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Patent · US10774787B2 · B2 · US

Coupling

(11) Publication number
US10774787B2
(21) Application number
15/591,636
(22) Filing date
2017-05-10
(30) Priority date
2016-08-08
(43) Publication date
2020-09-15
(45) Date of grant
2020-09-15
(51) IPC
F02K 1/76; F02K 1/80; F15B 15/14; F15B 15/16; F16B 7/10
(52) CPC
  • F02K Jet-propulsion plants: 1/80, 1/763
  • F15B Systems acting by means of fluids in general; fluid-pressure actuators, e.g. servomotors; details of fluid-pressure systems, not otherwise provided for: 15/1409, 15/1457, 15/1466, 15/1471, 15/16, 15/165
  • F16B Devices for fastening or securing constructional elements or machine parts together, e.g. nails, bolts, circlips, clamps, clips or wedges; joints or jointing: 7/105
(73) Assignee
Goodrich Actuation Systems Ltd
(72) Inventors
Andrew Hawksworth
(54) Title
Coupling
(57) Abstract

A coupling e.g. for an actuator, comprises a housing which is preferably in the form of a ring mounted around the end of the outer rod and which can be mounted to a component e.g. a cowl being deployed. Within the housing of the coupling is provided a ring disk. This is sized and arranged within the housing such that there is some clearance between the ring disk and the housing so as to permit some eccentric movement.

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Claims (5)

  1. An actuator assembly comprising; a first moveable component; and a second moveable component, moveable relative to the first moveable component; wherein the first and second moveable components are arranged to actuate, in use, respectively, first and second moveable parts; wherein the first moveable component is an outer rod and the second moveable component is an inner rod arranged for telescopic movement within the outer rod; and a coupling assembly, the coupling assembly comprising: a housing configured to be fixedly attached to a fixed component, and a moveable element arranged inside the housing and arranged to be fixed to the outer rod, wherein the moveable element is arranged in the housing such that it has freedom of movement within the housing in an eccentric path in two dimensions in response to a force exerted on the outer rod component such that a force transmitted to the first moveable component by movement of the second moveable component is accommodated by eccentric movement of the moveable element within the housing.
  2. The actuator assembly coupling of claim 1, wherein the housing is in the form of a ring and the moveable element comprises a ring or annular disk mounted within the housing for eccentric movement relative to the housing.
  3. The assembly of claim 1, wherein the eccentric movement is in a plane perpendicular to the axial direction of the outer and inner rods.
  4. The assembly of claim 1, wherein the coupling assembly is attached to the inner rod.
  5. The assembly of claim 1, wherein the actuator assembly is an actuator assembly for a TRAS system for use in an aircraft and wherein the first and second moveable parts are first and second flaps of the aircraft.

Description

This application claims priority to European Patent Application No. 16183215.9 filed Aug. 8, 2016, the entire contents of which is incorporated herein by reference.

The present disclosure relates to a coupling, particularly an eccentric coupling for, for example, an actuator assembly.

Many mechanical systems require a coupling component or structure for coupling two or more parts of an assembly and to allow or prevent various degrees of movement between coupled parts.

Coupling structures are known, for example, for joining components of an actuator assembly. Depending on the operation and structure of the actuator assembly, couplings or joints may be designed to accommodate some translation of movement between the two components joined by the coupling, so as to avoid ‘force fighting’ or damage to one or both components due to the force on one of the components.

The coupling of this disclosure will be specifically described in relation to an actuator such as commonly used in aircraft e.g. for deploying/moving cowls and flaps. The coupling may, however, find a very wide range of applications and is not limited to this specific field. There is a general need for an eccentric coupling that permits some movement of a first component when a force is applied to a second component coupled to the first.

Citations (13)

  • US2993472A
  • GB2395693A
  • US8931253B2
  • US8733228B2
  • US9206765B2
  • US20130284010A1
  • JP5728132B2
  • US9447700B2
  • US20150354500A1
  • US9476384B2
  • US9494108B2
  • FR3063532A1
  • US20190271282A1
Record as JSON
{
  "publication_number": "US10774787B2",
  "country": "US",
  "kind": "B2",
  "title": "Coupling",
  "abstract": "A coupling e.g. for an actuator, comprises a housing which is preferably in the form of a ring mounted around the end of the outer rod and which can be mounted to a component e.g. a cowl being deployed. Within the housing of the coupling is provided a ring disk. This is sized and arranged within the housing such that there is some clearance between the ring disk and the housing so as to permit some eccentric movement.",
  "claims": [
    "1. An actuator assembly comprising; a first moveable component; and a second moveable component, moveable relative to the first moveable component; wherein the first and second moveable components are arranged to actuate, in use, respectively, first and second moveable parts; wherein the first moveable component is an outer rod and the second moveable component is an inner rod arranged for telescopic movement within the outer rod; and a coupling assembly, the coupling assembly comprising: a housing configured to be fixedly attached to a fixed component, and a moveable element arranged inside the housing and arranged to be fixed to the outer rod, wherein the moveable element is arranged in the housing such that it has freedom of movement within the housing in an eccentric path in two dimensions in response to a force exerted on the outer rod component such that a force transmitted to the first moveable component by movement of the second moveable component is accommodated by eccentric movement of the moveable element within the housing.",
    "2. The actuator assembly coupling of claim 1, wherein the housing is in the form of a ring and the moveable element comprises a ring or annular disk mounted within the housing for eccentric movement relative to the housing.",
    "3. The assembly of claim 1, wherein the eccentric movement is in a plane perpendicular to the axial direction of the outer and inner rods.",
    "4. The assembly of claim 1, wherein the coupling assembly is attached to the inner rod.",
    "5. The assembly of claim 1, wherein the actuator assembly is an actuator assembly for a TRAS system for use in an aircraft and wherein the first and second moveable parts are first and second flaps of the aircraft."
  ],
  "description_excerpt": "This application claims priority to European Patent Application No. 16183215.9 filed Aug. 8, 2016, the entire contents of which is incorporated herein by reference.\n\nThe present disclosure relates to a coupling, particularly an eccentric coupling for, for example, an actuator assembly.\n\nMany mechanical systems require a coupling component or structure for coupling two or more parts of an assembly and to allow or prevent various degrees of movement between coupled parts.\n\nCoupling structures are known, for example, for joining components of an actuator assembly. Depending on the operation and structure of the actuator assembly, couplings or joints may be designed to accommodate some translation of movement between the two components joined by the coupling, so as to avoid ‘force fighting’ or damage to one or both components due to the force on one of the components.\n\nThe coupling of this disclosure will be specifically described in relation to an actuator such as commonly used in aircraft e.g. for deploying/moving cowls and flaps. The coupling may, however, find a very wide range of applications and is not limited to this specific field. There is a general need for an eccentric coupling that permits some movement of a first component when a force is applied to a second component coupled to the first.",
  "cpc": [
    "F02K 1/80",
    "F02K 1/763",
    "F15B 15/1409",
    "F15B 15/1457",
    "F15B 15/1466",
    "F15B 15/1471",
    "F15B 15/16",
    "F15B 15/165",
    "F16B 7/105"
  ],
  "ipc": [
    "F02K 1/76",
    "F02K 1/80",
    "F15B 15/14",
    "F15B 15/16",
    "F16B 7/10"
  ],
  "assignees": [
    "Goodrich Actuation Systems Ltd"
  ],
  "inventors": [
    "Andrew Hawksworth"
  ],
  "filing_date": "2017-05-10",
  "publication_date": "2020-09-15",
  "grant_date": "2020-09-15",
  "priority_date": "2016-08-08",
  "application_number": "US-201715591636-A",
  "family_id": "56740859",
  "cited_by_count": 0,
  "citations": [
    "US2993472A",
    "GB2395693A",
    "US8931253B2",
    "US8733228B2",
    "US9206765B2",
    "US20130284010A1",
    "JP5728132B2",
    "US9447700B2",
    "US20150354500A1",
    "US9476384B2",
    "US9494108B2",
    "FR3063532A1",
    "US20190271282A1"
  ]
}

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