Search International and National Patent Collections
Some content of this application is unavailable at the moment.
If this situation persists, please contact us atFeedback&Contact
1. (CN102271999) Bearing assembly

Office : China
Application Number: 201080004204.2 Application Date: 14.01.2010
Publication Number: 102271999 Publication Date: 07.12.2011
Publication Kind : A
Prior PCT appl.: Application Number:PCTGB2010050053 ; Publication Number:2010084338 Click to see the data
IPC:
B64C 13/42
F15B 18/00
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
13
Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
24
Transmitting means
38
with power amplification
40
using fluid pressure
42
having duplication or stand-by provisions
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
15
FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
B
SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
18
Parallel arrangements of independent servomotor systems
CPC:
B64C 13/42
F15B 15/1404
Applicants: Airbus Operations Ltd.
空中客车操作有限公司
Inventors: Parker Simon
西蒙·帕克
Agents: li hui wang xiaodong
北京三友知识产权代理有限公司 11127
北京三友知识产权代理有限公司 11127
Priority Data: 0900822.8 20.01.2009 GB
Title: (EN) Bearing assembly
(ZH) 轴承组件
Abstract: front page image
(EN) A bearing assembly for mounting a pair of spaced parallel actuators (3) between a wing and a control surface of an aircraft so that the actuators control deployment of said control surface from the wing in tandem is disclosed. The bearing assembly comprises a fixed member (18) for attachment to the aircraft and a movable member (8) attachable to the actuators. The fixed and movable members are coupled via a part-spherical bearing (14) and are configured such that the part-spherical bearing is located in the space between the actuators (3).
(ZH)

公开了一种轴承组件,所述轴承组件用于将一对间隔开的平行的致动器(3)安装在飞机的机翼和操纵面之间,以使得所述致动器一致地控制所述操纵面从所述机翼展开。所述轴承组件包括用于附接至所述飞机的固定构件(18)和可附接至所述致动器的可动构件(8)。所述固定构件和所述可动构件通过部分球面轴承联接(14)联接,并且构造成使得所述部分球面轴承被定位在所述致动器(3)之间的空间中。


Also published as:
EP2379406JP2012515676US20120006939RU2011134866CA2746800RU0002520706
BRPI1006866WO/2010/084338