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公开(公告)号：US11927150B2
公开(公告)日：2024-03-12
申请号：US17874825
申请日：2022-07-27
申请人： ROHR, INC.
发明人： Timothy Gormley
CPC分类号： F02K1/763 , F02C7/32 , F02K1/09 , F02K1/15 , F02K1/72 , F02K1/766 , F02K3/04 , F05D2260/4031 , F05D2260/53
摘要： A nacelle may comprise a fixed structure and a translating structure configured to translate relative to the fixed structure. A first drive system may be operationally coupled to the translating structure. The drive system may comprise a primary actuator coupled to the fixed structure and including a primary rod and a primary gear rotationally coupled to the primary rod, a torque shaft rotationally coupled to the primary gear, and a secondary actuator operationally coupled to the primary actuator via the torque shaft.
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公开(公告)号：US20230213002A1
公开(公告)日：2023-07-06
申请号：US17566175
申请日：2021-12-30
申请人： Rohr, Inc.
发明人： Timothy Gormley
CPC分类号： F02K1/62 , F02K1/123 , F05D2250/12 , F05D2260/57
摘要： 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.
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公开(公告)号：US20230175457A1
公开(公告)日：2023-06-08
申请号：US17542926
申请日：2021-12-06
申请人： Rohr, Inc.
发明人： Timothy Gormley
IPC分类号： F02K1/12
CPC分类号： F02K1/1207 , F05D2220/32
摘要： A variable area nozzle assembly for a gas turbine engine includes a nozzle disposed about a nozzle centerline and a fixed ring radially surrounding the nozzle. The nozzle includes a radially outer surface and a radially inner surface. The radially inner surface defines an outlet cross-sectional area of the nozzle. The nozzle is movable relative to the nozzle centerline between a first position of the radially inner surface defining a maximum area of the outlet cross-sectional area and a second position of the radially inner surface defining a minimum area of the outlet cross-sectional area. With the nozzle in the first position, the radially outer surface contacts the fixed ring. With the nozzle in the second position, the radially outer surface is spaced from the fixed ring.
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公开(公告)号：US20230003175A1
公开(公告)日：2023-01-05
申请号：US17720519
申请日：2022-04-14
申请人： ROHR, INC.
发明人： Timothy Gormley , Imad D. Ghandour
IPC分类号： F02K1/76
摘要： A method for deploying a thrust reverser includes translating a carrier along a track, transferring a first load between the carrier and a first reverser door in response to the carrier translating along the track, rotating the first reverser door between a closed position and an open position in response to the carrier translating along the track, transferring a second load between the carrier and a deployable fairing in response to the carrier translating along the track, and rotating the deployable fairing between a stowed position and a deployed position in response to the carrier translating along the track.
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公开(公告)号：US11300077B2
公开(公告)日：2022-04-12
申请号：US16560716
申请日：2019-09-04
申请人： ROHR, INC
发明人： Timothy Gormley
摘要： 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.
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公开(公告)号：US11286879B2
公开(公告)日：2022-03-29
申请号：US16025239
申请日：2018-07-02
申请人： ROHR, INC.
发明人： Timothy Gormley
摘要： The present disclosure provides a thrust reverser comprising a stationary structure defining an annular body with a centerline, a first reverser door pivotally coupled to the stationary structure by a pair of first reverser door hinges, a first reverser door hinge axis extending through the first reverser door hinges and positioned at a first angle relative to a centerline, and a second reverser door pivotally coupled to the stationary structure by a pair of second reverser door hinges, a second hinge line axis extending through the second reverser door hinges and positioned at a second angle relative to the centerline.
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公开(公告)号：US20220065195A1
公开(公告)日：2022-03-03
申请号：US17307603
申请日：2021-05-04
申请人： Rohr, Inc.
发明人： Timothy Gormley
摘要： An assembly is provided for an aircraft propulsion system. This assembly includes a first actuator, a second actuator and a linkage system. The linkage system is configured to transfer torque between the first actuator and the second actuator. The linkage system includes a first linkage shaft, a second linkage shaft and a gearbox. The first linkage shaft has a first centerline. The second linkage shaft has a second centerline offset from the first centerline. The gearbox is coupled to and is between the first linkage shaft and the second linkage shaft.
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公开(公告)号：US20210040915A1
公开(公告)日：2021-02-11
申请号：US16532070
申请日：2019-08-05
申请人： Rohr, Inc.
发明人： Timothy Gormley
IPC分类号： F02K1/76
摘要： A nacelle system having a translating structure is disclosed. In various embodiments, the system includes a fixed structure; a thrust reverser having a translating sleeve configured to translate relative to the fixed structure and in response to a first hydraulic system; and a variable area fan nozzle having a translating nozzle configured to translate relative to the translating sleeve and in response to a second hydraulic system. In various embodiments, the first hydraulic system and the second hydraulic system include a primary hydraulic actuator, the primary hydraulic actuator having a primary hydraulic fluid end and a primary gaseous fluid end; a secondary hydraulic actuator having a secondary hydraulic fluid end and a secondary gaseous fluid end; and a hydraulic supply line configured to fluidly couple the primary hydraulic fluid end of the primary hydraulic actuator to the secondary hydraulic fluid end of the secondary hydraulic actuator.
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公开(公告)号：US20200317320A1
公开(公告)日：2020-10-08
申请号：US16377669
申请日：2019-04-08
申请人： Rohr, Inc.
发明人： Timothy Gormley
摘要： A latch arrangement for a door includes a plurality of steps disposed at an interior of the door. One of the plurality of steps is rotatable relative to the door between a first position and a second position. The door is movable between a closed position and an open position. A latch is in operable communication with the rotatable step. The latch is engageable with a latch receiver to lock the door in the closed position in response to the rotatable step being in the first position. The latch is disengageable from the latch receiver when the step is in the second position thereby allowing the door to move to the open position.
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公开(公告)号：US10655564B2
公开(公告)日：2020-05-19
申请号：US15154516
申请日：2016-05-13
申请人： Rohr, Inc.
发明人： Timothy Gormley
摘要： An assembly is provided for an aircraft propulsion system with an axial centerline. This assembly includes a nacelle structure and a thrust reverser system. The nacelle structure includes a fan cowl, where a forward cavity extends axially into the nacelle structure from an aft end of the fan cowl. The thrust reverser system includes a sleeve, a cascade structure, a blocker door and a linkage. The sleeve is configured to translate axially along the centerline and relative to the nacelle structure between a forward stowed position and an aft deployed position. The cascade structure, the blocker door and the linkage are at least partially within the forward cavity when the sleeve is in the forward stowed position. The cascade structure is fixedly attached to the sleeve. The linkage extends between and is pivotally attached to the cascade structure and the blocker door.
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