MOUNTING ARRANGEMENT
First Claim
Patent Images
1. An assembly comprising a rigid electrical raft mounted to a body, wherein:
- the rigid electrical raft comprises electrical conductors embedded in a rigid material;
the rigid electrical raft is mechanically attached to the body using at least one fusible mount arrangement; and
the fusible mount arrangement is constructed and arranged to break when a predetermined load is applied to the assembly.
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Accused Products
Abstract
A rigid electrical raft is provided to a gas turbine engine via a fusible mount arrangement. The rigid electrical raft may be a part of an electrical system of the gas turbine engine, for example a part of the electrical harness. The fusible mount is arranged to break when a predetermined load is applied. The rigid electrical raft may be attached to a fan case of the engine, and the predetermined load may that which results from a fan blade being released from the hub. This ensures that the rigid electrical raft is protected from the load.
40 Citations
15 Claims
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1. An assembly comprising a rigid electrical raft mounted to a body, wherein:
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the rigid electrical raft comprises electrical conductors embedded in a rigid material; the rigid electrical raft is mechanically attached to the body using at least one fusible mount arrangement; and the fusible mount arrangement is constructed and arranged to break when a predetermined load is applied to the assembly. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14)
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15. A method of assembling a gas turbine engine having a rigid electrical raft comprising electrical conductors embedded in a rigid material, the method comprising:
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mechanically attaching the rigid electrical raft to a fan containment structure of the gas turbine engine using at least one fusible mount arrangement that is constructed and arranged to break when a predetermined load is applied to the fan containment structure, and at least one non-fusible mount arrangement constructed and arranged to remain intact when the predetermined load is applied to the fan containment structure, wherein; the predetermined load is lower than the load generated in the event of a fan blade being released from the gas turbine engine and striking the fan containment structure, and higher than the load generated in normal operation of the engine, such that after the predetermined load is applied, the rigid electrical raft is mechanically attached to the fan containment structure by the at least one non-fusible mount arrangement, but not by the at least one fusible mount arrangement.
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Specification