Note : Les descriptions sont présentées dans la langue officielle dans laquelle elles ont été soumises.
2l4~GZ~ 7
~ / r~
SP~C I~CATION .
The Inner Support Based Electromagnetic Propulsor is an engine
useful is the controlleà propulsion of air and space vehicules.
In the p~esently used flying machines, all flying machine engines
rely on~ air or the exploding of gaZes for propulsion. Most flying
machines are limiteà to one type of fligh~ from guidance point of
wieYI or with respect to airspace or space environnement.
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Page 2. r.
As it is known fast motion between a liquid and a heavier solid
can maintain the heavier solid on the surface of the liquid. Also
as it is kno~m, during magnetic attraction or repulsion the same
strenght of force acts on each side of the magnetic action.
I have found based on these facts the invention of an electromag-
netic propulsion engine comprising the flight capabilitys of all
previous machines in one by having a support base within, a new
concept in propulsion and flight. The engine can be made to operate
with electromagnetic attraction or repulsion or both. ~Nith a sys-
tem of attraction an iron or ferroma~netic plate can be used to
be attracted to the electromagnet, but there is a greater magnetic
strength if both parts are electro~nagnets.
Basic description as follows: Electro~agnets are firmly rnounted on
the outside support plates installed on t~le rib extensions of a
circular specially shaped container in which liquid mercury is cir-
culated or rotated by a paddle-w~leel at high speed and thorough
hole openings on said container, rods, leaning on hinge like flaps
on the high speed liquid mercury inside said container, while with
they opposit ends supporting the at traction plates above the said
electromagnets. When the electromagnets are- activated, the attrac-
tion plate, rod and flap units exerce a force on the high speed li-
quid mercury inside the said container, while an opposit force i8
exerced by the electromagnets on the container. The attraCtiOn
plates should not arrive in contact with the electromagnets and the
force of the speed of the liquid mercury should be greater on the
flaps maintaining the rods, then the force of the attraction. Each
.
21~5~07
Page 3. r.
activation realizes a jolt on the container in the direction vanted
while the opposing force is nulliried or overwhelmed by ~he high
speed mercury inside the said container.
The engine comprising a multitude of rod, attraction plate and
electromagnet units on t~le same cont~iner on top, bottom and sides
all around. Also mounted firmly on the rib extensions, a large wa-
sher shaped plate as mutual attachment, a second container identi-
cal but of o~posit inner construction, its paddle-wheel having an
opposit direction of rotation realized by a gearbox insert~d bet-
ween the axles rotated by an electric motor both secured to they
respective support plate. ~ach electromagnet is contacted for acti-
vation by switches at a flight control bo~rd and activated by three
turnables knobs for the number of activation vanted per second, a
knob for up, one for down and on~ for lateral. Activation should
be the same on the two containers to avoid rot~tion. The top of the
first container an~l the bottom of t~l~ second container are finished
off with washer like plates respectivly, allowing on the bottom the
input electric wires to t~le electric motor and on the top the elec-
tric wires connectin6 the electromag~nets to the control board. It
must be noted that said containers can be m~de dif ferently and cir-
culating of said mercury in them can be acheived in different ways
but no matter the shape or size they should not be fillea with li-
quid mercury to saturation, only at the needed level.
The electromagnets are made in a known way and to ha~e greater mag-
netic force, the attractiOn plates can be replaced by electromagnets
or a solenoid type electromagnet could be used and the rib extensi-
21~07
Page 4. r.ons could be increased if more place is needed for said magnets.
~he generating of electricity needed are produced in a known ~11ay
and all the electrical system should be installed the usual way.
When making the engine for specifics, common engineerin~ processes
should be used with reg~rd to practical shortcuts and usual practi- ==
cal procedures to material compositions or strengths. Many minor or
ma~or varlations are avail.~ble and still retaining the same concept.
In drawings which illustrate embodiments of the invention,
Figure I, is an exploded perspective view with parts broken away
of the main features of the container.
Figure 2, are two exploded perspective views of parts broken away
of the activity section's construction and differences,
A. ciockwise, B. contreclockwise rotation of paddlewheel.
Figure 3, are two perspective, half cut views of parts broken away
f ~. non activation's and B. the activation's assemblys.
igure 4, is a perspective view, with parts broken away of the up-
per container's assembly.
Figure 5, is a perspective view, with parts broken away of the full
propulsion engine ' s assembly .
Figure 6, is a schematic illustration of the flight control board.
Figure 7, i8 a schematic illustration of possible emplacements Of
main composants in a flight craft.
Figure I, as the main parts of the container, where (I) the down
section is a slightly cone shaped disc with (2) hole-emplacement
for ballbearing housing in the centre and (3) the activity section
with (4) emplacement for hinge like flaps on the inside and (5) em-
214~Q~
Page 5 . r.placement of screwable rod-linin~s acrosse, also having (6) an exit
valve to empty said container. The rim of the disc (7) is angled
and holes (8) are drilled in the disc and acrOSSe the flap emplace-
ments to permit introduction of holdin~;-pin, while also having lar-
geur (9) holes acrosse for assembly purposes with nuts and bolts.
On the outer side of said disc are sixteen (IO) rib-extentio~s wel-
ded on ~rrith prearranged lloles for, ( II ) rod-guide-plate securing,
(I2) for electromagnet-holding-plate securing, (I3) for the gearbox
or electric motor support-plate securing and (I4) the rib-joint-
plates mountings. The rib-extensions are havin~ on them (I5) acco-
modations with (I6) holes acrosse to secure the large lrasher like
finishing plate.
The (I7) paddle-~heel is a slightly cone shape thick disc with (I8)
hollow sections and (I9) the paddles which circulate between the
activity sections, having in its centre (20) a square shaped hole
to accomodate the axle or drive shaft, givin~ the rotation to said
wheel, ll~hich should not be in contact ~ith its surrondin~s which
are stationary with respect to rotation and for security reasons
(2I) small wheels are mounted on both side toavoid friction on pos-
sible occasional contacts.
The (22) lateral-ring is having sixteen (23) rib-extensions welded
on with prearranged holes (24) for rod-guide-plate securing, (25)
for first level electroma~net-holding-plate securing, (26) for se-
cond level electroma~net-holding-plate securing and (27) the rib-
joint-plate mountings, where (28) is the rib-joint-plate with holes
(29) to permit said mountings by nuts and bolts. The ring is fully
an (30) activity section with its (3I) rims angled to accomodate
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Page 6 . r.
assembling, secured by nuts and bolts acrosse (32) holes and also
having (33) holes to allow introduction of holding-pins thorough
(34) flap emplacements beside (35) rod-linin~ em~lacements.
The (36) up section of the container is slightly cone shaped while
the (37) activity section angles off to horizontal only showing
(38) rod-lining emplacements and (39) rim angled to ~ccol-llodate as-
sembly to be secured by nuts and bolts acrosse (40) holes and holes
to permit introductioll of pins, since all t~le ~ctivity sections are
having similar construction. (4I) is a closable opening to fill with
mercury the container, while (42) is the emplacement of the ball-
bearing housing in the usual manncr. The (43) rib-extensions welded
on having prearranged holes (44) for rod-guide-plate securing,
(45) for first level electrom~gnet-holding-plate securing, (46)for
second level electroi~iagnet-holdin~-plate securing and (47)rib-joint
plate mountings. The rib-extensions having on them (48)accomodations
with (49) holes acrosse to secure the large washer like plate.
Figure 2, illustrates construction of all the activity sections, in
(A) the clockwise rotation of the pad(ilewheel (50) is t~le direction
of the flow of mercury, where (5I) is the inside Or said activity
section' s wall with (3I) angled rim for assembling with nuts and
bolts thorough (32) hole. Said rim also having a smaller ilole (33)
to permit introduction of (52) flap-holding-pin thoroug~h (34) flap
emplacements and (53) tubes like extremity of (55) flaps which are
thin plates covering (35) the rod-lining-emplacements where (56)
the rod-linings are screwed in. Said rod-lining's (57) hollow tube
inside permits the rod-end to go thorough it, to make contact with
21~07
Page 7 . r.
said flaps. The rod-linings could have a lubrication system mounted
on them if needed. In (B) l~hich corresponds to the same activity
section as (A) but in the second container with contreclockwise ro-
tation of the paddlewheel, (58) is the direction of the flow of mer-
cury and all the componants .~re mounted accordingly. To summeri~,
in all activity sections the mounting of flaps should be such, that
the force of flow of said mercury, push said flaps against the wall
of the container, over .~nd covering the corresFonding rod-lining em-
placements. Said flaps when not activated should present the less
possible opposition to th~ flow of the mercury.
Figure 3, is illustrating; in (A ) non activation of a flap, rod and
electromagnet unit in its simplest form vlhere (I9) is the paddle
part of the paddleulheel with (50) direction of rotation and also
flow of (59) mercury, illustrated by dots, having above it (55)
flaps and (37) wall of activity section of t~le container with (56)
rod-lining installed and (52) holding-pin acrosse (53) tube like
flap extremity. The rods are made up of minimum t~;o pieces and when
the need arises several extensions are used. In this drawing the
part making contact with the flap called (60) rod-end have mouve-
ment possibility acrosse the rod-lining and the hole of (6I) rod-
guide-plate, above which it is joint with an elongated nut called
(62) rod-joint to the (63) plate-rod which in turn have mouvement
possibility acrosse the hole of (6~) t~e electromagnet-plate-hol-
der and a-~hole of (65)the electromagnet to be topped off by screw-
ing means by (66) the attraction-plate, above said electromagnet.
Said attraction-plate is also having a hole in it by which (67)
21~07
Page o . r.
the attraction-pl.~te-~uide is screwed in the electromagnet, to ob-
struct rotation of the attraction-plate and limit said plate's dis-
tance from the electromagnet, which have the usual (68) windings
and is secured by (69) scr e~s to th~ electromagnet-holding-plate.
In illustration (B) t~le activation processe is demonstrated where
the flap (55) is op~osing the flow of the mercury (5f) and it
must be noted that tlle attraction-plate should not arrive to the
electromagnet, me~ning, the flap at 45 angle should receive from
the flow of the mercury a greater force than the force of the elec-
tromagnetic attraction, also the paddle (I9) is never contacting
the flap. Note that (67) tlle attraction-plate-guide haved not
mouved with the attraction-plate.
Figure 4, is the upper ~lalf of th~ propulsor illustrating assemb-
ling, to give sense to figures I, 2 and 3. In it (36) the up sec-
tion with its (43) rib extensions, (22) the lateral ring with its
(23): rib extensions and ( I ) the down section with its (IO) rib
extensions, each of these three parts have (3I) angled rims to fit
and to be secured by nuts and bolts thorough (32) holes, after, the
(55) flaps haved been installed and holding pins inserted thorough
them by ( 8 ) holes and (I7~ the paddlewheel v~ith its (I93 paddle
and its (2I) security ~vheels, is placed betveen (70) the ballbea-
ring housing of the up section and (7I) the ballbearing housing of
the down section of said container. One end of (54) axle is intro-
duced in the centre of said paddlevlheel and said ballbearing hous-
ings while the other end is connected to (72) the gear of (73) the
gearbox secured by (74) nuts and bolt means to (?5) the gearbox-
214~007
.
Page 9 . r .platform, shaped to fit and to be secured also by (76) nuts and
bolts to the down section~s rib extensions. The gearbox is contain-
ing (77) two side gears to realize opposit rotation from (78) gear =~
of (79) the drive-shaft. (50) is the direction of rotation o~ said
paddlewheel, while (58) is the rotation of the drive-shaft. The rib
extensions (23) o~ the lateral ring are secured on top to (43) the
ribextensions of the up section and on the bottom to (IO) the rib
extensions of the down section, respectivly by (28) ri~- joints by
(~9) nuts and bolts. As said cont~iner is assembled it is forming
(80) t}~e activity-area ~Jhich is a full circle cavity where the mer-
cury, shown by dots, is circulated by (I9) th~- paddle of the paddle-
wheel. The activity sections or the activity area~s walls are having
(35) rod-lining emplacements, where the rod-linings are screwed in.
Mounted paralell to the activity area v~alls between and on the res-
pective rib extensions are (8I) the rod-guide-plate down section,
(82) the rod-guide-plate lateral ring and (83) tlle rod-guide-plate
up section, said rod-guide-plates ~re having on them (84) accomoda-
tions for securing thorough the pres-drilled ( 44) holes, by nuts
and bolts on said rib extensions. Each rod-guide-plate is having as
many (85) holes on it ~s its respective activity area wall has(38)
rod-lining emplacements, to permit (60) the rod-ends to slide in
both, to contact the respective flaps inside said activity area.
Further from the activity area wall past the rod-guide-plates and
paralell. to both are mounted on and between the respective rib ex-
tensions (86) the electromagnet-holding-plates down section, (87)
first level electromagnet-holding-plates lateral ring and (88) the
first level electromagnet-holding-plates up section, each having on
~.~
21~ 7
Page IO. r.
them (89) holes to perinit mouve-~ent of (90) the rod-extensions or
(63) the plate-rods thorough said holes and holes of (65) the elec-
tromagnets which are secured by screws to said plates which in turn
have (9I) accomodations for securing by nuts and bolts thorough pres
drilled (45) holes. The up section is having a (92) second level of
electromagnet-holding-plates installed and secured the same fashion,
also the lateral ring is having (93) a second level electromagnet-
holdin6-plates with holes and (94) accomodations to be secured by
nuts and bolts thorou~h (46) pres drilled holes on the respective rib
extensions. There can be as many levels of electromagnet-holdin~-
plates as the size of electro~nagnets needs space of installation. The
(60) rod-ends are secured to (90) rod-extensions by (62) rod-j~ints
and the (63) plate-rods connected similarly and having mouvement pos-
sibility acrosse (65) the electromagnets and past said electromagnets
the (66) attraction-plates are screwed on said plate-rods. The att-
raction-plates havin6 thorou~h the~n (67) the attraction-plate-6uides
screwed in said electromagnets. The (43) up section's rib extensions
are having on them (48) ~ccomodations to secure on t~lem (95) the
upper- r~ nl :hi ng_plate whic~l is shaped like a l~rge washer, while on
(IO) the down section's rib extensions are similar (I5) accomodati-
ons to be secured to (96 ) t~le mutual-securing-plate also shaped as
a large washer, meaninig it fully covers and only covers the strait
edges of said rib extensions. It is understood that all sixteen em-
placements between the rib extensions should be fully mounted and
they are similar ~lith the exeption of one where (6) the mercury exit
valve is and (4I) the mercury input, a closable opening is. It should
he noted that only the needed amount of mercury should be used and
21~007
Page II . r.
the most possible units of flaps, rods and electromagnets should be
installed. The electric ~ires should be installed in a usual manner
connected to the control bo~rd.
Figure 5, is the illustration of the assembling of the full propul-
sor without the electrical wirein6, which should be connected in a
known way. The propulsor is made up of (99) the upper container and
(IOO) the lower container the functionning of both is the same only
opposit to each other. Both having (I7) the paddlewheel, (I9) the
paddle, (80) the activity area with the liquid mercury illustrated
by dots, (55) the flaps aligned oppositly in each container, (65) the
electromagnets, (66) the attraction-plates, (60) the rod-ends, (90)
the rod-extensions, (63) the plate-rods, (6I)-(ôI)-(82) the rod-guide-
plates and (93)-(87)-(92)-(89)-(86) the electromagnet-holding-plates
installed and mountcd as ~lentionn~d previously. The apparent diffe-
rences start with (50) the clockv~ise direction of rotation of (54)
the axle, (73) the gearbox on (75) the gearbox-platform all relating
only to the upper sontainer, vrhile tlle lov~er container have (58) thc
counterclock~ise rotation of (79) the drive shaft from (97) the elec-
tric-motor giving the rotation of the paddlewheels inside both con-
tainers and said motor is secured by (98) nuts and bolt means to(I02)
the electric-motor-platform secured by usual (76) means and ways.
Said lower container is secured on top to (96) the mutual-securing-
plate and on the bottom to (IOI) the lower-finishing-plate. It is
preferable that the electric-motor's speed of rotation is fully con-
trollable, for slow starting.
Figure 6, ig illustrating the control board concerning only guidance
' ~
~145~7
Page I2. r.
and speed control of t~le propulsors, since said control board is
for a two engines fl~-craft in this case. While the drawing illus-
trates for practical reasons two ~alf circular shapcs, it should be
considered that it represents the circular shape of the propulsors
where the corresponding parts relate to said engine with (I03) rib-
divisions, meaning, (IOLI) the respective spaces between the rib-ex-
tensions on the engines. ~ach square is (I05) the contact-pushbutton
for activation, for several electromagnets, in this case the six
electromagnets beside the corresponding rib-extension on the upper
container's lateral-ring" first engine, therefore the corresponding
circles of the cont~ct-pushbuttons are as follows: (I06)the lateral-
ring up~er container first engine, (I07)tne lateral-ring lower con-
tainer first engine, (IO~) t~le lateral-ring upper container second
engine, (IO9)the lat:eral-ring lo~er container second engine, (IIO)
the up-section upper container first engine, (III)the up-section
lower container first engine, (II2)the up-section upper container
second engine, (II3)the up-section lower cont~iner second engine,
tII4)the down-section upper container first engine, (II5)the down-
section lower container first engine, (II6)the down-section upper
container second engine, (II7)tile down-section lower container se-
cond engine. The (IIô) crosses illustrated rne~ning, that particular
contact-pushbutton and the corresponding electromagnets are on po-
sition (ON) for activation. What was described above is the foncti-
onning of the guidance or the steerin~. The following relates to
speed control, where (II9) the activation-part of the control board
having (I20) the down-knob, (I2I) the up-knob and (I22) the lateral-
214~0~7
Page I3. r.knob ~Ihich are turnables and ~lavin~ on the~ arrows to point on the
respective (I23) calibration ~v~len s~id knobs are turned. The calib-
rations are only examplary and they signify the numbre of activation
per second realized by known electronic means and said numbre of ac-
tivation should be as many as possible. As the example in the draw-
ing all thc up-sections are contacted for~ and ar~ having fifty acti-
vations per second to keep the craft in levitation ~vhile the lateral
electroml~6nets are contacted only in (I24) sector and are having
sixty activations per second giving t}le craft an acceleration in the
(I25) direction. Many ot~ler alternatifs are possible in the same con-
text and all the electrical and electronic systems are known and
should be applied accordingly. The control board should have all
the many other obvious switches concernin~; the motor, the generator
and various other componants.
Figure 7, illustr~te a flight craft Iqith it's main componarlts empla-
cements, where (I26) is t~le crosse cut perspective wiew of the flight
craft of a sphere shape, slightly fl~ttened on top and bottom, vJith
three levels inside, (I27) the control level, (I28) the propulsor
level, (I29) the generator level and said three levels are also il-
lustrated from top wiew, pointed out by arrOwS. The control level ha-
ving (I30) windows all around and in the centre (I3I) the control-
board with (II9) the activation part of said board and (I32) passage
hole in (I43) the floor to accesse by ( I33) the fixed latter the pro-
pulsor level where two (I34)propulsor engines are installed from the
side thorough (I35) the rernovable p~nels of (I36) the shell of said
craft in a tunnel shaped by (I37) beam-frame, crossing said propulsor
214~007
.
Page I4. r.
level. ~he propulsors are secured between ( I38) solld barres, screwed
to (I44) the floor llaving a (I39) passage-hole, where (I33) the fi}~ed
latter continues to the generator level where tw~ (I40) motors are
rotating the respective (I4I) generators to produce the electricity
and the motors are secured on (I42) the bottom floor while (I45) the
fuel tanks are installed on the inside wall of the shell which have
a (I46) door to accesse outside. The electrical wires are crossing
on all levels to respecti~le destin~ltions in ~ known, orderly manner.
The many obvious details are not illustrated and are self evident. It
can be realized th~t many propulsors can be installed depending on
the deslgne vanted. Life support systemes are also self evident.
~'~
214~07 l~
Page ~i. r.
The following informations, wit~ several options are only made to
transmit a better ins~ght and some bases for calculations and should
not limit or restrict the invention in any way.
The squetch is a crosse cut wiew of a half container, not showing
the paddle of the paddlewheel.
~5cn~
Each container have approximetly I50 liters of circulated or rota-
ted liqid mercury. Each flap is 4 ~o 6 square-cm. The maximum dis-
tance of the attraction-plate from t~le electroma6net is I to 2 cm.
Each electromagnet should ~lave a ~?ulling force of I5 to 20 kg, at
its maximum, meaning ~hat the force of the speed of the mercury or
its centrifugal force should be slightly more then I5 to 20 kg on
the flap. Therefore only one container ' up-section can realize a
jolt of 50000 kg force approximetly on each activation or as an
exemple with only two propulsor-engines jolts of 200000 kg are at-
tainable in fractions of a second. Good results are realizable with
smaller electromagnetic pulling force then mentionned.
When the speed of rotation of the paddle-wheel is difined, to have
the maximum opposition to the flow of mercury on the flaps, the row
of flaps on the up-activity-sections and on the down-activity-secti-
ons should be slightly an~led to realize a maximum opposition when
activated .
With respect to guidance it is possible with differently construc-
214~7 l~
Page ~.r.ted propulsors to havc the whole propulsor mounted in a directable
frame, therefore havin~g a different solution for ~uidance.
It should be noted again that normal good engineering procedures ~;
and solutions should apply when designing for specifics.
Index .
I. Down s~ction. 23.- Rib extension lateral ring.
2. Emplacement for ballbearin~- 24, Securing hole for
3. Down activity section. rod-guide-plate.
4. Flap emplacements. 25. SeCUrinlg hlletrOmra~net-hol-
5. Rod-lining emplacements. ding plate.
6. Mercury exit v~lve. 26. Securing hole for second le-
7. Angled riln. vel electromagn
8. Holding p~n=holes. 27. Hole for rib joint.
9. Rim assembling holes. 28. Rib-joint-plate.
I0. Rib extensions do~:in ~eCtion 29. Hole on rib-Joint-plate.
II. Securing hole for 30. Ring activity section.
I2. Securing hole for electro- 3I. ~ngled rim of rin~.
magnet-holdin~,-plate. 32. Rim's assembling holes.
I3. Securing hole for gear or 33. Hole for holding-pin.
motor plate. 34. Flap emplacements lat . ring.
I4. Securing hole for 35. Rod-lining empl~cements.
I5. Accomodation to secure 36. Up section.
washer like plate. 37. Up activity section.
I6. Securing hole on I5's 38. Rod-lining emplaceinents.
accomodation .
I7. Paddle-wheel. 39. Angled rim of (up sec. )
40. Assembling hole on rim up sec.
I8. I~ollow section of (I7).
4I. Mercury input emplacement.
I9. Paddle. 42. Ballbearin em lacement.
20. S~uare hole for drive shaft. g P
43. Rib extensions up sec.
2I. Small wheels.
44. Hole for rod-guide-plate secu-
22. Lateral ring. ring up section.
i~
~ 21~ 7
Page 25 . r .
Index .
45, Hole for first level electro- 75. Gearbox platform.
magnet-plate securing. 76. Gearbox platform securings,
46. Hole for second level elec-
tromagnet-plate securing 77. Side gears,
47. Rib-joint hole. 78. Lower gear.
48. Accomodation to secure washer 79. Drive shaft,
like plate up section. 80. Activity area,
L~9, Hole on accomodation. 8I. Rod-guide-plate down section,
50. Direction clockwise, 82. Rod-6uide-plate lateral sec,
5I. Inside of activity section 83. Rod-guide-plate up section.
52. Flap-holding-pin. 84, Rod-guide-plate securings.
53. Tube like fla extremity, 85. Rod-6uide-plate hole,
P 86. Electromagnet holding
54. Axle, plate down section,
55. Flaps. 87. Electromagnet ilolding, plate
56. Rod-lining, first level la~eral sec.
57. Rod-lining's hollow tube, 88. Electromagnet holding plate
58 Direction contreclockwise, first level up section.
59 Mercury. 89. ~oles on holding platc,
90. Rod extensions.
60. Rod-end,
9I. Securing accomodation for
6I. Rod-6uide-plate, holding pl~te first level,
62. Rod-Joint. 92. Electromagnet holding plate
63. Plate-rod, second level up scction,
64. Electromagnet plate holder 93. Electromagnet holding plate
first level, second level lateral sec,
65. Electro!nagnet, 94. Securing accomodation for hol-
66. Attraction-plate, ding plate second level,
67. Attraction-plate-guide, 95, Upper finishing plate,
68, Magnet windings, 96. Mutual securing plate,
69. Electromagnet screw, 97. Electric motor,
70. Ballbearing housing up sec, 98. Elec, motor securing means.
7I. Ballbearing housing down sec, 99~ Upper container,
72. Upper gear, IOO~ Lower container .
73. Gearbox, IOI, Lower fi ni ~hi n~ plate,
74. Gearbox securing means. I02,Electric motor platform,
21~D~7
Index, Page ~6.r.
I03. Rib divisions. I26. The crosse cut rriew of the
I04. Respective spaces (ribs) flight craft.
I05. Contact pushbutton. I27. The control level.
06. Lateral rin~ upper container IZ8- T~le propulsor level.
first engine. I29. The generator level.
07. Lateral ring lower container I30. Windows.
first engine. I3I. Tlle control board.
08. Lateral rin~ upper container I32 Passage hole control level
09. Lateral ring lower c0ntainer I33- Fi~ed latter.
second engine. I34. Propulsor engine.
II0. IJp section upper container I35. Remouvable panel.
first engine. I36. T~le shell of the craft.
III. Up section lower container - -
first engine. I37. Tunnel llke beam frame.
II2. Up section u2per container I38. Propulsor securing barr.
second engine. I39. Passage hole propulsor level.
II3. Up section lower cont~iner I40. Motors for generator.
second engine. I4I. Generator.
I4. Down section upper container I42. The bottom floor.
I5. Down section lower container I43- The control level floor.
first enBin~. I4~1. The propulsor level floor.
I6. Down section upper container I45. Thc fuel tanks.
second engine I1~6. T~le eYlt door.
I7. Down secl;ion lower contai-
ner second enginc.
I8. Crosses (on) position.
I9. ~ctivation part of cont-
rol-board .
20. Down knob.
2I. Up knob.
22. Lateral knob.
23. C~librations.
24. Lateral contact (eYample).
25. Direction of flight.
