Granted Patent B2

US 12,560,194 · App. 18/128,156 · Granted Feb 24, 2026

Inventor: William Tulloch (Bristol, GB)

Assignee: AIRBUS OPERATIONS LIMITED

F16B43/009B64F5/10

Abstract

Claims (26)

1 . A washer device, comprising:

two annular components, each having a main face arranged to contact the main face of the other component, each main face having surface regions of different levels along an axis of the component, whereby relative rotation of one component with respect to the other about their common axis alters the effective thickness of the washer device;

at least one projection extending radially from one of the annular components and arranged to engage with at least one corresponding notch on the other annular component such that the annular components may be oriented in relative predetermined angular positions corresponding to different predetermined effective thicknesses of the washer device; and,

wherein the at least one projection is a plurality of radial projections extending outwardly from an outermost periphery of one component arranged to engage with a same number of corresponding notches on the other component.

2 . A washer device as claimed in claim 1 , in which the surface regions of different levels of each main face are formed by at least one step.

3 . A washer device as claimed in claim 1 , wherein the surface regions of different levels of each main face are formed by at least one ramp.

4 . A washer device as claimed in claim 1 , wherein one component is arranged to sit in a recess on the other component, the components having a coaxial central aperture.

5 . A washer device as claimed in claim 1 , further comprising a plurality of notches on one component with which the radial projection of the other component can engage.

6 . A washer device as claimed claim 1 , wherein at least one component includes permanently magnetic material.

7 . A washer device as claimed in claim 1 , further comprising visual indicators arranged to indicate to a user the effective thickness of the washer device when the components are in different respective relative positions.

8 . An aircraft component assembly including a washer device as claimed in claim 1 .

9 . An aircraft component assembly as claimed in claim 8 , further comprising a fastener extending coaxially through the washer device.

10 . An aircraft including an aircraft component assembly as claimed in claim 8 .

11 . A method of assembling aircraft components comprising the step of adjusting the effective thickness of the washer device as claimed in claim 1 .

12 . A method as claimed in claim 11 , in which the step of adjusting the effective thickness of the washer device further comprises the steps of separating axially the components of the washer device, rotating one component with respect to the other about the axis and then axially bringing the components together.

13 . A washer device, comprising:

two annular components, each having a main face arranged to contact the main face of the other component, each main face having surface regions of different levels along an axis of the component, whereby relative rotation of one component with respect to the other about their common axis alters the effective thickness of the washer device;

at least one projection extending radially from an outermost periphery of one of the annular components and arranged to engage with at least one corresponding notch on the other annular component such that the annular components may be oriented in relative predetermined angular positions corresponding to different predetermined effective thicknesses of the washer device;

wherein the at least one projection is a plurality of radial projections extending outwardly from an outermost periphery of one component arranged to engage with a same number of corresponding notches on the other component; and

wherein the surface regions of different levels of each main face are formed by a helical ramp extending around the circumference of its main face from a higher thickness region to a lower thickness region, and wherein the helical ramps of the two annular components cooperatively engage to adjust the effective thickness of the washer device through relative rotation.

14 . A washer device, comprising:

two annular components, each having a main face arranged to contact the main face of the other component, each main face having surface regions of different levels along an axis of the component, whereby relative rotation of one component with respect to the other about their common axis alters the effective thickness of the washer device;

at least one projection extending radially from an outermost periphery of one of the annular components and arranged to engage with at least one corresponding notch on the other annular component such that the annular components may be oriented in relative predetermined angular positions corresponding to different predetermined effective thicknesses of the washer device;

wherein the at least one projection is a plurality of radial projections extending outwardly from an outermost periphery of one component arranged to engage with a same number of corresponding notches on the other component;

wherein the surface regions of different levels of each main face comprise both at least one step and at least one helical ramp forming a gradual transition between different levels; and,

wherein the at least one step and the at least one helical ramp of one component are arranged to cooperatively engage with corresponding at least one step and at least one helical ramp of the other component to provide thickness adjustments through relative rotation of the components.

Priority Claims (1)

Continuity (1)

References Cited (26)