U.S. patent number 3,897,032 [Application Number 05/415,321] was granted by the patent office on 1975-07-29 for method for operating airships, particularly by means of hydrocarbon gas or hydrogen.
Invention is credited to Hermann Ernst Robert Papst.
United States Patent |
3,897,032 |
Papst |
July 29, 1975 |
Method for operating airships, particularly by means of hydrocarbon
gas or hydrogen
Abstract
A method of operating a lighter-than-air airship comprises
utilizing natural gas and/or hydrogen as the buoyant lifting gas
and as a source of power. The reduced buoyancy resulting from
consumption of part of the gas is replaced with a gas species
obtained by chemically converting part of the original gas. The gas
species may be, for example, substantially saturated water vapor
obtained by combustion of the original gas or hydrogen obtained by
the catalytic partial oxidation of a hydrocarbon with water
vapor.
Inventors: |
Papst; Hermann Ernst Robert
(D7742 St. Georgen, Black Forest, DT) |
Family
ID: |
27182435 |
Appl.
No.: |
05/415,321 |
Filed: |
November 13, 1973 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
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227887 |
Feb 22, 1972 |
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119335 |
Feb 26, 1971 |
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Foreign Application Priority Data
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Feb 26, 1970 [DT] |
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2009088 |
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Current U.S.
Class: |
244/96; 244/30;
244/61 |
Current CPC
Class: |
B64B
1/60 (20130101); B64B 1/58 (20130101) |
Current International
Class: |
B64B
1/60 (20060101); B64B 1/00 (20060101); B64B
1/58 (20060101); B64B 001/58 () |
Field of
Search: |
;244/97,96,98,99,61,30,31 ;136/83R,86B,86C,97 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Blix; Trygve M.
Assistant Examiner: Kelmachter; Barry L.
Attorney, Agent or Firm: Cushman, Darby & Cushman
Parent Case Text
This is a continuation of application Ser. No. 227,887, now
abandoned, filed Feb. 22, 1972 as a continuation-in-part of
application Ser. No. 119,335, now abandoned, filed Feb. 26, 1971.
Claims
What is claimed is:
1. A method of operating an airship which is maintained buoyant in
air by an original lifting gas which is inflammable and which is
lighter than air, said method comprising carrying said original
lifting gas in said airship as the sole fuel for generating driving
power for the airship, consuming at least a part of the original
lifting gas as fuel for supplying driving power for use by the
airship thereby effecting a reduced buoyancy of the airship and
restoring the reduced buoyancy by chemically converting a portion
of the original lifting gas to a different gas species which has at
least the same buoyancy effect as the gas which was consumed for
supplying power and storing said gas species whereby all said
lifting gas may be used for power production while maintaining
buoyancy.
2. A method as in claim 1 wherein the original lifting gas contains
a hydrocarbon and wherein the gas species obtained by chemically
converting a portion of the original lifting gas includes at least
one of water vapor and hydrogen, said method further including
feeding at least a portion of said gas species to a gas bag which
is separate from the original lifting gas.
3. A method as in claim 1 wherein the step of chemically converting
includes combustion of at least a portion of the original lifting
gas to produce heat and a combustion gas which includes water
vapor, said method further including condensing the water vapor
from the combustion gas, reconverting the condensed water to water
vapor with the heat obtained from said combustion, and feeding a
portion of the reconverted water vapor to a gas bag maintained
separate from the original lifting gas.
4. A method as in claim 3 including thermally insulating said gas
bag from the atmosphere.
5. A method as in claim 1 wherein the original lifting gas contains
a hydrocarbon and wherein the step of chemically converting
includes catalytically converting the hydrocarbon in the presence
of water vapor to hydrogen, carbon monoxide and carbon dioxide.
6. A method as in claim 1 wherein the step of chemically converting
produces hydrogen, said method further including generating
electrical energy with the hydrogen in fuel cells and propelling
the airship with blowers operated by the electrical energy.
7. A method as in claim 1 wherein the original lifting gas is
methane and wherein the step of chemically converting includes
reacting the methane with water vapor to produce carbon dioxide and
hydrogen.
8. A method as in claim 1 wherein the original lifting gas contains
a hydrocarbon and wherein the step of chemically converting is
carried out prior to take-off of the airship and produces at least
one of water vapor and hydrogen.
9. A method of operating an airship substantially without need for
liquid or solid fuel for motive energy, the airship employing as a
lifting medium an original buoyant gas including a hydrocarbon as a
portion of the lifting medium, said method comprising: carrying
said original buoyant gas in said airship as the sole fuel for
generating driving power for the airship, chemically reacting at
least a portion of the hydrocarbon with a reactant to generate
power for operating the airship and to produce a buoyant reaction
product which includes a gas selected from at least one of water
vapor and hydrogen, and compensating for reduced buoyancy resulting
from the chemical reaction by taking the original buoyant gas from
one chamber containing the same and storing said buoyant reaction
products in gaseous condition in separate buoyant gas chambers.
10. A method as in claim 9 wherein the hydrocarbon is methane,
wherein the reactant is oxygen and wherein the step of chemically
reacting includes the step of reacting the methane with the oxygen
to produce carbon dioxide and water.
11. A method as in claim 9 wherein the hydrocarbon is methane,
wherein the reactant is water vapor and wherein the step of
chemically reacting includes reacting the methane with the water
vapor to produce carbon dioxide and hydrogen.
Description
This invention relates to a method for operating lighter-than-air
airships of the type which employs substantially natural gas and/or
hydrogen both as the lifting or buoyancy means and also as the fuel
for the power supply of the airship for the purpose to avoid the
necessity of carrying additional solid or liquid fuels for
generation of motion energy.
A proposal which has already been known for quite some time
(Giffard 1855, Paris) concerns a steamdriven airship the lifting
body of which is filled with illuminating (coal) gas. The proposal
contemplates providing the heat for the steam engine with coal and
compensating for the loss in weight which occurs as a result of the
use of the coal by burning appropriate amounts of the lifting
illuminating gas.
It has been also proposed in U.S. Pat. No. 3,456,903, the
disclosure of which is incorporated by reference, to consume
natural gas in similar combination with Diesel oil for the power
supply of the airship.
Another proposal contemplates using natural gas as buoyancy means
and carrying water as additional ballast and vaporizing said water
for compensation of the loss of buoyancy by burning the natural gas
for power supply.
Due to this proposal, however, the additional water ballast reduces
the lift of the airship from the beginning of a lift, thus also
reducing the available lift for transport of goods.
In recently built dirigibles with helium as the lifting gas, to
compensate for the loss in weight in liquid fuel resulting from the
operation of the driving means the water was condensed from the
waste gases of the internal-combustion engine, in order to produce
ballast and to reduce the lift and thus reduce the otherwise
necessary draining of expensive helium or hydrogen. The actual lift
being available for transport purposes on a flight crossing the
atlantic was about 15 metric tons, while the weight of the fuel
including the weight of the container for the fuel was about 60
metric tons.
As far as it is also known (Zeppelin LZ 127) to use gaseous fuel
for combustion engines such fuel is heavier than air and does not
effect any positive effect on the buoyancy.
The purpose of the present invention is to eliminate the necessity
of solid or liquid fuel and of any additional ballast, either.
Thus, the airship of the invention is intended to avoid loss of
free transport weight capacity or -- from another view -- can be
built with reduced volume of buoyancy. Furthermore, it is another
object of the invention to reduce the danger of fire by accidental
burning of liquid fuel, which fuel normally would burn from the
bottom of the airship while any used inflammable buoyant gas will
burn over the head of any cabin in a direction less dangerous for
passengers.
It is known from a photographic picture of the accident of the
airship Hindenburg at Lakehurst in 1937 that most of the passengers
could be rescued because of this fact while the rest of the
passengers died because of the burning Diesel fuel flowing out of
the destroyed fuel tanks after heavily touching the ground.
Inflammable gases when used in an airship are not as much dangerous
as generally believed, as long as such gases are under some
pressure and are enclosed in a zone of noninflammable protection
gas, because of the effect of flame out. The environed protection
gas should be lowly heat conducting like carbon dioxide, nitrogen
or argon and under a somewhat increased pressure in comparison with
the buoyant gas. Also by way of this increased pressure the
envelope of the airship can be built double walled; reference is
made to U.S. Pat. No. 3,456,093.
Accordingly, the invention is characterized broadly in that the
reduced lift resulting from use of the lifting gas is restored at
least partially by gas which is obtained through the chemical
transformation of the lifting gas or of components thereof. The
obtained gas either specifically or with respect to its volume has
at least the same total of buoyancy as the consumed original gas,
i.e., in this way it is possible to maintain the total lift of the
airship constant or even to increase it, which also makes it
possible that with the gas which is obtained in the transformation
the buoyancy effect, which differs according to the flying
elevation of the airship, can be adjusted or altitude-stabilized
through use of corresponding different portions of the transformed
gas.
Such transformation can be accomplished by separating water from
the exhaust gas of means for burning natural gas for instance
driving combustion engines, heating apparatuses or even steam
generating apparatuses and reheating and revaporizing said water
preferably by use of the excess heat of said converting means. The
generated steam, then, is transferred to the buoyancy chambers of
the airship.
According to the invention the transformation of the natural gas
can be accomplished by chemically breaking it down in the presence
of water vapor in order to produce hydrogen gas to be employed
partly for compensation of buoyancy and partly for the operation of
fuel cells and other electric means. The transformation can be
performed prior to starting the airship as well as during the
flight.
According to the invention the specific overall buoyancy volume per
weight to be transported can be surprisingly reduced because any
additional lifting force for the motion fuel is avoided. Also the
weight for the construction of the fuel containers is not necessary
any more. Thus, the overall volume of the airship of the present
invention only depends on the weight of its specific construction
and on the desired capacity for transport weight.
If, for example, we proceed from the combustion of methane heated
to 100.degree.C by way of saturated water vapor being contained in
chambers contacting the cells containing the methane and if we
replace step by step its lifting volume having a lifting force of
0.77 kg/m.sup.3 in environed air of 0.degree.C by water vapor of
approximately the same temperature having a lifting force of 0.695
kg/m.sup.3, then we require for constant lift for 1 volume of
methane approximately one quarter more of water vapor. For
substitution of the natural gas by water vapor with respect to
constant lifting force only 62.5% of the water component gained by
the cleavage process is needed. In replacing the volume of natural
gas the water vapor by way of its one-quarter excess volume
replaces also an adequate volume of heated air being provided in
the compensation cells. Thus, by loss of the replaced heated air,
having for instance a temperature of 100.degree.C and a lifting
force of 0.35 kg/m.sup.3, which loss increases because of expansion
of the air with increased altitude of the flight, the airship
maintains a definite altitude. With increasing replacement of air
by vapor the lifting force increases and vice versa. Thus, in order
to stabilize the altitude of the flight, it is one principle of the
invention that the lift of consumed original gas is substituted by
water vapor replacing with its increased volume an adequate volume
of warm air being contained in the compensation cells.
The delivery of warm air from the compensation cells, which
delivery, depending on the more expansion of the gases with
increased altitude, is about 10% per kilometer, has to be restored
if the airship decreases. In order to perform a stabilized flight
without dropping ballast weight this restoration of lifting force
is accomplished by taking into the compensation cells an adequate
amount of air and heating it up to for instance 100.degree.C, for
which heating preferably the excess heat of the combustion engines
is used.
Furthermore, according to the invention it is contemplated to
employ a portion of the hydrogen produced by the cleavage process
of the buoyant natural gas after removing the carbon dioxide for
oxidation in fuel cells to generate electric power by means of
which electric motors of the main blowers for driving the airship
and of auxiliary equipment is supplied. If the electrically driven
blowers are equipped for normal flight speed in time of top power
circumstances additional combustion engines having a relatively
light specific weight can be used.
The necessary power for driving the airship can be remarkably
additionally reduced if the principle of removing the boundary
layer by suction is applied or the outer surface of the keel of the
airship; see U.S. Pat. Nos. 3,319,593, 3,410,510, 3,348,622 and
3,435,654. The airship is also covered by a foil of aluminum having
a hydrophobic surface layer of fluoro carbon resins (U.S. Pat.
application Ser. No. 808,636) which layer keeps the air flow along
the airship in laminar condition and the friction low. By use of
these principles the consumption of natural gas for driving
purposes is reduced and an adequate excess volume of the buoyancy
can be filled with other buoyant gases, like for instance helium or
hydrogen, which do not need to be changed or converted.
The method according to the invention can also be performed if the
saturated steam has another temperature than the natural gas. For
instance, the lifting force of natural gas at a temperature of
57.degree.C is the same as of water vapor at 100.degree.C. Under
such conditions also the volume of the natural gas to be replaced
by vapor is the same as of the vapor and it is not anymore
necessary to remove an excess of warm air from the compensation
cells in the course of the change of water vapor for natural gas,
constant altitude provided. By way of this effect the
interchangeability of the gases can be controlled over a wide range
of temperature and the energy of the gases can be used more
effectively.
By conversion of 1 mol of methane aside from the carbon dioxide the
volume of the produced water-component is twice the methane volume
(2 mol) due to the equation
CH.sub.4 + 20.sub.2 = CO.sub.2 + 2H.sub.2 O (1)
in the preferred embodiment of the method according to the
invention the natural gas or any other hydrocarbon gases gained
from natural oil, especially methane, is cleavaged in the presence
of water vapor by partial oxidation into gaseous hydrogen, whereby
an increased volume of gas is achieved. This conversion is
performed by two main steps of the following reactions which are in
general already known from the production of synthetic
fertilizers:
CH.sub.4 + H.sub.2 O = CO + 3H.sub.2 ( 2a)
CO + H.sub.2 O = CO.sub.2 + H.sub.2 ( 2b)
CH.sub.4 + 2H.sub.2 O = CO.sub.2 + 4H.sub.2
The carbon dioxide component can be freezed out although its
diminishing effect on the lifting force is only about 10% of the
hydrogen heated at 100.degree.C being contained in the buoyancy
chambers. Thus, separation of the carbon dioxide is not compulsory
and any additional equipment can be omitted.
For performance of reaction (3) rain water collected from the outer
surface of the airship can be used.
The necessary water can be obtained also from the exhaust gas of
burned natural gas along (1) of the following reactions:
Ch.sub.4 + 20.sub.2 = co.sub.2 + 2h.sub.2 o (1)
ch.sub.4 + 2h.sub.2 o = co.sub.2 + 4h.sub.2 ( 3)
2ch.sub.4 + 20.sub.2 = 2co.sub.2 + 4h.sub.2 ( 4)
thus, the lifting force of 1.5 kg of the consumed 2 m.sup.2
CH.sub.4 having a temperature of 100.degree.C the produced 4
m.sup.3 H.sub.2 at 100.degree.C have a lifting force of 4.9 kg
after reduction by the additional weight of 0.4 kg of the produced
2 m.sup.3 CO.sub.2 (at 100.degree.C). The gained new lifting force
after conversion of the gases is about: 4.5 kg - 1.5 kg = 3 kg. Due
to the remarkable increase of lifting force two third of the
produced hydrogen may be used for other than buoyant purposes.
According to reaction (3) by the use of water vapor already
existing as buoyant gas a new lifting force of 2.75 kg is also
gained.
This transformation which is given in the example and which occurs
primarily in natural gas (i.e., the transformation of methane) is
similarly valid for other hydrocarbons according to the invention,
for example:
C.sub.8 H.sub.18 + 8H.sub.2 O = 8CO + 17H.sub.2 ( 5)
8co + 8h.sub.2 o = 8co.sub.2 + 8co.sub.2 ( 6)
c.sub.8 h.sub.18 + 16h.sub.2 o = 8co.sub.2 + 25h.sub.2 ( 7)
the supply for reaction (7) can be performed by taking up a storage
of gaseous hydrogen at a natural oil well. Similar to the
conversion of methane the reactions (5) (6) and (7) can be
performed in presence of catalysts like for instance chromium oxide
and zinc oxide or nickel oxide or the like.
The saturated water vapor serves as a supply source for heating the
buoyant gases constantly at or close to 100.degree.C whereby the
vapor is partly condensed. By heating the gaseous hydrogen the
increase of lifting force is only 27 g/m.sup.3, however, the volume
of the hydrogen increases to the 1.367-fold. Thus, one cubic meter
having a weight of 0.089 kg at 0.degree.C after being heated to
100.degree.C is able to substitute 1.767 kg air (1.367 .times.
1.293 = 1.767) and the increase of lifting force resulting from
that replacing the air is from 1.21 kg to 1.678 kg at height above
sea level (760 mm air pressure).
Due to the consumption of water from ballast according to the
abovementioned reaction (3) an additional amount of lifting force
is obtained and the overall increase in lifting force by conversion
of one cubic meter natural gas at 100.degree.C is even (4 .times.
1.23) + (2 .times. 0.598) - 0.77 = 5.34 kg, without consideration
of the carbon dioxide.
The necessary heat consumption for the above-mentioned reaction (3)
is preferably covered by the excess heat of the combustion
engines.
It has to be mentioned that by use of the saturated water vapor the
buoyant gases can be maintained even at a less high temperature if
the saturated water vapor is mixed with other gases. In such
mixtures of gases the partial pressure of the saturated water vapor
can be varied. For instance at a partial pressure of 92.5 mm
mercury column or 0.083 kg/m.sup.3 the saturated condition of the
water vapor exists at a temperature of 50.degree.C.
The main advantage of the method according to the invention is that
the buoyant gas can be used for driving the airship without need
for any solid on liquid fuel or additional ballast to compensate
the consumption of the fuel buoyant gas. Consequently the airship
operated in accordance with the invention can have a remarkably
reduced overall volume or an adequately increased capacity of
lifting force available for transport purposes.
The invention will be further understood from the following more
detailed description taken with the drawing in which:
FIG. 1 is a schematic vertical sectional view of an airship driven
according to the invention and having several separate chambers or
cells within its body and a frame structure, indicated with dashed
lines, within which all of the necessary equipment for the
operation of the airship is installed as illustrated by means of an
enlarged schematic: and
FIG. 2 is a partial schematic representation of the catalyzer
reactor of FIG. 1.
The airship which is shown in FIG. 1 has a foldable pressure
airship hull 1 with properties which are as highly heat insulating
as possible, in particular against heat losses from the inside of
the airship to the atmosphere and, for example, with a construction
according to U.S. Pat. No. 3,456,903. Inside of the chamber 39
which is encompassed by the double-walled pressure airship hull 1
there are one or more separating intermediate walls 3a, 3b and 3c
which can be turned inside out within the airship hull and which
are composed preferably of flexible material. Individual walls
thereof can also be constructed as being heat insulating. These
separating intermediate walls are preferably arranged symmetrical
to the airship center.
The separating intermediate walls 3a, 3b and 3c subdivide the
chamber 39 into chambers 41 which are separated from one another
and which are equipped for cold air or heated air, for example by
means of inlet and outlet connections 41a, and are used as lift
compensating cells according to U.S. Pat. No. 3,456,903 the
disclosure of which is incorporated here by reference. Chambers 43
are filled with water vapor under saturation vapor conditions
(100.degree.C) at least in the proximity of the wall. These
chambers have an inlet and outlet connection 43a. Based on the
invertible gas-tight separating intermediate walls the volumes in
the chambers 41 and 43 are extraordinarily greatly changeable
either in reciprocal dependence or at the cost of the free volume
of the chamber 39 and, in all practice, to such an extent that the
separating intermediate walls touch each other mutually in the
longitudinal center of the airship and the volumes of the chambers
41 and 43 completely fill out the volume of the chamber 39. This is
correspondingly valid when, additionally to the chambers 41 and 43
through the separating intermediate walls 3a there are also
provided separated chambers for impellent gases, preferably gases
which produce lift, such as for example natural gas, methane
(CH.sub.4) or similar. Optionally, hydrogen can also be contained
in these chambers. These chambers have an inlet-outlet connection
37a.
The centrally located chamber 39 contains very general lifting
gases, for example also hydrogen (H.sub.2) or other lifting gases
including gas mixtures (even water vapor/gas mixtures) and has
inlet-outlet connections 39a and 39b. The handling of water vapor
or water vapor/gas mixtures is accomplished within the
heat-insulated tight airship hull according to U.S. Pat. No.
3,456,903.
The chambers 39, 37, 41 and 43 are preferably filled symmetrically
to the longitudinal center of the airship, but an asymmetric
filling can also be provided for the purpose of trimming the
airship. In addition, there can also be provided a so-called
"ballonet" or storage chamber 45 for protective gas which is used
preferably for filling the intermediate space of the double walled
pressure hull. This chamber 45 has an inlet-outlet connection 45a.
As protective gas one can use carbon dioxide (CO.sub.2) and/or
nitrogen (N.sub.2) and also air, which are preferably dried.
The filling of the chamber 39 with combustible lifting gas, for
example natural gas or methane (CH.sub.4), is done by means of
inlet and outlet connection 39a, 39b through a control valve 49
which is provided in the pressure airship hull 1. In order to
prevent damage from excess pressure the airship hull has preloaded
outlet relief pressure valves 51. Water vapor can also be filled in
directly from the outside through the inlet connection 43b into the
chamber 43, whereas the chambers 37 can be filled with hydrogen gas
through the inlet connection 37b. The inflammable lifting gas
(CH.sub.4) from the chambers 39 and/or 37 is converted to hydrogen
successively in the amount of the required power, for example in
the catalysis apparatus 60, and the water which thereby is created
is fed through waste gas pipes 47 to water vapor producers 35 and
heated there before it is fed into the chambers 43. The apparatus
60 may employ chromium oxide/zinc oxide or nickel oxide as the
catalyst. The hydrogen which occurs during the transformation is
fed to a fuel cell device 23 and 23a which also has storage
batteries for the purpose of creating electrical power and which is
started centrally from a control station 24 and for example by
means of regulators (speed-controlling devices 61) which is
connected into the central electrical lead pipe 24a. The electrical
connections belonging to the control devices 61 for speed and
capacity control of the electrical motors are shown in FIG. 1 as
short-dashed lines.
The main propulsion for the motion of the airship is provided by a
double-staged main blower 33 which preferably can be driven by
combustion motors or gas turbines, for which purpose the
inflammable lifting gas which is contained in the chamber 39 is
used as fuel. The airship moves by means of the forcing out of air
from an annular nozzle 9 of a main nozzle 11 provided on the rear
of the airship, whereby the propelling air is fed through a
connection 34 into a channel 15, as disclosed in U.S. Pat. No.
3,456,903 the disclosure of which is incorporated by reference. The
airship assembly 13 with steerable rudders 13a is connected to the
cone 45 of the ring-slot nozzle 13a. An auxiliary blower 31 is used
for propelling the airship during slow travel or normal travel.
A small blower 25 with electrical motor 25a is also provided which
is used for maintaining the protection gas pressure in the
intermediary space of the double walled pressure hull 1. Another
blower 27 with electrical motor 27a fills the chamber 41.
Finally there are also heat exchangers 55, the connecting leads of
which are however not represented in detail, as well as a device 57
for condensing water vapor preferaby of water components contained
in the exhaust gas. In these devices 57 parts are also
appropriately contained which can remove the carbon dioxide
(CO.sub.2) from the converted gas.
According to the schematic representation of FIG. 2 the reaction
heat which is released from the catalytic conversion of natural gas
or methane to hydrogen can be used for the production of water
vapor. This can also be achieved preferably together with the heat
transfer from exhaust gas heat.
The exhaust gases can be fed to the channel 15 so that they can
also be used for the lifting power of the airship.
With the above-mentioned devices the utilization of the inflammable
gases used at the starting, therefore above all natural gas or
methane (CH.sub.4) or even hydrogen gas, can be obtained in the
most varied manners in which they are taken from the chamber 39 (or
37) and converted to replace the loss of lifting power by means of
those exhaust gas components which themselves provide a usable
lift, i.e., hydrogen gas and above all water vapor. This is
possible in the most diverse variations so that in the figures by
far not all of the possibilities are shown. In this way the lifting
force can be regulated on a practically continuous basis by
controlling the different lifting forces.
* * * * *