-
公开(公告)号：US20180111680A1
公开(公告)日：2018-04-26
申请号：US15298959
申请日：2016-10-20
Applicant: Bell Helicopter Textron Inc.
Inventor： Carlos A. Fenny , Daniel B. Robertson , Kirk L. Groninga , Troy C. Schank
CPC classification number: B64C27/025 , B64C27/18 , B64C27/82 , B64C2027/8209 , B64C2027/8236 , B64D27/02 , B64D27/24 , B64D2027/026 , B64F1/362 , Y02T50/44 , Y02T50/64
Abstract: A rotorcraft capable of a hover mode and a forward cruise mode including a fuselage, a first electric propulsion system, a second electric propulsion system, and an electric power control unit to control power to the first and second electric propulsion systems in the hover and forward cruise modes. The first electric propulsion system is a tip jet cold flow system that imparts rotation on a pair of rotor blades disposed above a top surface of the fuselage, and a first electric motor configured to drive the tip jet cold flow system. The second electric propulsion system includes a propeller disposed in the rear of the fuselage and a second electric motor configured to drive the propeller.
-
公开(公告)号：US09951808B2
公开(公告)日：2018-04-24
申请号：US14481177
申请日：2014-09-09
Applicant: Bell Helicopter Textron Inc.
Inventor： Peter Q. Romano , Frank B. Stamps , Stephen R. Johnston , Peter H. Kintzinger
CPC classification number: F16C11/0695 , B64C27/001 , B64C2027/002 , F16C11/0614 , F16C11/0628 , F16C11/0652 , F16C2326/43
Abstract: A bearing assembly can include a top retainer; a middle retainer having a first concave spherical surface; a bottom retainer having a second concave spherical surface; a spherical ball member; and an elastomeric member coupled to the first concave spherical surface, the second concave spherical surface, and an outer surface of the spherical ball member.
-
公开(公告)号：US20180099738A1
公开(公告)日：2018-04-12
申请号：US15287467
申请日：2016-10-06
Applicant: Bell Helicopter Textron Inc.
Inventor： Brent Randal Achttien , Chyau J. Tzeng
CPC classification number: B64D31/04 , B64C13/30 , B64C29/0033 , G05G9/047
Abstract: The present invention includes a thrust control apparatus, method and kit for a tiltrotor craft comprising a thrust control handle; a first and a second bar connected to the thrust control handle and connected to a floor support; a first end of a transverse bar connected to the first bar; a linker connected to a second end of the transverse bar; and a crankbell connected to the floor support below the first and a second bars, wherein a first end of the crankbell is connected to the linker, wherein the thrust control handle has a substantially linear motion that controls engine thrust, and the crankbell transfers the substantially linear motion of the handle into a substantially perpendicular motion that engages an engine thrust control at a second end of the crankbell.
-
公开(公告)号：US20180087649A1
公开(公告)日：2018-03-29
申请号：US15709502
申请日：2017-09-20
Applicant: Bell Helicopter Textron Inc.
Inventor： Scott David Poster
CPC classification number: F16H57/0416 , B64C27/12 , B64D33/08 , F04D17/08 , F04D19/002 , F16H57/0475 , F16H57/0482 , F16H2057/02043
Abstract: A cooling apparatus includes one or more fans and one or more shafts. Each of the one or more fans includes a fan blade assembly. Each of the one or more shafts is operably coupled to an engine or a gearbox that rotates the shaft. Each fan blade assembly of the one or more fans is disposed on one of the shafts.
-
公开(公告)号：US20180087648A1
公开(公告)日：2018-03-29
申请号：US15354715
申请日：2016-11-17
Applicant: Bell Helicopter Textron Inc.
Inventor： Scott David Poster
CPC classification number: F16H57/0416 , B64C27/12 , B64C27/82 , F16H57/02 , F16H57/0404 , F16H57/0417 , F16H57/0435 , F16H57/0436 , F16H57/045
Abstract: The present invention includes a cooling system for a gearbox, the cooling system comprising: a pressurized housing in fluid communication with the gearbox configured to circulate a pressurized lubricant; and one or more cooling fins about the pressurized housing, wherein heat from the pressurized lubricant within the pressurized housing is actively convected through the one or more cooling fins.
-
Patent Agency Ranking
公开(公告)号：US20180087639A1
公开(公告)日：2018-03-29
申请号：US15709548
申请日：2017-09-20
Applicant: Bell Helicopter Textron Inc.
Inventor： Scott David Poster , Walter Riley , Gary Cope , Charles Hubert Speller, JR.
CPC classification number: F16H37/042 , B64C27/14 , B64D35/00 , F16H57/02 , F16H2057/02013 , F16H2057/02043 , F16H2702/00
Abstract: An engine reduction gear system includes at least two self-contained, independent engine reduction gearboxes, each capable of connecting to an aircraft engine. Each of the engine reduction gearboxes provides redundant, reduced speed to a main rotor gearbox via a shaft.
-
公开(公告)号：US09927322B2
公开(公告)日：2018-03-27
申请号：US14254117
申请日：2014-04-16
Applicant: Bell Helicopter Textron Inc.
Inventor： Robert Michael Laramee , Carlos Fenny
IPC: G01M3/28 , B64D45/00 , G01F23/00 , G01F23/292 , G01F23/296 , G01M3/32 , G01F23/02
CPC classification number: G01M3/2853 , B64D45/00 , B64D2045/0085 , G01F23/0007 , G01F23/02 , G01F23/292 , G01F23/296 , G01F23/2966 , G01M3/2869 , G01M3/3245
Abstract: A rotorcraft actuator monitoring system to monitor leakage past dynamic rotorcraft actuator seals of a rotorcraft actuator includes a body member and a fluid level indication housing attached to the body member. The body member is mounted to surround a dynamic rotorcraft actuator seal that seals fluid in a rotorcraft actuator, where the body member captures fluid that leaks past the dynamic rotorcraft actuator seal. The fluid level indication housing collects the fluid captured by the body member and indicates that a predetermined volume of fluid that leaked past the dynamic rotorcraft actuator seal has been collected.
-
公开(公告)号：US09925680B2
公开(公告)日：2018-03-27
申请号：US13914737
申请日：2013-06-11
Applicant: Bell Helicopter Textron Inc.
Inventor： Phillip A. Kendrick , Levi H. Armstrong
IPC: B29C70/54 , B32B3/12 , B26D1/157 , B26D7/01 , B29C69/00 , B29D99/00 , B29C53/60 , B26D1/10 , B26D3/16 , B26D1/08 , B29C65/00 , B32B37/14 , B29C70/30
CPC classification number: B26D1/157 , B26D1/08 , B26D1/10 , B26D3/167 , B26D7/01 , B29C53/60 , B29C66/543 , B29C69/001 , B29C70/30 , B29C70/545 , B29D99/0089 , B32B3/12 , B32B37/146 , Y10T83/04 , Y10T83/0405 , Y10T83/0524 , Y10T156/1026 , Y10T156/1059 , Y10T156/1066 , Y10T156/1079 , Y10T156/13 , Y10T156/1357
Abstract: A method of cutting a wafer of composite core from a bulk composite core includes stabilizing the bulk composite core with a fixture, the bulk composite core having a plurality of tube members. The method also includes cutting through each of the tube members to create the wafer while the bulk composite core is stabilized by the fixture.
-
公开(公告)号：US20180058119A1
公开(公告)日：2018-03-01
申请号：US15247235
申请日：2016-08-25
Applicant: Greenlee Textron Inc.
Inventor： John Wayne Kroening
Abstract: An assembly according to some embodiments of the disclosure includes an enclosure having a housing and door hingedly attached to the housing and a door stop mechanism which holds the door in an open position. The mechanism includes a link member pivotally connected to the door and to the housing. The link member has an elongated slot which extends along a portion of the link member. The slot has a linear portion and an enlarged opening at an end thereof which is offset from the linear portion. When the door is opened, a fastener, which is either mounted to the housing or to the door, slides along the slot until the fastener is positioned in the enlarged opening to hold the door open.
-
公开(公告)号：US20180057157A1
公开(公告)日：2018-03-01
申请号：US15252916
申请日：2016-08-31
Applicant: Bell Helicopter Textron Inc.
Inventor： Kirk Landon Groninga , Daniel Bryan Robertson
CPC classification number: B64C27/82 , B64C27/28 , B64C27/52 , B64C29/0033 , B64C39/008 , B64C2027/8245 , B64C2027/8254
Abstract: In some embodiments, an aircraft includes a fuselage having a forward portion and an aft portion. First and second ducted fans are supported by the forward portion of the fuselage. The first and second ducted fans are tiltable relative to the fuselage between a generally horizontal orientation, in a vertical takeoff and landing mode, and a generally vertical orientation, in a forward flight mode. A tailboom having an aft station extends from the aft portion of the fuselage. A cross-flow fan is disposed in the aft station of the tailboom and is operable to generate a pitch control moment.
-
-
-
-
-
-
-
-
-
Search Results
3499
records
(took 0.032 seconds)
