Patents by Inventor Michael J. WHITTLE
Michael J. WHITTLE 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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Publication number: 20240426251Abstract: A highly efficient gas turbine engine is provided. The fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.Type: ApplicationFiled: September 5, 2024Publication date: December 26, 2024Applicant: ROLLS-ROYCE plcInventors: Pascal DUNNING, Roderick M. TOWNES, Michael J. WHITTLE
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Publication number: 20240191657Abstract: A highly efficient gas turbine engine is a system wherein the fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.Type: ApplicationFiled: February 21, 2024Publication date: June 13, 2024Applicant: ROLLS-ROYCE PLCInventors: Roderick M. TOWNES, Michael J WHITTLE, Pascal DUNNING
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Publication number: 20230272752Abstract: A highly efficient gas turbine engine is provided. The fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.Type: ApplicationFiled: April 20, 2023Publication date: August 31, 2023Applicant: ROLLS-ROYCE plcInventors: Pascal DUNNING, Roderick M. TOWNES, Michael J. WHITTLE
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Publication number: 20220307448Abstract: A highly efficient gas turbine engine is provided. The fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.Type: ApplicationFiled: January 27, 2022Publication date: September 29, 2022Applicant: ROLLS-ROYCE plcInventors: Roderick M. TOWNES, Pascal DUNNING, Michael J. WHITTLE
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Publication number: 20220268216Abstract: A highly efficient gas turbine engine is a system wherein the fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.Type: ApplicationFiled: April 28, 2022Publication date: August 25, 2022Applicant: ROLLS-ROYCE plcInventors: Roderick M TOWNES, Michael J WHITTLE, Pascal DUNNING
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Publication number: 20210310408Abstract: A highly efficient gas turbine engine includes the fan of the gas turbine engine driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.Type: ApplicationFiled: June 11, 2021Publication date: October 7, 2021Applicant: ROLLS-ROYCE plcInventors: Pascal DUNNING, Michael J. WHITTLE, Roderick M. TOWNES
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Publication number: 20210207528Abstract: A highly efficient gas turbine engine is provided. The fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.Type: ApplicationFiled: March 23, 2021Publication date: July 8, 2021Applicant: ROLLS-ROYCE PLCInventors: Pascal DUNNING, Roderick M. TOWNES, Michael J. WHITTLE
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Publication number: 20200049065Abstract: A gas turbine engine is highly efficient. The fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.Type: ApplicationFiled: May 14, 2019Publication date: February 13, 2020Applicant: ROLLS-ROYCE plcInventors: Michael J WHITTLE, Roderick M TOWNES, Pascal DUNNING
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Publication number: 20200049064Abstract: A highly efficient gas turbine engine includes the fan of the gas turbine engine driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.Type: ApplicationFiled: May 14, 2019Publication date: February 13, 2020Applicant: ROLLS-ROYCE plcInventors: Pascal DUNNING, Michael J. WHITTLE, Roderick M. TOWNES
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Publication number: 20200049070Abstract: A highly efficient gas turbine engine is a system wherein the fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.Type: ApplicationFiled: May 14, 2019Publication date: February 13, 2020Applicant: ROLLS-ROYCE plcInventors: Roderick M. TOWNES, Michael J. WHITTLE, Pascal DUNNING
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Publication number: 20200049063Abstract: A highly efficient gas turbine engine includes a fan which is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.Type: ApplicationFiled: April 30, 2019Publication date: February 13, 2020Applicant: ROLLS-ROYCE PLCInventors: Michael J WHITTLE, Pascal DUNNING, Roderick M TOWNES
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Publication number: 20200049067Abstract: A highly efficient gas turbine engine has a fan that is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.Type: ApplicationFiled: May 28, 2019Publication date: February 13, 2020Applicant: ROLLS-ROYCE plcInventors: Roderick M TOWNES, Pascal DUNNING, Michael J WHITTLE
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Publication number: 20200049072Abstract: A highly efficient gas turbine engine includes a fan which is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, which results in efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.Type: ApplicationFiled: July 31, 2019Publication date: February 13, 2020Applicant: ROLLS-ROYCE PLCInventors: Michael J. WHITTLE, Pascal DUNNING, Roderick M. TOWNES
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Publication number: 20200049021Abstract: A highly efficient gas turbine engine includes a fan driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.Type: ApplicationFiled: May 28, 2019Publication date: February 13, 2020Applicant: ROLLS-ROYCE plcInventors: Roderick M. TOWNES, Pascal DUNNING, Michael J. WHITTLE
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Publication number: 20200049104Abstract: A highly efficient gas turbine engine is provided. The fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.Type: ApplicationFiled: May 28, 2019Publication date: February 13, 2020Applicant: ROLLS-ROYCE plcInventors: Roderick M. TOWNES, Pascal DUNNING, Michael J. WHITTLE
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Publication number: 20200049066Abstract: A highly efficient gas turbine engine is provided. The fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.Type: ApplicationFiled: May 14, 2019Publication date: February 13, 2020Applicant: ROLLS-ROYCE plcInventors: Pascal DUNNING, Roderick M. TOWNES, Michael J WHITTLE
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Publication number: 20190211704Abstract: A gas turbine engine, comprising: a component having a gas path wall with a gas path facing surface and an opposing air cooled surface, wherein the air cooled surface receives a supply of cooling air; a chamber which holds the cooling air for delivery to the air cooled surface; a test sample mounted within the chamber so as to be located in the supply of cooling air which is delivered to the air cooled surface, wherein the test sample is constructed of the same material as the gas path wall of the component.Type: ApplicationFiled: December 13, 2018Publication date: July 11, 2019Applicant: ROLLS-ROYCE plcInventor: Michael J. WHITTLE