Problem 5.144
The landing gear for an airplane is shown just prior to landing. Frame
ABCDE
lies in the
y´
plane. The
150 lb
weight of the wheel and frame acts at point
D
in the
y
direction, and the
250 lb
force due to drag acts at point
D
in the
x
direction. The frame is supported by a self-aligning thrust bearing at
A
,
and a self-aligning bearing at
B
. A torsional spring is installed at
C
; it has
20 in:lb=degree
stiffness, and the moment it produces is zero when the landing
gear is fully raised (i.e., frame
ABCDE
rotates about the positive
´
axis until it
lies in the
x´
plane). The force
P
applied at point
E
has
x
,
y
, and
´
direction
cosines of
3=5
,
0
, and
4=5
, respectively. Assuming the landing gear is in
static equilibrium, determine the value of Pand all support reactions.
5.15 in./C250 lb.15 in./Bx.37 in./D0; (7)
5.12 in./D0; (9)
)ByD 54:50 lb, (10)