-
公开(公告)号：US10196139B2
公开(公告)日：2019-02-05
申请号：US15986219
申请日：2018-05-22
Applicant: Bell Helicopter Textron Inc.
Inventor： Emily Schofield , Chad Lewis Jarrett , Daniel P. Sottiaux , Frank Bradley Stamps
Abstract: An apparatus comprising a drivelink comprising a housing including a socket, wherein the socket comprises a cross-sectional area, and a bearing cartridge disposed within the socket, wherein a cross-sectional area of the cartridge is less than the cross-sectional area of the socket. An apparatus comprising a drivelink comprising a housing having a socket, and a bearing cartridge positioned within the socket and comprising a first portion and a second portion, wherein the first portion is configured to undergo compression when a load is applied to the drivelink, and wherein the second portion is configured to not be in tension when the load is applied to the drivelink.
-
公开(公告)号：US10889366B2
公开(公告)日：2021-01-12
申请号：US16138672
申请日：2018-09-21
Applicant: Bell Helicopter Textron Inc.
Inventor： Chad Lewis Jarrett , Frank Bradley Stamps , Daniel Bryan Robertson , Kirk Landon Groninga , Matthew Edward Louis
Abstract: An aircraft comprising a pair of ducted thrusters. Each of the ducted thrusters comprises a duct surrounding a rotor assembly with a rotor hub having a plurality of rotor blades extending therefrom, wherein the plurality of rotor blades have a modulated angular distribution about a central longitudinal axis of the duct. Each of the ducted thrusters further comprises a stator assembly having a stator hub with a plurality of stator vanes extending from the stator hub to an interior surface of the duct, wherein each of the plurality of the stator vanes are angularly modulated around the stator hub such that angular spacing between pairs of adjacent vanes of the plurality of stator vanes varies for each pair of the adjacent vanes.
-
公开(公告)号：US20200094942A1
公开(公告)日：2020-03-26
申请号：US16138672
申请日：2018-09-21
Applicant: Bell Helicopter Textron Inc.
Inventor： Chad Lewis Jarrett , Frank Bradley Stamps , Daniel Bryan Robertson , Kirk Landon Groninga , Matthew Edward Louis
Abstract: An aircraft comprising a pair of ducted thrusters. Each of the ducted thrusters comprises a duct surrounding a rotor assembly with a rotor hub having a plurality of rotor blades extending therefrom, wherein the plurality of rotor blades have a modulated angular distribution about a central longitudinal axis of the duct. Each of the ducted thrusters further comprises a stator assembly having a stator hub with a plurality of stator vanes extending from the stator hub to an interior surface of the duct, wherein each of the plurality of the stator vanes are angularly modulated around the stator hub such that angular spacing between pairs of adjacent vanes of the plurality of stator vanes varies for each pair of the adjacent vanes.
-
Patent Agency Ranking
公开(公告)号：US10259576B2
公开(公告)日：2019-04-16
申请号：US15709153
申请日：2017-09-19
Applicant: BELL HELICOPTER TEXTRON INC.
Inventor： Chad Lewis Jarrett , Frank Bradley Stamps , Glenn Shimek
IPC: B64C27/51 , B64C27/605 , B64C27/35
Abstract: A rotary system including a grip having an opening forming a first bridge for receiving a centrifugal force bearing that faces inwardly towards the rotor mast. A rotor blade couples to the grip and a pitch horn positioned outside the opening pitches the rotor blade during flight. A bearing assembly attaches the first bridge to the yoke and controls blade forces exerted against the hub assembly during flight.
-
公开(公告)号：US20180290737A1
公开(公告)日：2018-10-11
申请号：US15986219
申请日：2018-05-22
Applicant: Bell Helicopter Textron Inc.
Inventor： Emily Schofield , Chad Lewis Jarrett , Daniel P. Sottiaux , Frank Bradley Stamps
CPC classification number: B64C27/35 , B23P19/04 , B64C27/41 , F16C7/04 , F16C11/083 , F16C27/063 , F16C2326/43 , F16D3/62 , F16F1/3863 , Y10T29/49643 , Y10T29/4984
Abstract: An apparatus comprising a drivelink comprising a housing including a socket, wherein the socket comprises a cross-sectional area, and a bearing cartridge disposed within the socket, wherein a cross-sectional area of the cartridge is less than the cross-sectional area of the socket. An apparatus comprising a drivelink comprising a housing having a socket, and a bearing cartridge positioned within the socket and comprising a first portion and a second portion, wherein the first portion is configured to undergo compression when a load is applied to the drivelink, and wherein the second portion is configured to not be in tension when the load is applied to the drivelink.
-
6.发明授权公开(公告)号：US09879722B2
公开(公告)日：2018-01-30
申请号：US13793683
申请日：2013-03-11
Applicant: Bell Helicopter Textron Inc.
Inventor： Chad Lewis Jarrett , Frank Bradley Stamps , Daniel P. Sottiaux
CPC classification number: F16C33/04 , B64C27/33 , B64C27/35 , F16C27/02 , F16F1/3842
Abstract: A bearing assembly comprises a bearing, a shim disposed within the bearing, and a component disposed within the shim. The shim comprises a first material, the component comprises a second material, and the first material has an elastic modulus value that is lower than an elastic modulus value of the second material. An apparatus comprises an elastomeric bearing, a fiberglass shim, and a steel spindle that is connected to the elastomeric bearing through the shim. A method for reducing strain in an adhesive layer that connects a bearing to a component comprises selecting a shim material having an elastic modulus value that is less than an elastic modulus value of the component and providing instructions to connect the component to the shim by placing the adhesive layer between an outer surface of the component and an inner surface of the shim.
-
公开(公告)号：US20180093764A1
公开(公告)日：2018-04-05
申请号：US15709153
申请日：2017-09-19
Applicant: BELL HELICOPTER TEXTRON INC.
Inventor： Chad Lewis Jarrett , Frank Bradley Stamps , Glenn Shimek
IPC: B64C27/605 , B64C27/35
CPC classification number: B64C27/605 , B64C27/35
Abstract: A rotary system including a grip having an opening forming a first bridge for receiving a centrifugal force bearing that faces inwardly towards the rotor mast. A rotor blade couples to the grip and a pitch horn positioned outside the opening pitches the rotor blade during flight. A bearing assembly attaches the first bridge to the yoke and controls blade forces exerted against the hub assembly during flight.
-
8.发明申请Low Shear Modulus Transition Shim for Elastomeric Bearing Bonding in Torsional Applications 有权低剪切模量过渡垫用于扭转应用中的弹性轴承粘合公开(公告)号：US20140255191A1
公开(公告)日：2014-09-11
申请号：US13793683
申请日：2013-03-11
Applicant: BELL HELICOPTER TEXTRON INC.
Inventor： Chad Lewis Jarrett , Frank Bradley Stamps , Daniel P. Sottiaux
CPC classification number: F16C33/04 , B64C27/33 , B64C27/35 , F16C27/02 , F16F1/3842
Abstract: A bearing assembly comprises a bearing, a shim disposed within the bearing, and a component disposed within the shim. The shim comprises a first material, the component comprises a second material, and the first material has an elastic modulus value that is lower than an elastic modulus value of the second material. An apparatus comprises an elastomeric bearing, a fiberglass shim, and a steel spindle that is connected to the elastomeric bearing through the shim. A method for reducing strain in an adhesive layer that connects a bearing to a component comprises selecting a shim material having an elastic modulus value that is less than an elastic modulus value of the component and providing instructions to connect the component to the shim by placing the adhesive layer between an outer surface of the component and an inner surface of the shim.
Abstract translation: 轴承组件包括轴承，设置在轴承内的垫片和设置在垫片内的部件。 垫片包括第一材料，该部件包括第二材料，并且第一材料具有低于第二材料的弹性模量值的弹性模量值。 一种装置包括弹性轴承，玻璃纤维垫片和通过垫片连接到弹性轴承的钢质心轴。 一种用于减小将轴承与部件连接在一起的粘合剂层中的应变的方法包括选择弹性模量值小于该部件的弹性模量值的垫片材料，并提供将部件连接到垫片上的指令， 组件的外表面和垫片的内表面之间的粘合剂层。
-
-
-
-
-
-
-
Search Results
8
records
(took 0.015 seconds)
