Method of applying ice removal fluid to a folding wing aircraft and method of operating a folding wing aircraft
A method of applying an ice-removal fluid ( 113 ) to a folding wing aircraft ( 100 ) is described, the method comprising applying the ice-removal fluid ( 113 ) to the folding wing portion ( 103 ) and holding the folding wing portion in an over-folded position ( 111 ) once the ice-removal fluid ( 113 ) has been applied. A method of operating an aircraft ( 100 ) during ground based operations is further described using the method of applying an ice-removal fluid ( 113 ).
1 . Method of applying an ice-removal fluid to a folding wing aircraft, the method comprising:
a) applying the ice-removal fluid to the folding wing portion;
and
b) holding the folding wing portion in an over-folded position once the ice-removal fluid has been applied.
2 . Method of claim 1 , wherein the step of applying ice-removal fluid is carried out when the folding wing portion is positioned in an unfolded position.
3 . Method of claim 1 , wherein the step of applying ice-removal fluid is carried out when the folding wing portion is positioned in an overfolded position.
4 . Method of claim 1 , wherein the step of applying ice-removal fluid is carried out when the folding wing portion is positioned between a fully unfolded position and an overfolded position.
5 . Method of claim 1 , wherein the angle between the folding wing portion and the fixed wing portion in the over-fold position is more than 90 degrees.
6 . Method of operating an aircraft during ground based operations comprising the steps of:
a) positioning the aircraft at an off-stand location and applying an ice-removal fluid to a folding wing portion of the aircraft in accordance with claim 1 ; and
b) positioning the aircraft in at the aircraft stand once the ice removal fluid has been applied.
7 . Method of operating an aircraft during ground based operations comprising the steps of:
a) positioning the aircraft at an aircraft stand and applying an ice-removal fluid to a folding wing of the aircraft in accordance with claim 1 ;
positioning the aircraft at an off-stand location once the ice removal fluid has been applied.
8 . Method of claim 1 , wherein the angle between the folding wing portion and the fixed wing portion in the over-fold position is at least 135 degrees.