Mounting bracket
A mounting bracket for mounting an accessory to a gas turbine engine, the mounting bracket including a space frame structure. The space frame structure including a plurality of struts joined to one another at nodes.
1. A mounting bracket for mounting an accessory to a gas turbine engine, the bracket comprising:
a space frame structure that includes a first layer and a second layer, the first layer including a plurality of first struts and the second layer including a plurality of second struts, and the first layer being parallel to the second layer;
a plurality of nodes that each joins together two or more struts of the plurality of first struts and the plurality of second struts; and
a third strut that is obliquely disposed with regard to both the first layer and the second layer such that the third strut extends from the first layer to the second layer to directly connect the first layer with the second layer.
2. The mounting bracket of claim 1 , wherein the first layer and the second layer of the space frame structure form a double layer grid.
3. The mounting bracket of claim 2 , wherein at least one node of the plurality of nodes is extended to form a pillar that forms a node for both the first layer and the second layer.
4. The mounting bracket of claim 2 , wherein the third node is disposed at a periphery of the mounting bracket.
5. The mounting bracket of claim 2 , wherein at least one of the plurality of first struts is linked by a brace to a corresponding one of the plurality of second struts.
6. The mounting bracket of claim 1 , wherein the space frame structure forms an L shape.
7. The mounting bracket of claim 1 , wherein at least one of the struts is curved.
8. The mounting bracket of claim 1 , wherein at least one node of the plurality of nodes is configured to form an attachment boss.
9. The mounting bracket of claim 8 , wherein a first plurality of extended nodes forms a first set of attachment bosses for attaching an accessory to the bracket.
10. The mounting bracket of claim 9 , wherein a second plurality of extended nodes forms a second set of attachment bosses for attaching the bracket to a casing or nacelle of a gas turbine engine.
11. The mounting bracket of claim 10 , wherein the first set of bosses lies substantially in a first plane and the second set of bosses lies substantially in a second plane, and the first and second planes are substantially perpendicular.