-
公开(公告)号：US12203428B2
公开(公告)日：2025-01-21
申请号：US17893555
申请日：2022-08-23
Applicant: Woodward, Inc.
Inventor： Matthew Polley , Dragan Micic , Kamran Eftekhari Shahroudi , Joseph Thomas Kopecek , James Cale
Abstract: The subject matter of this specification can be embodied in, among other things, a system that includes a flexible structure, a power inverter, a first electromechanical device configured to urge movement of a first portion of the flexible structure based on power received from the power inverter, a second electromechanical device configured to urge movement of a second portion of the flexible structure based on power received from the power inverter, a feedback sensor configured to provide a feedback signal indicative of alignment between the first portion and the second portion, and a controller configured to control operation of at least one of the first electromechanical device and the second electromechanical device based on the feedback signal.
-
公开(公告)号：US11867135B1
公开(公告)日：2024-01-09
申请号：US17944798
申请日：2022-09-14
Applicant: Raytheon Technologies Corporation
Inventor： Michael Murphy
CPC classification number: F02K1/1207 , F02K1/004 , F02K1/40 , F02K1/625 , F05D2220/32
Abstract: An assembly is provided for an aircraft. This aircraft assembly includes a powerplant. The powerplant includes a gas turbine engine, an exhaust nozzle and a flowpath extending from the gas turbine engine to the exhaust nozzle. The exhaust nozzle is movable between a first position and a second position. The exhaust nozzle is configured to exhaust combustion products, received through the flowpath from the gas turbine engine, when the exhaust nozzle is in the first position. The exhaust nozzle is configured to block flow of the combustion products through the flowpath when the exhaust nozzle is in the second position.
-
公开(公告)号：US11859578B2
公开(公告)日：2024-01-02
申请号：US17716477
申请日：2022-04-08
Applicant: Rohr, Inc.
CPC classification number: F02K1/625 , F02K1/72 , F05D2240/129
Abstract: A first cascade segment of a thrust reverser system has a first cascade segment flow area and is associated with a first lateral sector. A second cascade segment has a second cascade segment flow area and is associated with a second lateral sector. The second cascade segment flow area may be at least 1.2 times the first cascade segment flow area. The first lateral sector has a first leakage flow area and a first total flow area that is equal to a sum of at least the first cascade segment flow area and the first leakage flow area. The second lateral sector has a second leakage flow area and a second total flow area that is equal to a sum of at least the second cascade segment flow area and the second leakage flow area. The second total flow area may be within 10% of the first total flow area.
-
公开(公告)号：US11773806B2
公开(公告)日：2023-10-03
申请号：US17870255
申请日：2022-07-21
Applicant: Airbus Operations (S.A.S.)
Inventor： Thierry Gaches , Laurent Cazeaux
Abstract: An assembly includes a structure with 6 o'clock and 12 o'clock beams and front and rear curved beams, in which the 12 o'clock beam is mounted to be able to rotate on a pylon of an aircraft between a closed position and a raised position, a fan cowl fixed to the structure, a thrust reverser with a rear cowl and that is able to move in translation along the 6 o'clock and 12 o'clock beams between a forward position and a backward position, cascades fixed to the thrust reverser, and a mover for moving the thrust reverser. With such an arrangement, the fan cowl and the thrust reverser are fixed to the same structure, and it is this structure that is hinged to the pylon.
-
公开(公告)号：US20230213002A1
公开(公告)日：2023-07-06
申请号：US17566175
申请日：2021-12-30
Applicant: Rohr, Inc.
Inventor： Timothy Gormley
CPC classification number: F02K1/62 , F02K1/123 , F05D2250/12 , F05D2260/57
Abstract: A variable area nozzle assembly includes a fixed structure surrounding an exhaust duct extending along a nozzle axis. The fixed structure defines an exhaust duct outlet of the exhaust duct. The fixed structure includes a first side beam and a second side beam. Each of the first side beam and the second side beam extend in a direction axially aft from the exhaust duct outlet. Each of an upper thrust reverser door and a lower thrust reverser door are pivotably mounted to the first side beam and the second side beam at a first axial position. An upper panel and a lower panel are pivotably mounted to the upper thrust reverser door and the lower thrust reverser door, respectively, at a second axial position located axially forward of the first axial position. The upper panel and the lower panel define a nozzle outlet cross-sectional area therebetween.
-
Patent Agency Ranking
公开(公告)号：US11577849B2
公开(公告)日：2023-02-14
申请号：US17181577
申请日：2021-02-22
Applicant: Airbus Operations SAS
Inventor： Fabien Menou , Julie Cazalis
Abstract: A nacelle having a fan casing, a cowl that movable between an advanced position and a retracted position that opens an opening between a bypass duct and the outside, deflectors secured to the mobile cowl, wherein, in the advanced position, they are around the fan casing and wherein, in the retracted position, they are across the opening, and a fan ramp with a mounting base and flaps that are able to rotate on the mounting base between a stowed position and a deployed position. For each flap, the fan ramp has a return element that urges the flap) into the deployed position, and the deflectors have a stop in contact with the flap when the mobile cowl passes from the retracted position to the advanced position. Thus, in the advanced position, the flaps are folded back and their bulk is reduced.
-
公开(公告)号：US20230039569A1
公开(公告)日：2023-02-09
申请号：US17790684
申请日：2020-12-18
Applicant: SAFRAN NACELLES
Inventor： Sebastien Laurent Marie PASCAL , Patrick GONIDEC , Alexandre PHI , Paul FERREY
Abstract: A thrust reverser including doors and at least one flexible deflector obstructing a lateral opening of the thrust reverser when the doors are open. Such a deflector allows better controlling the airflows in thrust reverser configuration and maximizing the counter-thrust force.
-
公开(公告)号：US11408368B2
公开(公告)日：2022-08-09
申请号：US16836080
申请日：2020-03-31
Inventor： David L. Sutterfield , Todd S. Taylor , Jack D. Petty , Andrew Sanderson , Bryan H. Lerg
Abstract: A propulsion unit includes a gas turbine engine arranged along an axis and an exhaust system coupled to the gas turbine engine. The gas turbine engine includes an engine core configured to discharge a core flow and a fan configured to be driven by the engine core to discharge a bypass flow. The exhaust system receives the mixed bypass and core flows from the gas turbine engine.
-
公开(公告)号：US11300077B2
公开(公告)日：2022-04-12
申请号：US16560716
申请日：2019-09-04
Applicant: ROHR, INC
Inventor： Timothy Gormley
Abstract: A thrust reverser may include a frame, an actuation arrangement, a reverser door pivotally coupled to the frame, and a deployable fairing pivotally coupled to the frame, wherein the deployable fairing is configured to move away from a central axis of the thrust reverser to provide clearance for one of more thrust reverser pivot doors to rotate into a deployed position.
-
公开(公告)号：US11286878B2
公开(公告)日：2022-03-29
申请号：US16836065
申请日：2020-03-31
Inventor： Todd S. Taylor , David L. Sutterfield , Jack D. Petty , Andrew Sanderson , Bryan H. Lerg
Abstract: A propulsion unit includes a gas turbine engine arranged along an axis and an exhaust system coupled to the gas turbine engine. The gas turbine engine includes an engine core configured to discharge a core flow and a fan configured to be driven by the engine core to discharge a bypass flow. The exhaust system receives the mixed bypass and core flows from the gas turbine engine.
-
-
-
-
-
-
-
-
-
Search Results
292
records
(took 0.019 seconds)
