a heat sink on which the electronic device (42) is arranged and/or through a housing in which the electronic device (44) is arranged. The coolant may be permanently in the liquid state in a cooling circuit. The coolant may vaporise at least partially while cooling the electronic device.Type: ApplicationFiled: September 6, 2007Publication date: March 6, 2008Applicant: AIRBUS DEUTSCHLAND GMBHInventors: Ozan Uluc, Ahmet Kayihan Kiryaman, Andreas Frey