US924495A - Air-ship. - Google Patents

Air-ship. Download PDF

Info

Publication number
US924495A
US924495A US45801308A US1908458013A US924495A US 924495 A US924495 A US 924495A US 45801308 A US45801308 A US 45801308A US 1908458013 A US1908458013 A US 1908458013A US 924495 A US924495 A US 924495A
Authority
US
United States
Prior art keywords
carriage
air
ship
basket
stem
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US45801308A
Inventor
James M Park
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US45801308A priority Critical patent/US924495A/en
Application granted granted Critical
Publication of US924495A publication Critical patent/US924495A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft

Definitions

  • This invention relates to air ships, andthe primary object of; mg invention is the provision of positive an reliable means in con noction with an ai ship for freely supporting a gas or air bag relative to the steering and pro oiling mechanism, whereby the gas or air bag will be free to revolve in a horizontal plane irrespective of the direction or strata of an air current.
  • J I I A further object of my invention is coprovide an air ship that will be equally balanced, rigid and safe for traveling or observation purposes.
  • A. further object of this invention is to" utilize a revoluble, rigid or flexible body for to an air ship irrespective of carriage planes and propellers.
  • Figure 1 is an elevation of the air ship constructed in accordance withmy inventiompartly broken away'and partly in section
  • FigQZ is a plan of the carriage or basket thereof
  • Fig. 3 is a vertical cross sectional view of a portion of the air shi
  • Fig. 4 is a sectional view of a modifie. form of construction.
  • the present invention relates to that type ofaeronautical crafts
  • the stem 1 intermediate the ends thereof is provided with a fixed platform 7 having an annular ball race 8 for-anti friction balls ,9.
  • this structure comprises two. disk-shaped members 10 having peripheral flanges 11.
  • the members 10 are provided with central openings 12 connected y a vertical sleeve 13, which surrounds the stem 1.
  • the interior of the members 10 and the exterior of the sleeve 13 are lined or coated, as at 14, to provide a non-leakable structure-
  • the members win some in stances can .be made of a rigid, light and dubag.
  • the peripheral flanges 11 are provided with a fixed fan-tail rudder 15, this rudder keepin the direction of an air current by reason 0 the structure being mounted upon ball bearings between the latform 7 and the head 4.
  • T e head 2 is rovided with an annular race for anti-friction balls 165, and revolubly mounted upon these balls is a carriage or basket 17,, ore'l'erably oblong in plan.
  • the carriage or basket 17 is provlded with a central vertical sleeve 18 surrounding the lower part of the stem 1, and the upper end of this sleeve is cupped to accommodate anti-friction balls 19.
  • These balls are adapted to bear against the stem 1 and are retained in place by a cap 20 threaded u on said stem. '0 will of course be understoo that this cap is placed upon the stem 1 prior to securing the platform 7 and the head 4 in position.
  • the shai ts 22- protrude from the end of the carriaga or basket 17 and areprovided with pro pcllers 26. 4
  • the drive shaft 23 is driven by a motor 27 or similar source of power located in the carriage or basket 17. 1,
  • the carriage or basket 17 is provided with a bearing 28 and journaled in this bearing and the bearing 21 is a shaft 28* having a gear wheel 28* adapted to mesh with the lowermost-gear wheel 24.
  • a gear wheel 28 meshing with a'gear wheel 28, mounted upon ashalt 28 lower end of the shaft 31 is provided with a propeller wheel 32 for lifting and elevating on air ship irrespective of the overheed structure.
  • the lowermost propeller shaft 22 is prolonged and provided with a beveled gear Wheel 29 meshing with a beveled year wheel 29 mounted upon the upper end 01 8, vertical shaft 29 journaled in the corriagepr basket 17.
  • the lower end oi the shaft 29" is pro vided with a propeller 29 adapted to eooperete with the propeller Wheel. 32.
  • a vertical stein In an air ship, a vertical stein, an ver-- head structure" revolubly-niountod on the upper portion of the stern, and comprising two disk-shaped members having adjoining peripheral flanges, a. rudder seonred thereto, a carriage revolubly-mounted on the lower portion of the stem, propellers carried by said carriage, means in the carriage for driving said propellers, and u nninually-operablerudder earned by the carriage.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Earth Drilling (AREA)

Description

J. M. PARK. AIR SHIP.
, APPLICATION IILED OUT. 16, 1908.
9%,495. Pa-tented'June8,1909.-
"D/Vi tn moan or I adding stability or upper has 4.
arcs
cr bs.
JAMES M. PARK, OF PITTSBURG, PENNSYLVANIA.
No. scenes.
Specification of Letters Patent.
Patented. June 8,1909.
Application filed October 16, 1308. Serial No. 453,013.
1 i112, drawing. 1
This invention relates to air ships, andthe primary object of; mg invention is the provision of positive an reliable means in con noction with an ai ship for freely supporting a gas or air bag relative to the steering and pro oiling mechanism, whereby the gas or air bag will be free to revolve in a horizontal plane irrespective of the direction or strata of an air current. J I I A further object of my invention is coprovide an air ship that will be equally balanced, rigid and safe for traveling or observation purposes. l
A. further object of this invention is to" utilize a revoluble, rigid or flexible body for to an air ship irrespective of carriage planes and propellers.
With t above and other. objects in view which will more readily appear'as the invention is better understood, the same consists in the novel construction, combination and arrangement of parts to be presently described and then specifically claimed.
In the drawings Figure 1 is an elevation of the air ship constructed in accordance withmy inventiompartly broken away'and partly in section, FigQZ is a plan of the carriage or basket thereof, Fig. 3 isa vertical cross sectional view of a portion of the air shi and Fig. 4 is a sectional view of a modifie. form of construction.
As heretofore stated, the present invention relates to that type ofaeronautical crafts,
known as air shi s either lighter or heavier than air, which i epends upon theconstruc: tion and use of thesame Y in carrying my invention into effect, I use a vertical stem 1 having the lower end thereof provided with a head 2, while the opposite end 3 is threaded'for a detachable The head 3 is provided with an annular race '5 for antifriction balls 6.
The stem 1 intermediate the ends thereof is provided witha fixed platform 7 having an annular ball race 8 for-anti friction balls ,9.
= Between the balls 6 and 9 is supported a rigid or flexible structure that is preferably oircu lar in plan and elliptical in elevation. As
shown in the drawings, this structure comprises two. disk-shaped members 10 having peripheral flanges 11. The members 10 are provided with central openings 12 connected y a vertical sleeve 13, which surrounds the stem 1. The interior of the members 10 and the exterior of the sleeve 13 are lined or coated, as at 14, to provide a non-leakable structure- The members win some in stances can .be made of a rigid, light and dubag. In either instance, the peripheral flanges 11 are provided with a fixed fan-tail rudder 15, this rudder keepin the direction of an air current by reason 0 the structure being mounted upon ball bearings between the latform 7 and the head 4. T e head 2 is rovided with an annular race for anti-friction balls 165, and revolubly mounted upon these balls is a carriage or basket 17,, ore'l'erably oblong in plan. The carriage or basket 17 is provlded with a central vertical sleeve 18 surrounding the lower part of the stem 1, and the upper end of this sleeve is cupped to accommodate anti-friction balls 19. These balls are adapted to bear against the stem 1 and are retained in place by a cap 20 threaded u on said stem. '0 will of course be understoo that this cap is placed upon the stem 1 prior to securing the platform 7 and the head 4 in position.
In the carriage or basket -17 is arranged a bearing 21 for propeller shafts 22 and a drive shaft 23, said propeller shafts being provided with gear wheels 24 adapted to mesh with a gear wheel 25 carried by the shaft 23. The shai ts 22- protrude from the end of the carriaga or basket 17 and areprovided with pro pcllers 26. 4
. The drive shaft 23 is driven by a motor 27 or similar source of power located in the carriage or basket 17. 1,
The carriage or basket 17 is provided with a bearing 28 and journaled in this bearing and the bearing 21 is a shaft 28* having a gear wheel 28* adapted to mesh with the lowermost-gear wheel 24. Upon the shaft 23 is mounted. a gear wheel 28 meshing with a'gear wheel 28, mounted upon ashalt 28 lower end of the shaft 31 is provided with a propeller wheel 32 for lifting and elevating on air ship irrespective of the overheed structure.
The lowermost propeller shaft 22 is prolonged and provided with a beveled gear Wheel 29 meshing with a beveled year wheel 29 mounted upon the upper end 01 8, vertical shaft 29 journaled in the corriagepr basket 17. The lower end oi the shaft 29" is pro vided with a propeller 29 adapted to eooperete with the propeller Wheel. 32.
In hi 4 of the drawings, I have illustrated smod' cation of my invention wherein the upper end of the stem 1 is provided with a fixed head 83 adapted to be secured, as by rivets 34 m; the bottom of a rigid or flexible structure. in this instance, the carriage or basket 17 will be free to rotate in a horizontalplane relative to the overhead structure.
While in the drawings forming a part of this application there are illustrated the preferred embodiments of my invention, 1t 1s obvious that the same can be varied or changed as to shape, proportion and manner carried by the upper end of said stein, suit overhead structure comprising the shaped members hev'ing adjoining perh lurul flanges, a rudder secured to the ll; 9 said structure, a carriage rovolubly mourned upon the head on the loner end oi said stein,
\ invent; w
structure comprising two rigid disks having eripherzil adjoining edges, u rudder carried liy said structure, 0. earrings revolubly ID on n ted upon the lower end oi stein, propellers revolubly supported b y said earrings, :1, rudder carried by said carriage, and means lovcated in suid carriage for imparting a rotary movement to said pro xellers.
3. In an air ship, a vertical stein, an ver-- head structure" revolubly-niountod on the upper portion of the stern, and comprising two disk-shaped members having adjoining peripheral flanges, a. rudder seonred thereto, a carriage revolubly-mounted on the lower portion of the stem, propellers carried by said carriage, means in the carriage for driving said propellers, and u nninually-operablerudder earned by the carriage.
In testimony whereof l; :iliix my signature in the presence of two witnesses.
JAMES M, PAH hi.
Witnesses MAX H. Sno ovrrz,
K. H. BUTLI
US45801308A 1908-10-16 1908-10-16 Air-ship. Expired - Lifetime US924495A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US45801308A US924495A (en) 1908-10-16 1908-10-16 Air-ship.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US45801308A US924495A (en) 1908-10-16 1908-10-16 Air-ship.

Publications (1)

Publication Number Publication Date
US924495A true US924495A (en) 1909-06-08

Family

ID=2992925

Family Applications (1)

Application Number Title Priority Date Filing Date
US45801308A Expired - Lifetime US924495A (en) 1908-10-16 1908-10-16 Air-ship.

Country Status (1)

Country Link
US (1) US924495A (en)

Similar Documents

Publication Publication Date Title
US1905345A (en) Marine vessel
CN102105357A (en) A flying machine comprising twin contra-rotating vertical axis propellers
US815211A (en) Amusement-vehicle.
US3503573A (en) Disk flying craft
US924495A (en) Air-ship.
US731394A (en) Life-saving vessel.
US2072611A (en) Cycle power unit
US1374487A (en) Airship
US1868976A (en) Aircraft propelling mechanism
US2046613A (en) Bearing for rotary machine-elements
US1402291A (en) Crane
US2109539A (en) Amusement device
US2438661A (en) Propeller assembly
US1245902A (en) Aeroplane-motor.
US1655317A (en) Flying machine
US1034430A (en) Flying-machine.
US1020274A (en) Feathering propeller-wheel.
US1750382A (en) Propelling device
US653435A (en) Means for propelling vessels.
US1220903A (en) Alternative driving-gearing for freezers.
US572667A (en) Hyacinthe trenta
US1418248A (en) Combined aeroplane and helicopter
US678670A (en) Railroad ferris wheel.
US1373775A (en) Helicopter
US610177A (en) Richard gaertner