US1890113A

US1890113A - Aeroship

Info

Publication number: US1890113A
Application number: US598578A
Authority: US
Inventors: Samuel E Hitt
Original assignee: Individual
Current assignee: Individual
Priority date: 1932-03-14
Filing date: 1932-03-14
Publication date: 1932-12-06
Anticipated expiration: 1949-12-06

Description

Dec. 6, 1932. s. E. HITT 0,

AEROSHIP Filed March 14, 1952 9 Sheets-Sheet 1 INVENTOR W \TNESS Dec. 6, 1932. s. E. HITT 1,390,113

r AEROSHIP Fileu Ma rch-14, 1952 g sheets-Sheet 2,

lNVEN-TOR Jame/5 4;?"

Dec. 6, 1932.

S. E. HlTT AEROSHIP Filed March 14, 1932 9 Sheets-Sheet 3 a, 1932. s. E. HITT 1,390,113

AEROSHIP Filed March 14, 1932 9 She'ets-Sheet 4 LEW \NVENTOR \NH'NESS Dec. 6,1932 5, HlTT 1,890,113

AEROSHIP Filed March 14, 1932 9 Sheets-Sheet 5 fimaawm I Jaw/5M m INVENTOR Dec. 6, 1932. s. E. HITT v 1,890,113

AEROSHIP Filed March 14, 1932 9 Sheets-Sheet 6 Q a a WWNESS 1 3! v LE W LEW MM INVENTOR Dec. 6, 1932. 5, H|TT 1,890,113

AEROSHIP Filed March 14,1932 9 Sheets- S heet 7 INVENTOR WH'NE'SS Dec; 6 1932. s, lTT 1,890,113

IAEROSHIP Filed March 14. 1932 9 ShaetS-Sheet 8 IN V ENTOR W \T N E55 Dec. 6, 1932.

S. E. HlTT AEROSHIP Filed March 14, 1952 9 Sheets-Sheet 9 WYTNESS 6M .6 WWW INVENTOR JMZZFM Patented Dec. 6, 1932 UNITED STATES SAMUEL a. 11mm, or ELYYRIAV, OHIO I AERO SHIP Application filed March 14, 1932. Serial-No. 598,578.

This invention relates to anaer o-planeship, hereinafter called an aeroship, atwo hulled seagoing vessel carrying air propulsion units and lifting planes and which at high speeds glides over the surface of the water or skips upon the crests of waves on an even keel.

The lifting planes are further described in my application, Safety surfaces for aerofoils, filed November 11, 1981, Serial No. 574,264. 7

My aeroship carries a thousand passengers and is equipped to provide them with the speed, safety, conveniences, comfort and luxury of modern travel.

In my aeroship the hulls are 600 feet long or more and are spaced 150 feet apart or more, to reduce rolling and pitching to a minimum.

In good flying weather, the aerofoils lift the hulls as the speed increases until they are almost out of the water and the water resistance is reduced to a minimum.

My aeroship is equipped with sixty thousand horse power, consisting of thirty-two, 1500 horse power air propulsion units and four, 3000 horse power steering units, and has a cruising speed of eighty miles an hour and x a maximum speed of one hundred miles an hour, crossing the Atlantic Ocean in twentyfour hours. I

When running at such speeds my aeroship maintains an even keel and does not roll.

In case the aeroship runs into afog or bad weather and comes to anchor to ride out the storm and a high sea is running,the ship is put to a severe test.

The two hulls are therefore positively and pivotedly connected in such a way astoleave each hull free to ride the waves, i. e., to pitch independently. 1

The two hulls are spaced and pivotedly connected fore and aft by aerofoils ortruss like biplanes and by spanners directly under them, the biplane trussand spanner at each end of hull being in the same plane when the hulls are parallel. Should the hulls pitch and be not parallel, then the biplane truss and the spanner under it have a relative rotative motion, causing the parallelogramto slightly warp.

Likewise, should the action of the waves; tilt one of the bows up for instance, and leave the sterns of the two hulls at the same level, the forward spanner swings upwardly and draws the two bows closer together,;hor izontally, causes the forward biplane to tilt and leaves the aft biplane level.

The rolling of the hulls is stabilized by connecting each hull fore and aft indirectly to the plane trusses.

To meet these conditionsand problems, the objects of my invention are as follows d To provide anaeroship for ocean travel to transport safely a thousand passengers at speeds from eighty to onehundred miles per 110111.

To provide entirely enclosed hulls with sealed water-tight chambers to render the hulls practically non-sinkable.

To provide a distribution of such ,chanibers to safeguard the hull from turning turtle in case the hull becomes detached from the rest of the aeroship.

To provide the hull with three water-tight decks and means of water closure at the stain ways or other openings. 7

To provide each hull withsuificient buoyancy to float the whole ship in case of ac cident.

To provide the hulls with side plates and partitions so reinforced as to constitute a truss capable of carrying the hull load when the hull is supported by waveaction principally at the center orends, or whenthe hull is lifted nearly out of the water by the aerofoils and is supported principally .near the hull ends.

To provide lifting planes forward andaft, the planes carriedbytrusses capable of carrying mostof the propulsion units. v

To provide ring mounting of the plane trusses, the ring housings being pivotally mounted on turntables on the fore and aft decks, constituting a universal jointbetween the plane truss and the hull.

To provide spanners under the plane trusses tospacethehulls apart.

To provide connection of the spanner to hull on center line of pivotal connection of plane housing to turntable so that the plane truss and spanner are parallel when the hulls are parallel and constitute a near parallel motion when the hulls are not parallel.

To provide a turntable for support of the outer ring housings, with one set of rollers to support the planes at rest or at slow speeds and another set of rollers to carry the reversed load when the planes lift more than their own weight and what they carry above the rollers.

To provide a center ring mounting at the center of the plane truss, midway between hulls, to stabilize the plane, the ring housing prevented from turning by pin connection to the spanner below it, so that when the hulls pitch relatively to one another, the plane only pitches half the angle between hulls.

To provide'wheel or roller hearings in the ring mountings of the aerofoils or planes, permitting rotation of the planes.

To provide the center ring mounting of the plane with an electric motor drive for control of plane inclination.

To provide the motor drive for plane inclination with worm gearing to automatically lock the plane in place when the motor is out To provide a diagonal connector to keep the hulls practically abreast at all times. i

To provide a diagonal tension cable between hulls with forward and aft connections opposite to those of the diagonal connector, the cable kept taut to relieve the connector from compressive strain.

To provide universal joints at connections of spanners, connector and diagonal cable to the hulls.

To provide a pneumatic take up for the diagonal cable to compensate variation in distance between connections of cable to hulls, when the hulls pitch.

To provide the cable take up with an electrical Windlass for adjustment of length of the diagonal cable between universal joint and Windlass.

To provide air cylinders between the hull turntables and the plane ring housings to stabilize the rolling of hulls.

To provide for automatic pressure regula tion for the hull stabilizing cylinders.

To provide air propulsion units at the bow and stern of hulls with turntable mountings for steering.

' To provide a Searchlight, mounted on the forward plane and counterbalanced to maintain a level beam.

To provide an air compressor for the air cylinders.

To provide electrical power for the motors, air compressor unit, lighting, heating, cooking and other purposes;

To provide a pilot house with switch board and other apparatus for the control of pro 'ste'ering'unit omitted.

Fig. 7 shows pin connection of center ring housing to spanner.

Fig. 8 is a sectional plan on line 88 of Fig. 7.

Fig.9 'isa plan of forward connections of fiiagona'l connector and spanner to the port ull.

' Fig. 10 is a sectional elevation on the line 10'10 of Fig. 9. a

Fig. 11 is an end view and part section of the same. Q

Fig. 12 is a plan of forward connections of diagonal cable and spanner to starboard hull. Fig.'13 is a part sectional plan of turntable.

Fig. 14 is a part sectional elevation of turntable.

Fig. 15 is a part side view of central plane ringhousing showing motor drive for plane inclination.

Fig. 16 is a sectional elevation showing roller mounting of an outer plane ring in its ring housing.

Fig. 17 is a sectional elevation showing the roller mounting of the center plane ring housing on its ring.

Fig. 18 shows the spring mounting of rollers on the outer housings.

Fig. 19 is an end view of the same.

Fig. 20 is a plan of aft connections of diagonal cable and spanner to port hull, showing take up.

Fig. 21 is an elevation of the same.

Fig. 22 is a plan and part section of center part of diagonal connector and diagonal cable. I l

' Fig.23 is an elevation of the same.

Fig. 24 is an elevation of an outer ring housing and bull cylinder and mounting on turntable. 1

- Fig. 25 is a side View of the same.

Fig. 26 is a plan of the turntable.

Fig. 27 is a plan of an outer ring housing.

Numerals :In Figs. 1, 2, 3, 4, 5, 6, 20, 24 and 25, 1 is the port hull and 2 the starboard hull, spaced apart by the forward spanner 3 and'aft spanner 4 and'kept abreast by the diagonal connector 5 and the diagonal cable 6.

Turntables

7 and 8 are mounted on the forward and aft decks of hull 1. Turntables 9 and 10 are mounted on the forward and aft decks of hull 2.

The forward and

aft spanners

3 and 4 are connected to the

hulls

1 and 2 by

universal joints

11 and 15, 11 and 15' shown in Figs. 9, 10, 11, 12, 20 and 26, mounted on the

turntables

7, 8, 9 and 10. The diagonal connector and the

cross spanners

3 and 4 are connected to the same universal joints 11 and 15 and have the same pivotal centers.

On the forward turntable 7 of hull 1, the universal joint 11 carries the connection 12 of the port end of spanner 3 and connection 14 of the forward end of connector 5. On the forward turntable 9 of hull 2, the universal joint 15 carries the connection 16 of the starboard end of spanner 3 and connection 17 of the forward end of the diagonal cable 6. On the aft turntable of hull 2, the universal joint and connections are similar to those of the forward end on hull 1.

In the double universal joint 11, shown in Figs. 4, 9, 10, 11 and 12, the spherical ball 20 is mounted on the stationary shaft 21 carried by the base 22 with collar seat 23 and fastening bolt 24. The split shell 25, of uniform thickness, fits over the ball 20 and is fastened to the spanner 3 by the plates 12.

The connector 5 is connected to the universal joint 11 by the split strap 14, cap 26 and bolts 27. The strap 14 and cap 26 fit over the shell 25. The weight of connector 5 is carried by the strap 28 secured to the strap 14 by bolt 29 and to the cap 26 by bolt 30. The spanner 3 and the connector 5, therefore, swing about the same center.

The base 22 is mounted on top of each of the four turntables, centering the spherical joints 11 and11, 15 and 15 on vertical center line of turntable. Therefore, the turntable is free to revolve without affecting the angular motions of the

spanners

3 and 4 and the connector 5.

On the aft turntable 8 of hull 1, the universal joint 11' carries the connection 12 of the port end of the aft spanner 4. The aft end 17 of the diagonal cable 6, in plan, is in line with the center of the universal joint 11 as shown in Fig. 20.

When the hulls pitch unevenly, the triangle formed by the hull 1, the aft spanner 4 and connector 5, and the triangle formed by hull 2, the forward s anner 3 and connector 5, both angles fold or hinge about the center line of connector 5, which is the line between centers of the universal joint 11 and 15'.

Therefore, should the bow of hull 1 rise, as shown in Fig. 3, and the above triangles start to fold up, then the longitudinal center of diagonal cable 6 rises with regard to center of connector 5.

In Figs. 22 and 23, the cable 6 is shown passing through the connector 5 with a bottom roller 18 to carry its weight when down and with side guide rollers 19, giving the central.

portion of cable 6 a free vertical travel equal to the maximum relative pitch of hulls measured at the turntable centers.

In Fig. 3, the aeroship is shown at slow speed or at anchor, taking a huge wave thirty feet high from trough to crest, without disadvantage to the hull connections.

30 is the forward lifting plane and 31 the aft lifting plane, both of which carry air propulsion units 32. 33 are the steering units, decribed in the patent to me, Propeller turret for propulsion and steering of aeroships, Dec. 29, 1931, No. 1,838,258.

34 are the outer plane ring housings and 35 the center ring housings, which carry the pilot houses 36. 37 are the pennant masts, located on the outer ring housings 34, in plain View of the pilot for direction of wind.

The upper deck 38, floor of the observation cabins 39, being about thirty feet above the water line, the glazed sides 40 of the cabins 39, are not subject to heavy wash.

The lifting planes 30 and 31 are roller mounted in the outer ring housings 34, which are pivotedly connected at 41 to brackets 42 centrally mounted on the top of

turntables

7, 8, 9 and 10 on the decks of and in the medial planes of

hulls

1 and 2. The center line of the pivotal connection 41 of the outer ring housings 34 to the brackets 42, aasses through the center of the universal bearings '11 and 11, 15 and 15' for the

spanners

3 and 4 and the connector 5.

When the

hulls

1 and 2 pitch unevenly. the ring mounting centers of the outer housings 34 move forward and backward, causing the lifting planes 30 and 31 to get out of square with the hulls. The outer housings 34 are always square with the lifting planes 30 and 31 and therefore turn same relatively to the hulls when the hulls pitch, causing a small movement of the

turntables

7, 8, 9 and 10.

In Figs. 13 and 14, the turntable is shown to have a kingpin 43 mounted in bracket 44 secured to the hull deck 45, kingpin 43 is held'in place by bolt 46. The turntable top 47 is centered by the bearing 48 of the center bracket 49 carried by the top framing 50.

The load due to the weight of lift ng plane 30 or 31, is carried by the inside rollers 51. running between the upper track 52 carried by the upper framing and the lower track 53, supported by the lower framing 54 on the hull deck 45. The inside rollers 51 are spaced by pins 56 between rings 57 and 58 V centered by radial spokes 59 secured to the hub 60, which turns on the hub 61 of the bracket 44.

The reversed load due to the lift of the plane, 30 or 31, is carried by the outside rollers 62 and 63, running on tracks 64 and 65, supported by the upper framing 50 by hangers 66 and 67, which carry beams' 68 and 69. The hull load is transmitted from hull frant ing through posts 71 to beams '72 and 73 and

upper tracks

74 and 75. 1

The inner set 62 of Outside rollers' are spaced by rings 76 and 77, centered by rollers 78. The outer set 63 of the outside rollers are spaced by'rings i7 9 and 80 and centered by rollers 81.

In case some of the rollers fail, the turntable then operates on the safety surfaces between the hook ring 82 mounted on the turret and the ring 83 and flanged ring 84 carried by the top framing 50. The turntable cover 85 extends down over the safety surfaces to protect them from the weather so they may be greased.

As shown in Figs. 2, 3, 4, 6, 15 and 24, the lifting aerofoil 30 is shown a biplane, with upper plane and lower plane 91, with struts 92, bracing 93 and 94, cross bracing 95 and 96, outer rings 97 and central rings 98, all built together to form a plane truss 99, capable of carrying the loads due to lift and the weight, of the propulsion units 32.

The propulsion units 32 are secured below the lower surfaces of both the upper plane 90 and the lower plane 91, and are spaced clear of the struts 92 and the bracing 93 and 94.

The lifting plane truss 99 is carried by the outer housings 34, having

pin connections

41 and 41 in

bearings

100 and 101 on bracket 42 carried on

turntables

7, 8, 9 and 10. The center housing 35, as shown in Figs. 3, 6, 7, 8 and 15, is carried by the plane truss 99 and is held from turning by pin connection102 to the spanner 3.

The plane truss 99 is roller mounted in the

housings

34 and 35 and held from revolving byrworm gear connection on center housing 35. By making theoplane truss 99 fast at the center only, the pitching of the plane is equalized to half the'angle of pitch between the hulls.

When the hulls pitch, therefore, and the outer housings 34 tilt relatively forward and backward, the plane truss 99 7 revolves through a small angle in the outer housings 34.

As shown in Figs. 24, 25 and 27, the

brackets

103 and 104 are a part of the outer housing 34. The

hull stabilizing cylinders

105 and 106 are pivotedly mounted at 107 and 108 on

brackets

109 and 110, which are mounted on top of each of the four turntables and are pivotedly connected at 111 and 112 to the

brackets

103 and 104 by connecting

rods

111 and 112.

The

forward'hull cylinders

105 and 106 and the aft hull cylinders 105a and 106a, are for the purpose of'reducing the roll of the hulls to a minimum.

To accomplish this purpose I have devised a system of step-up pressures in the cylinders, automatically controlled by a pendulum located in the transverse longitudinally central plane of hull and at a height approxi-' mating the average location of the rolling center, which depends on the shape ofthe bottom and the displacement, which is variable.

When the hull rolls two degrees'from vertical, a conductor element carried by the hull makes contact with a conductor element carried by the pendulum and energizes a magnet which operates a pneumatic valve atthe cylinder, admitting to the cylinder an air pressure of twenty-five pounds per square inch.

When the hull rolls five degrees from vertical, another contact, magnet and valve admits to the cylinder an air pressure of fifty pounds. l/Vhen the hull rolls ten degrees from vertical, a. third contact, magnet and valve admits to'the cvlinder an air pressure of one hundred pounds.

This device is called by me an automatic pneumatic electric three stage step-up pressure regulator.

By having three distinct constant pres sures, the action is always positive. I For instance, should hull 1 roll to starboard, the outer cylinders 105 and 105a on hull 1 are put in compression and the reaction against the outer housings 34 held by the forward and aft planes 30 and 31, tends to check the rolling and to return the hull 1"to normal. In a similar way, wheneither hull starts to roll outwardly, the inside pairs of cylinders 106 and 106a are under compres sion.

For a light sea, the hulls roll about'two degrees, for a moderate sea, about five degrees and for a heavy sea, about ten degrees on each side of vertical, when the aeroship is at slow speed or at anchor.

In Figs. 7 and 8, the pin connection 102 of the centerring housing 35 to the cross span-' nor 3 shows the pin 102 carried by bracket 115, held in place by pin head 116and bolt 117 The pin 102 is free to turn in and to slide up and down in its cylindrical bearing in the ball 118, which is free to turn in the spherical bearing 119120, which is rigidly mounted in the cross spanner 3. The center ring housing 35 is thus centered by and held against rotative movement by this universal connection 102118119 to the cross spanner 3. Relative to the spanner 3, the housing 35 is therefore free to move up and down, to rotate horizontally, or to swing bodily about the center of the universal hearing 118119. 7

As shown in Figs. 4, 6, 15, 16' and 17, the outer and central plane truss rings 97 and 98 are rail and wheel mounted in'the'

plane ring housings

34 and 35. V

In Fig. 17, the rails 130 are mounted on the center ring 98and run on the wheels 131 mounted within the center ring housing 35 by axles 132 and bearings 133. The center ring 98 is centralized with its housing 35 by rollers 134 mounted with brackets 135 on the center housing 35, the rollers 134 engaging a central annular projecting flange 136 on the central plane ring 98.

The flange 136 carries an annular worm gear 137 engaged by the worm 138 driven by the motor 139 and mounted on housing 35 with shafting 140, bearings 141 and 142 and coupling 143 as shown in Fig. 15.

The outer plane truss rings 97 are mounted within their housings 34 with rails 150 running on flangeless wheels 151 carried within the outer ring housings 34 by axles 152 and bearings 153. The outer ring 97 is provided with a central annular projecting flange 154, engaged by rollers 155, spring mounted on bracket 156 within the outer housing 34. The outer rings 97 are built integral with the plane truss 99 and their distance apart is fixed. When the hulls pitch and the plane truss 99 is no longer parallel to the spanner 3, the two are a. little closer together and the outer housings 34 also draw in a little. This 9 small end movement or sliding of the outer housings 34 relative to the plane truss 99 is taken up by spring mounting of the rollers 155 as shown in Figs. 18 and 19, in which the roller 155 is carried by the pin 157 on shell 158 with side bearings 159 in guides 160 on the bracket 156. The shell 158 encloses the spring 161, whichhas a bearin at the shell end 162 and on the cylindrical boss 163 carried by the bracket 156. The advantage of this arrangement is the assistance given to the rail wheel contacts in moving the turntable and thus holding the outer ring housings 34 square with the plane truss 99.

In Figs. and 21, the take-up for the aft end of the diagonal cable 6 consists of the pneumatic cylinder 170 mounted on top of the turntable 8, gland 171, plunger 172, car 174, with wheels 175 running on track 176, rope drum 17 7 mounted on the car 174 with bearings 178, worm gear 179 secured to drum 177 and driven by worm 180, shaft 181, gears 182 and 183 and motor 184, mounted on the car 174.

The drum cable 188 passes over

sheaves

189 and 190 and serves the sheaves 191 and.

192. The sheave 191 is carried by bracket 193 mounted on a turntable 194 on a stand 195 secured to the top of the hull turntable 8.

The turntable 194 is centered on the center line of diagonal cable 6, which passes through the universal joint 11, when

hulls

1 and 2 sea.

The electric take-up is for the purpose of erection, replacement and adjustment. The

The hull has a smooth bottom 201, with longv radius keel 202, and flat portions 203 tapering upwardly therefrom at degrees, vertical sides 204, long radius bilge 205 between t e bottom 201 and the sides 204, cabin sides 206, curved gunwale plate 207, sloping side tops 208 inclined 30 degrees from horizontal between the gunwale plate 207 and cabin sides 206, and cabin top 209. The bottom, sides and top of hull are tangent to a circle to obtain high ratio of volume of weight.

This construction of hull bottom 201, together with the long radius bilge 205, reduces the pounding effect ofthe waves to a minimum. The V-shaped bottom 203 also reduces the water resistances rapidly as the hull lifts and the hull water line falls.

The observation cabins 39 extend between the turntables and 8 on hull 1 and between 9 and 10 on hull 2.

38 is the upper deck for the observation cabin 39. 210 is the main deck in line with the fore and aft decks 45. 211 is the lower deck, 212 flooring of the hold, with manhole 213 over the oil reservoir. The above decks are all water tight. g

I A stairway 214 leads from the upper deck 38 to the main deck 210. Stairway 215 leads from the main deck 210 to the lower deck 211.

At

stairway openings

216 and 217 ,water tightfloor doors are provided similar to those shown in the patent to me, Cabin for air and water craft, July 21, 1931, No. 1,815,103. 218 is a hinged floor door with water tight closure in the lower deck 211 at top of the ladder 219.

Sealed port holes 220 are provided for the lower deck 211. The sides 206 of the observation cabin 39 are provided with water tight windows 40. In all living quarters of the hull, the air is changedby. artificial ventilation.

The oil reservoir'is in the

keel chambers

221 and 222, provided with bafiling plates to pre vent the oil from surging.

For life saving purposes, air

tight chambers

223, 224, and 225 are provided next to the hull bottom 20.3 and 205 and chambers 226 at the gunwales.

, The hull is further divided lengthwise by cross partitions into a number of compartments capable of water tight closure by means of rubber doors similar to those described in the cabin patent referred to above. The

hulls are heavily loaded at the turntables at slow speeds and almost entirely suspend- The hull.

ed from turntables at high speeds.

is therefore provided with longitudinal'partitions and bracing, which, with the hull shell, constitute a truss capable of carrying the hull-load.

The observation cabin 39 is provided with comfortable chairs 227, writing tables, smok-.

ing room and every convenience.

I State rooms 228 are located on the main deck 210. The lower deck2l1 is provided with main cabin, dining room and kitchen, office,

forward for crew. 3

The electric generator unit 229, air compressor and other machinery are located in quarters for ofiicers and aft quarters the hold onthe floor 212.

Passengers board the aeroship at the upper deck level on the perforated platform 231' and enter the observation cabin39 by the door 230. v V

The captain gives the signal, motors are started and all is made ready. The inspector reports the temperature and ventilation system right and all outside openings closed. Order is given to cast off and puts to sea on its own power.

.On reaching open water, the aeroship is steeredinto its course. 1 7 y The steering is effected by the pilot wheel. The pilot observes the switchboard and sees that the reversingswitch ,for the forward turrets is up'and the reversing switchufori the aft'turrets is down, or'in reverse. A movement of the pilot wheel to the right, then steers the aeroship to starboard and a movement to the left, steersthe aeroship to port,

as explained in patent to me, Propulsion and steering of aeroships," Jan. '12, 1932, No;

Speed is increased to eighty miles an hour, when the aeroship glides f lightly over the surface of the "water or skips upon'the crest of waves.

Shouldthere be a stro'ng'wind ofi' port, for

instance, then, as soon as the compass indicates'the aeroship is 'onits course, the 'pilot throws up the reversing switch for the aft steering turrets, so that all of the steering turrets will revolve'inthe same direction. *The pilot then turns the pilot wheel to the T left, turning all turrets so their propellors face part way toward the wind. An adjustment of this kind is made every few minutes until the steering units face s'ufiiciently into the wind to counteract theabeam or slde comi ppnent of thejwind force and holdthe aero-;

the aeroship ship on its course straight ahead without;

brought back to center to cutout the steering motors. I v

.If there is no wind, the turrets all stand in straight ahead position and all of their 4 power is utilized for the aeroship. -i I When it is desired to change the course, the aeroship is steered by the propeller turrets in a similar manner anda new adjustment made for direction. of the wind. Should the aeroship encounter bad weather or "run into a fog and it becomes necessary to run at slow speed or come to anchor to ride out a storm, the lifting planes are partially uncovered as explained in patent to me referred to above, Safety surfaces for aerofoils, and the aeroship rides the. heavy seat. On account of the weight of the all metal lifting planes and hulls, and with the lifting planes partially uncovered, no wind short of a cyclone can do the aeroshipany forward movement of serious damage.

. Thelength and spread of hulls prevents the aeroship from being turned over by action of the waves.

pheric movements and avoids violent storms by increasing the speed of aeroship to one hundred miles per hour and by changing his course to keep out of its way, evenif he findsv it necessary to turn back. In such a case, if a heavy sea is running and it is not advis able to turn about, the aeroship can be run backward at reduced speed by the propellor turrets. If more speed isrequiredthe lift ing planes are turned upside down and all of the air propellers become availablejfor backward movement, with. some assistance from the lifting planes.

y In cases of emergency,'as a. precautionary measure, the passengers in the'observation cabin are ordered below and the floor door Y closed after them.

On occasi0n,'the openings for the. ventilae tion. system can be closed and sealed from the inside. e

Thus, at no time are the lives of passen gers. endangered. I

On nearing harbor, signal is given'to slow down and the aeroship is gradually brought to 'rest.' I,

Casting anchor, entered.

Iclaim; v 1. In a two hulled aeroship orsimilar craft, a lifting aerofoil mounted forward on the two said hulls, a lifting aerofoil mounted aft passengers leave as they on the two said hulls, air propulsion units carried by the said aerofoils, each of the said direction at The pilot is forewarned of major atmosv hulls consisting of an outer shell capable of water closure, doors in the said shell opening outwardly and means of water closure of the said doors.

2. In a two hulled aeroship or similar craft, a lifting aerofoil mounted forward on the two said hulls, a lifting aerofoil mounted aft on the two said hulls, air propulsion units carried by the said aerofoils, the said hull consisting of an outer shell capable of water closure, upper, main and lower decks capable of water closure within the said outer shell, stairway between the said upper and main decks, stairway between the said main deck and the said lower deck, stairway openings in the said decks for the said stair-ways and means of closure of the said stairway openings, the said means consisting of a floor car door construction, substantially as specified.

3. In a two hulled aeroship or similar craft, a lifting aerofoil mounted forward on the two said hulls, a lifting aerofoil mounted aft on the two said hulls, air propulsion units carriedby the said aerofoils, each of the said hulls consisting of an outer shell capable of water closure, three water tight decks, water tight cross partitions, openings in the said decks and the said partitions for communication, and means of water closure of the said cross partition, the said means consisting of a disappearing rubber door, substantially as specified.

l. In a two hulled aeroship or similar craft, a lifting aerofoil mounted forward on the two said hulls, a lifting aerofoil mounted aft on thetwo said hulls, air propulsion units carried by the said aerofoils, the said hull having an outer shell capable of water closure, compartments for passengers and crew capable of water closure, sealed floating chambers adjacent to the gunwales, sealed floating chambers adjacent to the bilge, sealed floating chambers adjacent to the sloping bottom, and sealed oil chambers adjacent to the shell keel plate, substantially as specified.

5. In a two hulled aeroshi p or similar craft, an aerofoil mounted forward on the two said hulls, an aerofoil mounted aft on the two said hulls, air propulsion units carried by the said aerofoils, the said hnll consisting of an outer shell capable of water closure, upper, main and lower decks and cross partitions within the said shell constituting compartments for passengers and crew, longitudinal and trans verse partitions constituting a double bottom with oil tank in the said double bottom adjacent to the keel plate of the said hull, sealed floating chambers adjacent to the sloping bottom, sealed floating chambers at the bilge adjacent to the hull sides, sealed floating chambers at the gunwales, adjacent to the hull sides, and a chamber located symmetrically about the vertical media-l plane of hull in the hold onthe lowest floor level, for machinery.

6. In a two hulled aeroship or similar craft, a lifting aerofoil mounted forward on the two said hulls, a lifting aerofoil mounted aft on the two said hulls, air propulsion units carried by the said aerofoils, a forward spanner spacing the two said hulls apart latterly and. forwardly, an aft spanner spacing the two said hulls apart latterly and aft, the said forward and aft spanners having the same length, a diagonal connector connecting the forward part of one of the said hulls with the aft part of the other of the said hulls, a diagonal cable connecting the forward part of the hull opposite to the aforesaid forward connector hull connection, the said cable connecting the aft part of the other of the said hulls opposite to the aforesaid aft connector hull connection, double universal oints mounted on the forward parts of the two said lir is and t as aft part of one of the said hulls, the said universal oint having the same center for one of the said spanner connect-ions and one of the said diagonal connections.

7. In a two hulled aerosh'ip or similar craft, a lifting aerofoil mounted forward on the two said hulls, a lifting aerofoil mounted aft on the two said hulls, air propulsion units carried by the said aerofoils, double universal joints mounted forward and aft on the dec (s of the said hulls, the said mounting being in medial plane of hull and on vertical center line of the said mounting of the said aerofoil, spanncrs spacing the said hulls forward and aft connecting to the said universal joints, diagonal connector between the forward part of one hull and the aft part of the other hull connecting to the said universal joints, a diagonal cable connecting the forward part of the hull opposite to the aforesaid forward connector hull connection, and means for taking up slack in the said cable, the said means consisting of an air cylinder, plunger, car, rope drum with power drive, the drum rope serving a multiple sheave reduction rigr connecting the said drum with the aft one. of the said cable, substantially as specified.

8. In a two hulled aeroship or similar craft, an aerofoil mounted forward on the two said hulls, an aerofoil mounted aft on the two said hulls, air propulsion units carried by the said aerofoils, turntables mounted on the forward. deck and on the aft deck of each of the said hulls, an outer ring housing pivotally mounted on each of the said turntables. outer rings mounted on the said aerofoils in the medial planes of the said hulls, and roller mounting of the said aerofoil outer ring in the said outer housing.

9. In a two hulled aeroship or craft, an aerofoil mounted forward on the two said hulls, an aerofoil mounted aft on the two said hulls, air propulsion units carried by the said aerofoils, universal mounting of the said aerofoil on the said hull as per claim 8 similar spanners of equal length spacing the said hulls apart latterly, universal mounting of the said spanners on the said hulls, one of the said aerofoils and. its companion spanner constituting a near parallel motion when the equal length spacing the two said hulls forwardand aft, universal mounting of the said spanners on the said hulls, a diagonal con-- nector between the forward part of one hull and the aft part of the other hull, universal mounting of the said connector on the said hulls, a turntable mounted on forward and aft parts of each of the said hulls, an outer ring housing pivotedly mounted on each of the said turntables, outer rings carried by the said aerofoils, roller mounting of the said outer ring in the said outer ring housing, a

center ring carried by each of the said aerofoils, a center ring housing, a roller mounting of the said center ring housing on the said center ring, a pin carried by the said center ring housing, a universal joint carried by the said spanner adjacent to the said aerofoil,,the said pin engaging the said universal joint on the said spanner, a central annular flange on the said center ring, rollers mounted within the said center ring housing engaging the said center ring flange, a central annular flange on the said outer housing, and rollers spring mounted within the said outer ring housing engaging the said outer ring flange. 11. In a two hulled aerosh1p or similar craft,a lifting aerofoil mounted forward on the two said hulls, a lifting'aerofoil mounted aft on the two said hulls, air propulsion units carried by the said aerofoils, universal mounting of the said aerofoils on the said hulls, spanners of equal length spacing the said hulls forward and aft, universal mountings between the said spanners and the said -hulls,a diagonal connector between the forward vpart of one hull and the aft part of the other hull, universal mountings of the said connector on the said hulls, the universal connection of the said connector to hull havingthe same center as the said universal connection of the'said spanner to hull, a center ring carried by the said aerofoil, a center ring houslng, roller mounting of the sald center ring housing on the said center ring, universal pin connection between the said center ring housing and the ad acent spanner, an annular worm gear carried by the said center ring, a worm carriedby the said center ring housing and engaging the said worm gear,

and a motor drive for the said center ring, the said drive consisting of the said worm, shafting, coupling, motor gear reduction and motor mounted on the said center ringhousing. I

"12. In a two hulled aeroship or similar craft, a lifting aerofoil mounted forward on the two said hulls, a lifting aerofoil mounted aft on the two said hulls, spanners of equal length spacing the said hulls apart latterly forward and aft, the said aerofoil consisting of upper and lower aeroplanes built together as a biplane, an aerofoil structure for the said biplane consisting of upper and lower plane frames, struts, longitudinal diagonal bracing, and transverse diagonal bracing forming a truss, air propulsion units suspended from the upper plane frame below the lower lifting surface, between the said diagonal bracing, air propulsion units suspended from the lower plane frame below the lower lifting surface, between the said diagonal bracing, outer rings built integral with the said biwith the said biplane structure,'universal mounting of the said outer rings on the said hulls, and universal connection of the said center ring to the spanner adjacent thereto.

13. In a two hulled aeroship or similar craft, an aerofoil mounted forward on the two said hulls, anv aerofoil mounted aft .on the two said hulls,- the said aerofoil constituting a biplane truss, air propulsion units carried by thesaid. aerofoils, spanners of equal'length spacing the two hulls latterly, forward and aft, diagonal connector between the forward part of one hull and the aft part of the other hull, turntables mounted forward and aft on the said hulls, outer housings pivotedlymounted on the said turntables, supporting the said aerofoilsat equal heights above the said hulls, and roller mounting of the said aerofoil inthe said outer housing, the'said aerofoil, the said spanner under, it: and the outer housing adjac'ent thereto, forming a parallelogram when the two said hulls are parallel and constitute a. near parallel motion when the c pitch unevenly and are. not

hulls apart latterly forward and aft, diagonal connector between the forward part of one hull and the aft versal mountings of the said spanners and the said connector on the said hulls, t'urn tables mounted on the said hulls'forward and aft, outer housings pivotedly mounted on thesaid turntables, roller mountingof the said aerofoils in the saidouter housings,

part of the other hull, unibrackets on the said outer housing, air cylinders mounted on the hull deck near the hull sides and in a transverse plane through the center of the said outer housing, a plunger engaging the said cylinder and pin connected to the said bracket, means for supplying fluid pressure to the said cylinder and means for stabilizing the said hulls against rolling by varying the intensity of the said fluid pressure.

15. In a two hulled aeroship or similar craft, a lifting aerofoil mounted forward on the two said hulls, a lifting aerofoil mounted aft on the two said hulls, air propulsion units carried by the said aerofoils, a pilot house mounted on the said forward aerofoil, steering units mounted at the bow and at the stern of each of the said hulls, the said steering unit consisting of an air propeller and combustion engine drive, turret mounting of each of the said steering units, electric motors, shafting and gearing for turning the said turrets in either clockwise or counterclockwise direction and centralized control of the said electric motors from the said pilot house, substantially as specified.

16. In a two hulled aeroship or similar craft, a lifting aerofoil mounted forward on the two said hulls, a lifting aerofoil mounted aft on the two said hulls, air propulsion units carried by the said aerofoils, steering units mounted on the bow and stern of each of the said hulls, the said steermg unit consisting of an air resisting propulsion unit swiveled upon a vertical axis and mounted on a turntable having an electric motor drive, steering means for rotating the two forward turrets in the same direction, steering means for rotating the two aft turrets in the same direction, and in opposite direction to the said rotation of the forward turrets, and means for changing direction of rotation of the said turrets, independently or in groups.

17. In a two hulled aeroship or similar craft, a lifting aerofoil mounted forward on the two said hulls, a lifting aerofoil mounted aft on the two said hulls, air propulsion units carried by the said aerofoils, steering units mounted on the bow and stern of each of the said hulls, the said steering unit consisting of an air resisting propulsion unit swiveled upon a. vertical axis and mounted on a turntable having an electric motor drive, steering means for rotating the four said turrets independently, steering means for rotating the said turrets in groups, one of said groups comprising the forward turrets, another of said groups comprising the two aft turrets, another of said groups comprising all four of the said turrets, and means for changing direction of rotation of the said turrets, independently or in groups.

18. In a two hulled aeroship or similar craft, a lifting aerofoil mounted forward on the two said hulls, a lifting aerofoil mounted aft on the two said hulls, air propulsion units carried by the said aerofoils, the said aerofoil consisting of upper and lower aeroplanes built together to form a biplane truss, a pilot house carried by the said biplane truss, the said pilot house being centrally located with regard to the said hulls, and mounted high enough above or low enough below the said biplane truss to be practically free from slip stream interference.

19. In a two hulled aeroship or similar craft, a lifting aerofoil mounted forward on the two said hulls, a lifting aerofoil mounted aft on the two said hulls, air propulsion units carried by the said aerofoils, the said aerofoil consisting of upper and lower aeroplanes built together to form a biplane, openings in the lifting surfaces of the said aeroplanes, slide valve closure for the said openings, electric motor drive for the said slide valve 010- sure, the said valves arranged in groups on the said aeroplanes, a pilot house on the said biplane, and means for control of all of the said electric motors from the said pilot house.

20. In a two hulled aeroship or similar craft, a lifting aerofoil mounted forward on the two said hulls, a lifting aerofoil mounted aft on the two said hulls, air propulsion units carried by the said aerofoils, spanners spacing the said hulls apart latterly, diagonal cable between the forward part of one hull and the aft part of the other hull, a pneumatic electric takeup for the said diagonal cable, an electric motor drive for the said takeup, steering turrets mounted on the bow and stern of each of the said hulls, electric motor drives for the said turrets, openings in the lifting surfaces of the said aerofoils, arranged in groups, slide valve closure for the said openings, electric motor drive for the said slide valve closure, a pilot house centrally mounted on top of the said forward aerofoil, a pilot house centrally mounted underneath the said aft aerofoil, means of control of the said electric motors for the slide valve closures of the forward aerofoil from the said forward pilot house, means of control of the said electric motors for the slide valve closures of the aft aerofoil from the said aft pilot house, means of control of the electric motor for cable take-up from the aft pilot house, and means of control of the said electric motors for the steering turrets both from the said forward pilot house and from the said aft pilot house.

Signed at Elyria, in the county of Lorain and State of Ohio, this 12th day of March,

SAMUEL E. HITT.