Patents by Inventor Jaman El Masalme
Jaman El Masalme 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: 11592181Abstract: A gas turbine combustion chamber, having a combustion chamber housing, a burner positioned at least partially in the combustion chamber housing and a flame tube positioned in the combustion chamber housing. An upstream end of the flame tube has a flame tube cover. In the region of the flame tube cover radially inside the flame tube cover a mixing tube of the burner extends, which defines a pre-primary combustion zone. Between the mixing tube of the burner and the flame tube cover an axial air flow passage is formed, via which air can be conducted in the axial direction outside along the mixing tube, and into the flame tube cover radial air flow passages are introduced via which the air following the axial air flow passage can be conducted in the radial direction of the flame tube cover for cooling the flame tube cover.Type: GrantFiled: September 19, 2019Date of Patent: February 28, 2023Assignee: MAN ENERGY SOLUTIONS SEInventors: Jaman El Masalme, Stefan Clauss, Jan-Niklas Bleyl
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Patent number: 10662800Abstract: A gas turbine with a compressor, in which air can be compressed; with at least one burner having a combustion chamber, which can be supplied with the compressed air and in which a fuel can be combusted in the presence of the compressed air subject to heating the air; a turbine, in which the heated air can be expanded; a diffuser arranged, seen in flow direction of the expanded air, downstream of the turbine; a plurality of temperature sensors, dependent on the measurement values of which a thermodynamic mean temperature or mixed-out turbine outlet temperature of the expanded air can be determined. The temperature sensors are arranged in the region of a diffuser cover, which at an outlet end of the diffuser closes off a hollow space of the diffuser positioned radially inside of a flow duct of the diffuser.Type: GrantFiled: January 17, 2018Date of Patent: May 26, 2020Assignee: MAN Energy Solutions SEInventors: Christian Günther, David Kluβ, Jaman El Masalme
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Publication number: 20200124283Abstract: A gas turbine combustion chamber, having a combustion chamber housing, a burner positioned at least partially in the combustion chamber housing and a flame tube positioned in the combustion chamber housing. An upstream end of the flame tube has a flame tube cover. In the region of the flame tube cover radially inside the flame tube cover a mixing tube of the burner extends, which defines a pre-primary combustion zone. Between the mixing tube of the burner and the flame tube cover an axial air flow passage is formed, via which air can be conducted in the axial direction outside along the mixing tube, and into the flame tube cover radial air flow passages are introduced via which the air following the axial air flow passage can be conducted in the radial direction of the flame tube cover for cooling the flame tube cover.Type: ApplicationFiled: September 19, 2019Publication date: April 23, 2020Inventors: Jaman El Masalme, Stefan Clauss, Jan-Niklas Bleyl
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Publication number: 20180266277Abstract: A gas turbine with a compressor having stator side guide blades and rotor side moving blades, a burner a combustion chamber; with a turbine); with a diffuser arranged downstream of the compressor, which has an inside wall and an outside wall and; an intermediate housing following the outside wall. An outlet side guide blade ring of stator side, outlet side guide blades (30a) of the compressor has an inner shroud and an outer shroud. First fastening devices are formed on the outer shroud (34) of the guide blade ring via which the guide blade ring is attached to the intermediate housing, second fastening devices are formed, on the inner shroud (33) of the guide blade ring via which the inside wall of the diffuser is directly attached to the guide blade ring.Type: ApplicationFiled: March 15, 2018Publication date: September 20, 2018Inventors: Emil ASCHENBRUCK, Stefan CLAUSS, Andreas KLEINEFELDT, Jaman EL MASALME, Michael BLASWICH
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Publication number: 20180209293Abstract: A gas turbine with a compressor, in which air can be compressed; with at least one burner having a combustion chamber, which can be supplied with the compressed air and in which a fuel can be combusted in the presence of the compressed air subject to heating the air; a turbine, in which the heated air can be expanded; a diffuser arranged, seen in flow direction of the expanded air, downstream of the turbine; a plurality of temperature sensors, dependent on the measurement values of which a thermodynamic mean temperature or mixed-out turbine outlet temperature of the expanded air can be determined. The temperature sensors are arranged in the region of a diffuser cover, which at an outlet end of the diffuser closes off a hollow space of the diffuser positioned radially inside of a flow duct of the diffuser.Type: ApplicationFiled: January 17, 2018Publication date: July 26, 2018Inventors: Christian GÜNTHER, David KLUß, Jaman EL MASALME
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Patent number: 9739176Abstract: A turbomachine includes: a stator-side housing having: a plurality of stator-side guide vane supports fastened to the stator-side housing, stator-side guide vanes fastened to the stator-side guide vane supports, and axially spaced guide vane rings; and a rotor having a plurality of rotor-side moving blades. At least two guide vane supports are jointly fastened to and centered on a flange of the stator-side housing.Type: GrantFiled: October 22, 2014Date of Patent: August 22, 2017Assignee: MAN Diesel & Turbo SEInventors: Emil Aschenbruck, Jaman El Masalme, Michael Blaswich
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Patent number: 9377197Abstract: A gas turbine combustion chamber has a housing (1), a flame tube (2) received therein, and a perforated plate (3) which at least partially surrounds the latter and which is fastened at both of its end faces (3.1, 3.2) to the housing.Type: GrantFiled: July 20, 2010Date of Patent: June 28, 2016Assignee: MAN Diesel & Turbo SEInventors: Jaman El Masalme, Emil Aschenbruck, Reiner Brinkmann
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Patent number: 9182039Abstract: A sealing segment for sealingly connecting two structural components parts which are movable relative to one another, with two sealing bodies which are connected to one another by a web and which can be arranged in recesses of the structural component parts in an articulated manner, and a sealing segment arrangement with a plurality of sealing segments of this type, and a flow machine with a sealing segment arrangement of this type.Type: GrantFiled: November 3, 2008Date of Patent: November 10, 2015Assignee: MAN Diesel & Turbo SEInventors: Emil Aschenbruck, Michael Blaswich, Jaman El Masalme, Frank Reiss
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Patent number: 9140452Abstract: Combustor for a turbine having a housing in which an air collecting chamber, a combustion antechamber, and a combustion chamber are formed. A combustor head plate is arranged in the housing so that the combustor head plate separates the combustion antechamber from the combustion chamber. A baffle plate is arranged in the combustion antechamber so that the baffle plate divides the combustion antechamber into a first sub-chamber adjoining an air supply fluidically connected with the air collecting chamber and a second sub-chamber adjoining the combustor head plate. Wherein baffle plate has a plurality of through-passages that fluidically connect the first sub-chamber with the second sub-chamber so that air that has flowed into the first sub-chamber from the air collecting chamber via the air supply can flow into the second sub-chamber via the through-passages and to a back surface of the combustor head plate facing the second sub-chamber.Type: GrantFiled: October 27, 2010Date of Patent: September 22, 2015Assignee: MAN Diesel & Turbo SEInventors: Frank Reiss, Jaman El Masalme
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Publication number: 20150118039Abstract: A turbomachine includes: a stator-side housing having: a plurality of stator-side guide vane supports fastened to the stator-side housing, stator-side guide vanes fastened to the stator-side guide vane supports, and axially spaced guide vane rings; and a rotor having a plurality of rotor-side moving blades. At least two guide vane supports are jointly fastened to and centered on a flange of the stator-side housing.Type: ApplicationFiled: October 22, 2014Publication date: April 30, 2015Inventors: Emil ASCHENBRUCK, Jaman EL MASALME, Michael BLASWICH
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Publication number: 20120144834Abstract: A gas turbine combustion chamber has a housing (1), a flame tube (2) received therein, and a perforated plate (3) which at least partially surrounds the latter and which is fastened at both of its end faces (3.1, 3.2) to the housing.Type: ApplicationFiled: July 20, 2010Publication date: June 14, 2012Applicant: Man Diesel & Turbo SeInventors: Jaman El Masalme, Emil Aschenbruck, Reiner Brinkmann
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Publication number: 20110265483Abstract: Combustor for a turbine, and gas turbine outfitted with a combustor. The combustor has a housing in which an air collecting chamber, a combustion antechamber, and a combustion chamber are formed. A combustor head plate is arranged in the housing so that the combustor head plate separates the combustion antechamber from the combustion chamber. A baffle plate is arranged in the combustion antechamber so that the baffle plate divides the combustion antechamber into a first sub-chamber adjoining an air supply fluidically connected with the air collecting chamber and a second sub-chamber adjoining the combustor head plate. Wherein baffle plate has a plurality of through-passages that fluidically connect the first sub-chamber with the second sub-chamber so that air that has flowed into the first sub-chamber from the air collecting chamber via the air supply can flow into the second sub-chamber via the through-passages and to a back surface of the combustor head plate facing the second sub-chamber.Type: ApplicationFiled: October 27, 2010Publication date: November 3, 2011Applicant: MAN Diesel & Turbo SEInventors: Frank REISS, Jaman El Masalme
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Publication number: 20110094240Abstract: A swirl generator for injecting fuel into a gas turbine by injection of the fuel into a channel of the swirl generator of the gas turbine. The fuel injection is predetermined by the arrangement of a fuel injecting insert in a swirl generator segment.Type: ApplicationFiled: October 22, 2010Publication date: April 28, 2011Applicant: MAN Diesel & Turbo SEInventors: Holger HUITENGA, Jaman El Masalme, Emil Aschenbruck, Reiner Brinkmann
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Publication number: 20100247005Abstract: A sealing segment for sealingly connecting two structural components parts which are movable relative to one another, with two sealing bodies which are connected to one another by a web and which can be arranged in recesses of the structural component parts in an articulated manner, and a sealing segment arrangement with a plurality of sealing segments of this type, and a flow machine with a sealing segment arrangement of this type.Type: ApplicationFiled: November 3, 2008Publication date: September 30, 2010Inventors: Emil Aschenbruck, Michael Blaswich, Jaman El Masalme, Frank Reiss