Patents by Inventor Niklas Jansson
Niklas Jansson 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: 11946399Abstract: A temperature sensing unit includes a temperature sensor and a substrate including a first region and a second region. The temperature sensor is arranged in the second region. The second region extends away from the first region.Type: GrantFiled: December 29, 2020Date of Patent: April 2, 2024Assignee: TE Connectivity Norge ASInventors: Niklas Jansson, Bjornar Berge Lie, Harald Aadland, Oyvind Rortveit
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Patent number: 11300439Abstract: A sensor assembly for measuring a level of a liquid includes a measuring section through which a measuring current runs during operation of the sensor assembly and a temperature compensation section. The temperature compensation section compensates a temperature dependent variation of the measuring current within a predetermined operational temperature range.Type: GrantFiled: June 17, 2020Date of Patent: April 12, 2022Assignee: TE CONNECTIVITY NORGE ASInventor: Niklas Jansson
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Publication number: 20210115833Abstract: A temperature sensing unit includes a temperature sensor and a substrate including a first region and a second region. The temperature sensor is arranged in the second region. The second region extends away from the first region.Type: ApplicationFiled: December 29, 2020Publication date: April 22, 2021Applicant: TE Connectivity Norge AGInventors: Niklas Jansson, Bjornar Berge Lie, Harald Aadland, Oyvind Rortveit
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Publication number: 20200400484Abstract: A sensor assembly for measuring a level of a liquid includes a measuring section through which a measuring current runs during operation of the sensor assembly and a temperature compensation section. The temperature compensation section compensates a temperature dependent variation of the measuring current within a predetermined operational temperature range.Type: ApplicationFiled: June 17, 2020Publication date: December 24, 2020Applicant: TE Connectivity Norge ASInventor: Niklas Jansson
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Patent number: 10806032Abstract: An electronic system for a fluid property sensor comprises a fluid printed circuit board adapted to analyze a property of a fluid, an external connector, and an intermediate printed circuit board. The intermediate printed circuit board is electrically connected between the fluid printed circuit board and the external connector.Type: GrantFiled: November 20, 2018Date of Patent: October 13, 2020Assignees: TE CONNECTIVITY NORGE AS, MEAS FRANCEInventors: Maciej Ziemak, Ion Grozea, Marcin Rusak, Bengt Eliassen, Conrad Judersleben, Jose Fernandez, Niklas Jansson, Rafael Ferrer Ruiz
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Publication number: 20190159341Abstract: An electronic system for a fluid property sensor comprises a fluid printed circuit board adapted to analyze a property of a fluid, an external connector, and an intermediate printed circuit board. The intermediate printed circuit board is electrically connected between the fluid printed circuit board and the external connector.Type: ApplicationFiled: November 20, 2018Publication date: May 23, 2019Applicants: Wema System AS, MEAS FranceInventors: Maciej Ziemak, Ion Grozea, Marcin Rusak, Bengt Eliassen, Conrad Judersleben, Jose Fernandez, Niklas Jansson, Rafael Ferrer Ruiz
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Patent number: 9670789Abstract: A composite guide vane for a gas turbine structure is adapted to extend in a guide vane direction from a first housing towards a second housing of the gas turbine structure. The guide vane includes a guide vane length in the guide vane direction and the guide vane includes a first attachment portion with at least one first opening for attachment of the guide vane to the first housing. The first opening extends in a first opening direction which forms an angle with the guide vane direction. The guide vane includes a cover portion including a first material and a core portion which is at least partially enclosed by the cover portion.Type: GrantFiled: March 14, 2011Date of Patent: June 6, 2017Assignee: GKN Aerospace Sweden ABInventors: Niklas Jansson, Robert Reimers
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Patent number: 9435215Abstract: A gas turbine structure includes a guide vane. The gas turbine structure (further includes a first housing and a second housing and the guide vane extends from the first housing to the second housing. The guide vane includes a leading edge and a trailing edge and the guide vane extends from the leading edge to the trailing edge along a mean camber line. The guide vane includes a first attachment structure, a first fastening arrangement and a second fastening arrangement. Moreover, the first attachment structure includes a stiffening member extending over at least a portion of a circumference of the first housing. Furthermore, the stiffening member includes a stiffening member center point as measured along the mean camber line.Type: GrantFiled: March 14, 2011Date of Patent: September 6, 2016Assignee: GKN Aerospace Sweden ABInventors: Niklas Jansson, Robert Reimers
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Publication number: 20140294579Abstract: A composite guide vane for a gas turbine structure is adapted to extend in a guide vane direction from a first housing towards a second housing of the gas turbine structure. The guide vane includes a guide vane length in the guide vane direction and the guide vane includes a first attachment portion with at least one first opening for attachment of the guide vane to the first housing. The first opening extends in a first opening direction which forms an angle with the guide vane direction. The guide vane includes a cover portion including a first material and a core portion which is at least partially enclosed by the cover portion.Type: ApplicationFiled: March 14, 2011Publication date: October 2, 2014Applicant: GKN AEROSPACE SWEDEN ABInventors: Niklas Jansson, Robert Reimers
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Patent number: 8757919Abstract: A component includes a first member, a second member and a device for fastening the first member to the second member. A first hole extends through a portion of the first member and a second hole extends through a portion of the second member. The first member and the second member are positioned such that the first hole and the second hole coincide. The fastening device includes an elongated fastening element arranged in the coinciding holes and a bushing arrangement arranged around the fastening element and adapted to establish a load transmission path between the first member and the second member. A first part of the bushing arrangement is arranged such that an inner surface thereof is positioned at a distance from an exterior surface of the fastening element for establishing a first load transmission path via the bushing arrangement and bypassing the fastening element in a first load condition.Type: GrantFiled: August 29, 2008Date of Patent: June 24, 2014Assignee: Volvo Aero CorporationInventors: Rickard Samuelsson, Niklas Jansson
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Publication number: 20140161605Abstract: A gas turbine structure includes a guide vane. The gas turbine structure (further includes a first housing and a second housing and the guide vane extends from the first housing to the second housing. The guide vane includes a leading edge and a trailing edge and the guide vane extends from the leading edge to the trailing edge along a mean camber line. The guide vane includes a first attachment structure, a first fastening arrangement and a second fastening arrangement. Moreover, the first attachment structure includes a stiffening member extending over at least a portion of a circumference of the first housing. Furthermore, the stiffening member includes a stiffening member center point as measured along the mean camber line.Type: ApplicationFiled: March 14, 2011Publication date: June 12, 2014Inventors: Niklas Jansson, Robert Reimers
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Patent number: 8459942Abstract: A gas turbine engine component is provided including at least one ring element, and a plurality of circumferentially spaced load carrying vanes extending in a radial direction of the ring element. The load carrying vanes have an internal structure with an anisotropic load carrying property, and the internal structure is configured so that a main load carrying direction is in parallel with the extension direction of the load carrying vane. The component includes a stiffening structure bridging the distance between at least two adjacent load carrying vanes in the circumferential direction of the ring element, and the at least two adjacent load carrying vanes are attached to the stiffening structure.Type: GrantFiled: March 28, 2008Date of Patent: June 11, 2013Assignee: Volvo Aero CorporationInventors: Anders Sjunnesson, Niklas Jansson, Robert Reimers, Rickard Samuelsson
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Publication number: 20110299917Abstract: A component includes a first member, a second member and a device for fastening the first member to the second member. A first hole extends through a portion of the first member and a second hole extends through a portion of the second member. The first member and the second member are positioned such that the first hole and the second hole coincide. The fastening device includes an elongated fastening element arranged in the coinciding holes and a bushing arrangement arranged around the fastening element and adapted to establish a load transmission path between the first member and the second member. A first part of the bushing arrangement is arranged such that an inner surface thereof is positioned at a distance from an exterior surface of the fastening element for establishing a first load transmission path via the bushing arrangement and bypassing the fastening element in a first load condition.Type: ApplicationFiled: August 29, 2008Publication date: December 8, 2011Applicant: VOLVO AERO CORPORATIONInventors: Rickard Samuelsson, Niklas Jansson
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Publication number: 20100111685Abstract: A gas turbine engine component is provided including at least one ring element, and a plurality of circumferentially spaced load carrying vanes extending in a radial direction of the ring element. The load carrying vanes have an internal structure with an anisotropic load carrying property, and the internal structure is configured so that a main load carrying direction is in parallel with the extension direction of the load carrying vane. The component includes a stiffening structure bridging the distance between at least two adjacent load carrying vanes in the circumferential direction of the ring element, and the at least two adjacent load carrying vanes are attached to the stiffening structure.Type: ApplicationFiled: March 28, 2008Publication date: May 6, 2010Applicant: Volvo Aero CorporationInventors: Anders Sjunnesson, Niklas Jansson, Robert Reimers, Rickard Samuelsson