11227 patents
Page 7 of 562
Utility
Systems and methods for variable microchannel combustor liner cooling
2 Jan 24
In accordance with an embodiment of the disclosure, a system includes a combustor liner disposed about a combustion chamber of a combustor of a gas turbine system.
Scott Robert Simmons, Ronald James Chila
Filed: 25 Feb 19
Utility
Ceramic composite combustor dome and liners
2 Jan 24
A combustor for a turbomachine engine includes a dome made of a ceramic matrix composite (CMC) material, the dome being secured within a support structure.
Ryan Christopher Jones, Shai Birmaher, Nicholas John Bloom, Daniel J. Kirtley, Gerardo Antonio Salazar Lois, Anquan Wang, Trevor James Hahm
Filed: 15 Oct 21
Utility
Gas turbine combustion section having an integrated fuel cell assembly
2 Jan 24
A combustion section defines an axial direction, a radial direction, and a circumferential direction.
Seung-Hyuck Hong, Richard L. Hart, Honggang Wang, Anil Raj Duggal, Michael Anthony Benjamin, Andrew Wickersham, Narendra Digamber Joshi
Filed: 10 Nov 22
Utility
Combustor chamber mesh structure
2 Jan 24
A combustor includes an inner liner and an outer liner defining a combustion chamber.
Ravindra Shankar Ganiger, Hiranya Nath, Daniel J. Kirtley
Filed: 13 Sep 22
Utility
Combustor with a dilution hole structure
2 Jan 24
A combustor including a skeleton structure.
Ravindra Shankar Ganiger, Hiranya Nath
Filed: 13 Sep 22
Utility
Detecting the spoofing of a signal
2 Jan 24
An aircraft and non-transitory computer-readable medium for detecting the spoofing of a signal from a satellite in orbit.
Stefan Alexander Schwindt
Filed: 16 Sep 22
Utility
System and method for controlling time dilation in time-sensitive networks
2 Jan 24
A system and method determine a clock drift and a clock variance of each node in plural nodes of a time-sensitive Ethernet network.
Stephen Francis Bush, Guillaume Mantelet
Filed: 22 Dec 20
Utility
Heat sink assemblies for transient cooling
2 Jan 24
A heat sink assembly for use with at least one heat-emitting component where the heat sink assembly includes a first phase change material conductively coupled to the at least one heat-emitting component and changing phase at a first temperature and a second phase change material conductively coupled to the first phase change material and changing phase at a second temperature, which is greater than the first temperature.
Michel Engelhardt, Paul Otto Stehlik, Judd Everett Swanson
Filed: 15 Oct 19
Utility
Thermal management system
2 Jan 24
A thermal management system including a fluid flow mechanism.
Kevin Edward Hinderliter
Filed: 13 May 21
Utility
Systems and Methods of Alignment Control for Neuromodulation Delivery System
28 Dec 23
The present discussion relates to structures and devices to facilitate application of an ultrasound therapy beam to a target anatomic region in a replicable manner.
David Andrew Shoudy, Weston Blaine Griffin, Radhika Madhavan, Jeffrey Michael Ashe
Filed: 28 Jun 22
Utility
System and Method for Forming Slots In a Coating Present on a Component
28 Dec 23
A system for forming slots in a coating present on a component includes an electromagnetic radiation beam emitting device having a base, an arm coupled to the base, and a scan head coupled to the arm.
Hongqiang Chen, Hrishikesh Keshavan, Curtis Alan Johnson, Jaewon Moon
Filed: 28 Jun 22
Utility
Methods and Systems for Manipulating an Additive Build Assembly
28 Dec 23
An additive manufacturing system includes an additive manufacturing unit that includes a housing for additively processing a powder material along a build direction into a build assembly.
Eric Olen Lambert, Archie L. Swanner, JR., James J. Murray, Maxwell E. Miller
Filed: 28 Jun 22
Utility
Method of Manufacturing Wind Turbine Blade with Core Member and Wind Turbine Blade with Structural Member
28 Dec 23
The present invention relates to a method of manufacturing a wind turbine blade (10), comprising the steps of placing a fibre lay-up including one or more fibre layers on the mould surface of a blade mould (60), arranging a load-bearing structure (45) and a core member (62) on the fibre lay-up such that the core member (62) is arranged between the load-bearing structure (45) and the leading edge (18) and/or between the load-bearing structure (45) and the trailing edge (20), and infusing resin into the blade mould to impregnate the fibre lay-up.
Klavs JESPERSEN, Lars NIELSEN
Filed: 16 Nov 21
Utility
Aircraft Engine
28 Dec 23
A method of operating an aircraft engine coupled to a wing of an aircraft including: setting a pitch of a plurality of rotor blades of a rotor assembly of the aircraft engine at non-uniform pitch angles along a circumferential direction of the aircraft engine such that the plurality of rotor blades define a first pitch at a first position and a second pitch at a second position, wherein the second position is 180 degrees offset from the first position, and wherein the first pitch is different from the second pitch.
Brendan Michael Freely, Kurt David Murrow, Michael James McMahon
Filed: 14 Sep 23
Utility
Advance Ratio for Single Unducted Rotor Engine
28 Dec 23
A method is provided of operating a single unducted rotor engine, the single unducted rotor engine comprising a single stage of unducted rotor blades.
Syed Arif Khalid, Andrew Breeze-Stringfellow
Filed: 14 Sep 23
Utility
Composite Components and Methods for Preventing Flow from Infiltrated Component During Re-infiltration
28 Dec 23
A method for modifying a composite component may include positioning a barrier segment between an infiltrated segment of the composite component and a green segment to form an assembly; and initiating an infiltration process.
Juan P. Borja, Daniel Gene Dunn, Jared Hogg Weaver, Anant Achyut Setlur
Filed: 28 Jun 22
Utility
Methods for Joining Ceramic Components to Form Unitary Ceramic Components
28 Dec 23
Methods for forming a unitary ceramic component are provided.
Jerome Geoffrey Magnant, Jared Hogg Weaver, Daniel Gene Dunn
Filed: 28 Jun 22
Utility
Cold Spray Duct for a Gas Turbine Engine
28 Dec 23
A component for a turbine engine may be formed by spraying particulate with a nozzle toward a substrate.
Apostolos Pavlos Karafillis, Eric Dean Jorgensen, Craig Douglas Young, Jonathan Harry Kerner, Leonardo Ajdelsztajn
Filed: 12 Sep 23
Utility
Seal Assemblies for Turbine Engines and Related Methods
28 Dec 23
A seal assembly for an aeronautical turbine engine includes a passive flow regulator.
Deepak Trivedi, Rahul Anil Bidkar, Bugra Han Ertas
Filed: 28 Jun 22
Utility
Compliant Shroud Designs with Variable Stiffness
28 Dec 23
Methods, apparatus, systems and articles of manufacture are disclosed.
Ravindra Shankar Ganiger, Praveen Sharma, Jeffrey D. Carnes, Herbert Chidsey Roberts
Filed: 8 Sep 23