Panel attachment system
A gas turbine engine exhaust panel mounting system comprising a panel, a casing and an attachment assembly for removably connecting the panel to the casing comprises a retaining portion, a clamping portion, and a ‘C’-shaped connecting link. The connecting link has a first attachment portion and an opposite second attachment portion with the first and second attachment portions being connected to one another by a center portion. Each of the first and second attachment portions is substantially parallel to one another and extends in the same direction from respective ends of the center portion. The first attachment portion is fixedly connected to the casing by the clamping portion, and the second attachment portion is slidingly connected to the panel by the retaining portion.
1. A gas turbine engine exhaust panel mounting system comprising:
a gas turbine engine exhaust panel;
a gas turbine engine exhaust casing; and
an attachment assembly including:
a retaining portion;
a clamping portion; and
a ‘C’-shaped connecting link,
the ‘C’-shaped connecting link having a first attachment portion and an opposite second attachment portion, the first and second attachment portions being connected to one another by a centre portion, each of the first and second attachment portions being substantially parallel to one another and extending in the same direction from respective ends of the centre portion, the first attachment portion being fixedly connected to the gas turbine engine exhaust casing by the clamping portion, and the second attachment portion being slidingly connected to the gas turbine engine exhaust panel by the retaining portion,
wherein the clamping portion includes a first end and an opposite second end, the first end having a slot formed through the first end and adapted to accommodate the first attachment portion, the second end being connected to the gas turbine engine exhaust casing.
2. The gas turbine engine exhaust panel mounting system as claimed in claim 1 , wherein the second end of the clamping portion comprises a threaded portion, the threaded portion extending through a hole in the gas turbine engine exhaust casing, a clamping nut being threadingly engaged with the threaded portion such that as the clamping nut is tightened the first attachment portion is securely clamped within the slot.
3. The gas turbine engine exhaust panel mounting system as claimed in claim 1 , wherein the first attachment portion is provided with a notch, the notch being adapted to abut against the slot of the clamping portion.
4. The gas turbine engine exhaust panel mounting system as claimed in claim 1 , wherein a centre axis of the clamping portion is coincident with a centre axis of the retaining portion.
5. The gas turbine engine exhaust panel mounting system as claimed in claim 1 , wherein the centre portion is formed with a rectangular cross-sectional profile.
6. The gas turbine engine exhaust panel mounting system as claimed in claim 5 , wherein the width sides of the centre portion are streamlined.
7. The gas turbine engine exhaust panel mounting system as claimed in claim 1 , wherein the retaining portion comprises a recess adapted to accommodate the second attachment portion.
8. The gas turbine engine exhaust panel mounting system as claimed in claim 7 , wherein the retaining portion is formed with a top hat cross-sectional profile with the recess being located within the top hat cross-sectional profile.
9. The gas turbine engine exhaust panel mounting system as claimed in claim 1 , wherein a surface of the gas turbine engine exhaust casing is provided with an anti-rotation stop, the first attachment portion abutting against the anti-rotation stop to thereby prevent relative rotation between the first attachment portion and the anti-rotation stop.
10. The gas turbine engine exhaust panel mounting system as claimed in claim 1 , wherein the retaining portion is formed from sheet metal or sheet metal alloy.
11. The gas turbine engine exhaust panel mounting system as claimed in claim 1 , wherein the ‘C’-shaped connecting link is formed from sheet metal or sheet metal alloy.
12. The gas turbine engine exhaust panel mounting system as claimed in claim 11 , wherein the sheet metal or sheet metal alloy has a thickness within the range of 4 mm to 6 mm.