Firefighting use of Zeppelins?
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Firefighting use of Zeppelins?  
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1.  Vince Brannigan  
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 Mais opções 31 ago 2002, 13:00
Grupos de notícias: sci.military.naval
De: Vince Brannigan <vze2t...@verizon.net>
Data: Sat, 31 Aug 2002 16:00:36 GMT
Local: Sab 31 ago 2002 13:00
Assunto: Re: Firefighting use of Zeppelins?

Picosoft wrote:
> BTW, did we ever decide what the Brooklyn Bridge was made out of?

The towers are masonry

vince


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2.  Keith Willshaw  
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 Mais opções 1 set 2002, 11:59
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De: "Keith Willshaw" <keith@kwillshaw_NoSpam.demon.co.uk>
Data: Sun, 1 Sep 2002 15:59:17 +0100
Local: Dom 1 set 2002 11:59
Assunto: Re: Firefighting use of Zeppelins?

"Vince Brannigan" <vze2t...@verizon.net> wrote in message

news:3D70E871.354EDDD0@verizon.net...

> Picosoft wrote:

> > BTW, did we ever decide what the Brooklyn Bridge was made out of?

> The towers are masonry

And the cables and deck are steel

Keith


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3.  simon  
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 Mais opções 31 ago 2002, 22:07
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De: simon <simona...@erols.com>
Data: Sat, 31 Aug 2002 20:59:05 -0400
Local: Sab 31 ago 2002 21:59
Assunto: Re: Firefighting use of Zeppelins?

Why? I'm not being a pain, I'm just curious. An airfoil is an airfoil, or
is there some scaling factor, (the airship body passes through its length
over a much longer period of time than the wing on a plane)  or is it
because it is of (approximately) circular cross section.  I gather that
the reynolds number for airships is radicly different than for airplanes.
No, realy, I'm curious to get a thumbnail dexcription of why the lift that
the body an airship gets would be 10times less dependant on AOA than
an aircraft wing.

> >However
> >the AOA on an airship, as well as representing a much smaller percentage
> >of lift, is also changed MUCH (I'm guessing ~2 orders of magnitude) more
> >slowly, leading to a less controllable vehicle.

> I think that a generous estimate.

I actually think that you're right here, probably more like 4 orders, I was
trying
to be generous, I like the big old Zeppelins, but it is hard to come up with a
worse
job for them.  Reading accounts of how barely controllable they were, it is
difficult to imagine them lasting long near a forest fire before they were
either
sucked into an updraft, or simply torn in two by the winds.

I would go so far as to say that you could probably NEVER get a rigid airship
approved
for paying passengers by the FAA.  While materials technology and structural
modeling has come along way since the 1920s, I suspect that said modeling would
indicate that you could not get sufficient safety factors in the structure.
Back then
there was alot of guessing and hoping at what the aerodynamic loads would be
in the air.  And of course the airplanes that you would compare it to have
become
radicly safer than aircraft of the 1920s.


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4.  Brad Meyer  
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 Mais opções 1 set 2002, 17:19
Grupos de notícias: sci.military.naval
De: Brad Meyer <bradm...@attbi.com>
Data: Sun, 01 Sep 2002 20:19:08 GMT
Local: Dom 1 set 2002 17:19
Assunto: Re: Firefighting use of Zeppelins?

The airfoil of, say, a Cessna 182 is radically different then that of
a F-16. The air ship is a poor airfoil and generates virtually no lift
whatsoever. Because it is a close to (or at) neutral bouancy in the
air, it can be moved up or down by thrust (much like a submarine in
water) but changes in angle of attack of the airship have no more
effect on the lift it produces then similar changes on a submarine.

>. . . or
>is there some scaling factor, (the airship body passes through its length
>over a much longer period of time than the wing on a plane)  or is it
>because it is of (approximately) circular cross section.

This last. The shape generates little or no lift

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5.  Picosoft  
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 Mais opções 1 set 2002, 23:11
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De: "Picosoft" <m...@worldnet.att.net>
Data: Mon, 02 Sep 2002 02:11:11 GMT
Local: Dom 1 set 2002 23:11
Assunto: Re: Firefighting use of Zeppelins?
Well, I'm pretty much done with this topic, but I can't let this go by. The
airfoil formed by the airship body only generates zero lift if the elevator
(or engine thrust) is neutral. Otherwise it will generate *considerable*
lift.

Pretty much like an F-16 airfoil actually.

"Brad Meyer" <bradm...@attbi.com> wrote in message

news:7qs4nugleei0lvor8869r4cejk43sj5r9r@4ax.com...


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6.  simon  
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 Mais opções 2 set 2002, 11:35
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De: simon <simona...@erols.com>
Data: Mon, 02 Sep 2002 10:26:39 -0400
Local: Seg 2 set 2002 11:26
Assunto: Re: Firefighting use of Zeppelins?

Agreed, which is has lift with a greater AOA dependence?

> The air ship is a poor airfoil and generates virtually no lift
> whatsoever. Because it is a close to (or at) neutral bouancy in the
> air, it can be moved up or down by thrust (much like a submarine in
> water) but changes in angle of attack of the airship have no more
> effect on the lift it produces then similar changes on a submarine.

But operational subs usually use lift generated both on the hull and the diving
planes for controll. Using thrust is the provenance of small research subs
and black ops where zero movement stationkeeping is required.  In
Das Boot, the reason that everyone ran to the front in a crash dive was
to lower the bow, and thereby change the AOA of the sub.  (admittedly,
the presence of diving planes weakens my arguement, but see below.

> >. . . or
> >is there some scaling factor, (the airship body passes through its length
> >over a much longer period of time than the wing on a plane)  or is it
> >because it is of (approximately) circular cross section.

> This last. The shape generates little or no lift

The mere fact that the control surfaces are located in the tail like most
aircraft would seem to gainsay this.  Look at it this way,  when the elevator
control surfaces rise, the lift on the tail surfaces DECREASES, and the tail drops.

However, the AOA of the body of the Zeppelin increases and the lift
generated INCREASES.  The fact that the ship then moves up means
that the lift generated by the body is greater than the lift generated by
the tail surfaces. The fact that the amount of dynamic lift is smaller than
static lift does not change the fact that the lift generated by the body
(in the absence of any diving-plane like appendages) is greater than
the lift generated by the tail.

ISTR that to much downangle on the ship resulted in the Shenendoah
stalling UPWARDS while trying to escape an updraft on its last flight.

The problem for controlability is that said lift is proportinately smaller
compared to both wetted area and mass than is the case with airplanes.
This, and the fact it is a relatively weak structure mean that it takes
MUCH longer to respond to wind gusts, changes in temperatrue and
pressure etc.. than airplanes.  This would be even more true of the
proportion of thrust generated by rotors and wetted area as compared
with helicopters.


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7.  Picosoft  
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 Mais opções 1 set 2002, 21:59
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De: "Picosoft" <m...@worldnet.att.net>
Data: Mon, 02 Sep 2002 00:59:28 GMT
Local: Dom 1 set 2002 21:59
Assunto: Re: Firefighting use of Zeppelins?

> do you have the slightest idea what happens above a fire?  Hint, hot air
is
> thinner.  Tehre are also updrafts.

I meant to respond to this particular point, but I guess I forgot. This is
important and I should have dealt with it.

You are, of course, correct, hot air is less dense, and in less dense air
the helium in the airship will expand. This is why I specify using only
engine power and not buoyancy to lift the water. This way the 500,000 cubic
meter (max helium volume) airship needs to start with only 300,000 cubic
meters (or so) of helium.

This is enough buoyancy to lift the ship, fuel and minimum of ballast.All
other lifting will be done by rotating the engines upward or by dynamic
lift. If the ship encounters hot air, then the helium will have plenty of
room to expand.

If extremely low pressure is encountered then the cells will be able to
withstand a fair amount of superpressure. Only in extreme instances would
helium need to be vented. Let's consider a worst case scenario: Let's assume
that all six rotors have been destroyed and the airship has been blown high
aloft and lost half it's helium. This would leave it very heavy and without
engine power.

Would all aboard be doomed? No. What you would do in this case is begin
heating the helium as the airship begins to descend. Using auxiliary power
you should be able to restore neutral buoyancy and free balloon to a safe
area. Then perform a controlled descent to the most convenient 500 acre
field and land. Replace helium, replace rotors, fly to Akron for repairs.


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8.  Vince Brannigan  
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 Mais opções 1 set 2002, 22:26
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De: Vince Brannigan <vze2t...@verizon.net>
Data: Mon, 02 Sep 2002 01:26:29 GMT
Local: Dom 1 set 2002 22:26
Assunto: Re: Firefighting use of Zeppelins?

Picosoft wrote:
> > do you have the slightest idea what happens above a fire?  Hint, hot air
> is
> > thinner.  Tehre are also updrafts.

> I meant to respond to this particular point, but I guess I forgot. This is
> important and I should have dealt with it.

> You are, of course, correct, hot air is less dense, and in less dense air
> the helium in the airship will expand.

No, before the that transfers to the airship, it tends to lose buoyancy

> This is why I specify using only
> engine power and not buoyancy to lift the water.

exactly how?  vertical lift a la helicopter or something else?

> This way the 500,000 cubic
> meter (max helium volume) airship needs to start with only 300,000 cubic
> meters (or so) of helium.

again , how do you generate the vertical lift?

> This is enough buoyancy to lift the ship, fuel and minimum of ballast.All
> other lifting will be done by rotating the engines upward or by dynamic
> lift. If the ship encounters hot air, then the helium will have plenty of
> room to expand.

see above.  if you are picking up the water by helicopter lift, the helicopter
does the job more efficiently

> If extremely low pressure is encountered then the cells will be able to
> withstand a fair amount of superpressure. Only in extreme instances would
> helium need to be vented. Let's consider a worst case scenario: Let's assume
> that all six rotors have been destroyed and the airship has been blown high
> aloft and lost half it's helium. This would leave it very heavy and without
> engine power.

> Would all aboard be doomed? No. What you would do in this case is begin
> heating the helium as the airship begins to descend. Using auxiliary power
> you should be able to restore neutral buoyancy and free balloon to a safe
> area. Then perform a controlled descent to the most convenient 500 acre
> field and land. Replace helium, replace rotors, fly to Akron for repairs.

this is silly  ints not "low pressure" its low density.

Vince


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9.  Picosoft  
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 Mais opções 1 set 2002, 22:56
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De: "Picosoft" <m...@worldnet.att.net>
Data: Mon, 02 Sep 2002 01:56:22 GMT
Local: Dom 1 set 2002 22:56
Assunto: Re: Firefighting use of Zeppelins?

">

> again , how do you generate the vertical lift?

> see above.  if you are picking up the water by helicopter lift, the
helicopter
> does the job more efficiently

Since you have a whole thread on the V-22 (on that topic I substantially
agree with you, btw), you must understand the concept. Point engines up,
spin rotors, lift water. A helicopter will NOT do this more efficiently. A
helicopter has to lift its own weight in addition to any water. It has to
carry 9 tons of helicopter for every ton of water. An airship's weight is
supported by helium. All the engines need to lift is water.

Actually this is not entirely true. If the fire is at a different altitude
than the lake, then the airship will have to lift some of its weight to that
altitude. But even so the airship would be much more efficient than any
helicopter or airplane. In addition the airship doesn't have to return to
base after after every three water drops to refuel. It could probably
operate for twenty hours straight if two crews were aboard.


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10.  Vince Brannigan  
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 Mais opções 2 set 2002, 09:23
Grupos de notícias: sci.military.naval
De: Vince Brannigan <vze2t...@verizon.net>
Data: Mon, 02 Sep 2002 12:19:03 GMT
Local: Seg 2 set 2002 09:19
Assunto: Re: Firefighting use of Zeppelins?

you miss my point.  as in the V-22 a helicopter can be optimized for the lift of
its rotor.  A tilt rotor is suboptimal.
The ratio on helicopter is not 9-1

> Actually this is not entirely true. If the fire is at a different altitude
> than the lake, then the airship will have to lift some of its weight to that
> altitude. But even so the airship would be much more efficient than any
> helicopter or airplane. In addition the airship doesn't have to return to
> base after after every three water drops to refuel. It could probably
> operate for twenty hours straight if two crews were aboard.

It has to carry all those crews. all of which add to the overhead

vince


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