Bronzavia D 30 bombsight
The Bronzavia D 30 was fitted aboard the LeO.451 and DB-7 bombers.
Read the manual (in French)
Study the pictures (partly translated)
The Bronzavia D 30 seems to be a rather simple targeting system, more sophisticated
than the Blenheim's but less than complex systems like the famous Norden
sight. That is to say the bombardier is still dependant on the pilot to fly
the aircraft over the target. Some LeO.451s were eventually fitted with a
more sophisticated system, including a gyroscopic stabilized bomb sight coupled
to the plane's autopilot - but only after the Armistice.
Bombsight description:
The Bronzavia D 30 bombsight is partly externally mounted on the DB-7,
its lower part being outside the glass nose. When planes are parked on the
ground this equipment is protected by some piece of cloth or leather. Actually
the Bronzavia sight was designed for larger aircraft and it is not that
surprising that the DB-7 does not have as much room in the bombardier's
position as the LeO.451. This is visible on
some of those DB-7 pics
.
The D 30 has the form of a periscope and can rotate around the vertical
axis. It is linked to a target heading indicator (the "repetiteur type 11",
or "indicateur de Cap" ) that is mounted on the pilot's instrument panel.
All bombardment parameters are input via knobs on the upper part of the sight.
The "repetiteur type 11" seems to be fitted on the DB-7 immediately under
the pilot's directional gyro. (Indeed, it is also fitted near the directional
gyro aboard the LeO.451
as this page shows
) It does not show on the
DB-7 manufacturer's pic
(because, exactly like the gunsight, this equipment was fitted by the
Armée de l'air, not by Douglas), but it is (barely) visible
on this photograph of an operational DB-7's cockpit
. Notice the horizontal thing immediately left of the yoke axis, and
the wire hanging from it.
Aside from a complex bombardment data parameter entry, the bombardier interacts
with the bombsight using the following controls:
- the crank (located on the front right-hand side)
- rotating the crank allows the bombardier to call for heading adjustments
to the pilot, by modifying the target heading indicator's display
- the pedal (located on the left of the floor mounting)
- The interaction sounds complex but here's what I understand: when
the pedal is depressed, rotating the crank will also rotate the bombsight
around the vertical axis. When not depressed, the pilot's indicated target
varies but the bombsight does not rotate.
- the exploration button (probably the big knob mounted aft on the sight's
right-hand side)
- The exploration button allows the bombardier to rotate his view through
the bombsight around the pitch axis, when the bombsight is set in a particular
("Cinémométrie" - I don't know what that means) mode. In "bombardment
mode", however, the sight's view angle in pitch is determined from bombing
parameters and no longer adjustable.
Bombing procedure:
After various settings/calibration procedures (tediously explained in pages
1-5 of the manual), the bombardier guides the pilot above the target as explained
in page 6-7 of the manual. Here's how:
He locates the target in his sight, looking beyond the bombardement angle
via the exploration button, and if needed by rotating the sight in direction.
At the same time, the angle of rotation is indicated to the pilot on the
"repetiteur Bronzavia type 11" indicator. The pilot uses this information
to correct the aircraft's heading until it is aligned on the target. There
is probably no need for vocal interaction between the crew members at this
point.
If important corrections in heading are needed, the bombardier rotates the
sight with the crank while depressing the pedal. If only fine corrections
are needed, he only modifies the indicated target heading without turning
the sight by using the crank without depressing the pedal. When the target
appears on the sight reticule's vertical line, the heading is correct.
When the view pitch angle is in 10-15° range of the bombardment angle,
the bombardier switches to "bombardment mode". When the target is in the
center of the cross the bombs are released.
Various questions (now with answers):
Question 1: Does the bombardier manually rotate the sight to keep the
target aligned, or is the sight somehow automatically rotated - perhaps
via a synchronization with the directional gyro? Notice it is the same Sperry
directional gyro on the LeO as on the DB-7 (or a license-built copy).
The sight is manually rotated, either my the main handle
on the left, or by the the little crank on the front right. However, there
is a calibration procedure with the directional gyro (page 6 of the manual),
so the target heading indicator certainly gives accurate heading corrections.
Question 2: How exactly are input the bombardment parameters on the
sight - at least there are altitude, aircraft speed, perhaps wind or slip?
The parameter input is very complex: wind speed, wind direction,
aircraft ground speed, aircraft ground heading, height relative to the ground,
bomb ballistic parameters ("traînage", whatever that means).
Question 3: what are exactly the optical characteristics of the periscope,
we need at the very least the magnification (if any) and the field of view
from a SHAA document (I don't have the document reference
right now though)
- Field of view: 30°
- Magnification: 1.5
- Reticle colour: black by day, red by night
Question 4: are the bombs manually released by the bombardier using
the sight's reticule, or is there a more sophisticated system? What is
the use of the stopwatch on the bombsight?
The bombs are manually released. The stopwatch is used
for speed measurement and calibration procedures (via angular speed of an
observed spot on the ground).
Question 5: what is the interaction, if any, with the aircraft's autopilot?
None.
Question 6: how does the reticule aspect change as the bombardment parameters
are input?
The manual does not say, however it is unclear anything
at all changes.