公开(公告)号：US2834010A

公开(公告)日：1958-05-06

申请号：US52378855

申请日：1955-07-22

申请人： LUNDY MFG CORP

发明人： SIERADZKI HENRY J

IPC分类号： B64C13/42

CPC分类号： B64C13/42

公开(公告)号：US1834623A

公开(公告)日：1931-12-01

申请号：US45697530

申请日：1930-05-29

申请人： CLAIR JEROME LE ROY ST

发明人： CLAIR JEROME LE ROY ST

IPC分类号： B64C13/42

CPC分类号： B64C13/42

公开(公告)号：US11697490B2

公开(公告)日：2023-07-11

申请号：US17574835

申请日：2022-01-13

申请人： Goodrich Actuation Systems SAS

发明人： Karl Potier ,  Arnauld Hervieux ,  Sebastien Vandevoir

IPC分类号： B64C13/40 ,  B64C9/16 ,  B64C9/08 ,  B64C13/28 ,  B64C13/42

CPC分类号： B64C13/40 ,  B64C9/08 ,  B64C9/16 ,  B64C13/341 ,  B64C13/42

摘要： An actuation system for a control surface for an aircraft includes a first, second, third and fourth actuator, a first and second bell crank, and at least one push pull rod system. Each of the first and second bell cranks comprises a first and a second crank arm, the first and second crank arms intersect with and are joined to each other at an intersection, the first and second crank arms extend from the intersection at an angle to each other, the first bell crank is pivotally connected to the sub-structure by a first pivot extending through the first bell crank's intersection, and the second bell crank is pivotally connected to the sub-structure by a second pivot extending through the second bell crank's intersection.

公开(公告)号：US11506231B2

公开(公告)日：2022-11-22

申请号：US17283268

申请日：2018-10-08

申请人： SAAB AB

发明人： Magnus Landberg ,  Erik Agerbjörk

IPC分类号： F15B15/26 ,  B64C13/30 ,  B64C13/42 ,  B64C13/50 ,  F15B15/14

摘要： A method for controlling a control surface multirod actuator arrangement and the arrangement including: a first and a second multirod actuator configured to move or clamp around a first set of piston rods; a third multirod actuator configured to move or clamp around a second set of piston rods; a control unit configured to control motion of the first set of piston rods in a first motion mode and to control motion of the second set of piston rods in a second motion mode. Steps are moving at least one piston rod of first set of piston rods and/or clamping in parked position at least one piston rod of the second set of piston rods.

公开(公告)号：US20220228609A1

公开(公告)日：2022-07-21

申请号：US17614799

申请日：2020-05-26

申请人： Parker-Hannifin Corporation

发明人： Steven A. Krane ,  Dean R. Pollee ,  Scott N. Johns ,  David A. Scranton ,  Bernard J. Strehlow

IPC分类号： F15B20/00 ,  B64C13/42 ,  F15B3/00

摘要： A power transfer unit includes a first hydraulic circuit, a second hydraulic circuit fluidly connected to the first hydraulic circuit, a pump and motor assembly fluidly connected between the first hydraulic circuit and the second hydraulic circuit, an isolation valve arranged along the first hydraulic circuit and fluidly connected to an inlet of the pump and motor assembly. The isolation valve is movable between a closed position and an open position to prevent and enable high-pressure fluid flow to the inlet, respectively. An unloader valve is arranged along the second hydraulic circuit and fluidly connected to an outlet of the pump and motor assembly, and an orifice is arranged along the second hydraulic circuit and fluidly connected to the unloader valve to reduce back pressure in the second hydraulic circuit.

公开(公告)号：US11117651B2

公开(公告)日：2021-09-14

申请号：US16190935

申请日：2018-11-14

申请人： SAFRAN LANDING SYSTEMS UK LTD ,  SAFRAN LANDING SYSTEMS

发明人： Roy Evans ,  Olivier Collet ,  Jean Philippe Vaslin

IPC分类号： B64C25/24 ,  B64C25/22 ,  B64C25/26 ,  B64C13/42 ,  B64D45/00 ,  B64C25/20

摘要： An aircraft assembly, having: a reference component; a first component and a first actuator, the first actuator configured to move the first component relative to the reference component; a second component and a second actuator, the second actuator configured to move the second component relative to the reference component; a position sensor configured to measure a position of the first component, and to output a position value, the sensor being capable of outputting a plurality of non-zero position values; and a controller configured to control the movement of the second component by the second actuator based at least partially on the position value output by the position sensor.

公开(公告)号：US10800515B2

公开(公告)日：2020-10-13

申请号：US15964109

申请日：2018-04-27

申请人： Goodrich Actuation Systems SAS

发明人： Thomas Moulon ,  Quentin Ricard

IPC分类号： B64C13/28 ,  F16H25/20 ,  B64C13/42 ,  F16H25/24 ,  B64C5/16

摘要： A lower attachment system for a trimmable horizontal stabiliser actuator comprising: a ballnut for being disposed on a screwshaft of the actuator and forming a part of a primary load path of the lower attachment system; a trunnion connected to the ballnut and forming a part of the primary load path of the lower attachment system; a failsafe plate disposed about the trunnion and forming a part of a secondary load path; a secondary connection connected to the failsafe plate and forming a part of the secondary load path; a sheet plate attached to a first mounting point on the secondary connection and a second mounting point on the ballnut; and an adjustment mechanism provided with the sheet plate for adjusting the size or position of the sheet plate to adapt it to fit a distance between the first and second mounting points.

公开(公告)号：US20190112031A1

公开(公告)日：2019-04-18

申请号：US16224794

申请日：2018-12-19

申请人： The Boeing Company

发明人： Patrick J. McCormick ,  Neal V. Huynh ,  Timothy G. Overton ,  Alan Marx

IPC分类号： B64C13/42

CPC分类号： B64C13/504 ,  B64C13/42

摘要： A system of an aircraft includes a system pump and a booster pump. The system pump is configured to provide hydraulic fluid to the hydraulic system at a first working pressure. The booster pump is configured to supply hydraulic fluid to at least one boostable actuator at a second working pressure higher than the first working pressure. The boostable actuator is operatively coupled to and configured to actuate at least one flight control surface of an aircraft. The booster pump is configured as a high-pressure accumulator and an accumulator energizer, or as a hydraulic actuator pump and a variable speed motor.

公开(公告)号：US20180370616A1

公开(公告)日：2018-12-27

申请号：US16014298

申请日：2018-06-21

申请人： Airbus Operations Limited

发明人： George HOWELL ,  Nicholas CRANE

IPC分类号： B64C13/42 ,  B64C25/22 ,  B64C25/60

摘要： A hydraulic system 300 for an aircraft including a backup hydraulic pressure source 216 to provide hydraulic pressure to a brake 222 in the event of a failure condition of a primary hydraulic brake pressure source. The hydraulic system 300 also includes a landing gear backup system to provide hydraulic pressure to enable extension and/or retraction of landing gear 100. The backup hydraulic pressure source 216 is arranged to provide hydraulic pressure to the landing gear backup system in the event of a failure condition of a primary landing gear hydraulic pressure source.

公开(公告)号：US09797490B2

公开(公告)日：2017-10-24

申请号：US14671327

申请日：2015-03-27

申请人： Russel Hugh Marvin ,  David H. Leach

发明人： Russel Hugh Marvin ,  David H. Leach

IPC分类号： H01F27/24 ,  F16H25/20 ,  H02K9/22 ,  B64C13/28 ,  B64C13/42 ,  H02K7/06 ,  H02K16/00

CPC分类号： F16H25/205 ,  B64C13/28 ,  B64C13/42 ,  F16H2025/2075 ,  H02K7/06 ,  H02K9/22 ,  H02K16/00 ,  Y02T50/44 ,  Y10T74/18624

摘要： An actuator for moving a first component relative to a second component includes a first actuating mechanism secured to the first component and having a first motor, a first nut, and a first shaft secured to the first motor and the first nut such that the first nut is rotatable with the first motor. A second actuating mechanism is secured to the second component and has a second motor, a second nut, and a second shaft secured to the second motor and the second nut such that the second nut is rotatable with the second motor. A screw is threadably engaged with the first nut and the second nut such that rotation of at least one of the first motor and the second motor causes movement between the first and second nuts to move the second component relative to the first component.