US1043376A - Equilibrator. - Google Patents

Equilibrator. Download PDF

Info

Publication number
US1043376A
US1043376A US65540111A US1911655401A US1043376A US 1043376 A US1043376 A US 1043376A US 65540111 A US65540111 A US 65540111A US 1911655401 A US1911655401 A US 1911655401A US 1043376 A US1043376 A US 1043376A
Authority
US
United States
Prior art keywords
buckets
bucket
equilibrator
nose
water
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
US65540111A
Inventor
Melvin Vaniman
Ida L Vaniman
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.)
INTERNATIONAL AERONAUTICAL CONSTRUCTION Co
INTERNAT AERONAUTICAL CONSTRUCTION Co
Original Assignee
INTERNAT AERONAUTICAL CONSTRUCTION Co
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 INTERNAT AERONAUTICAL CONSTRUCTION Co filed Critical INTERNAT AERONAUTICAL CONSTRUCTION Co
Priority to US65540111A priority Critical patent/US1043376A/en
Application granted granted Critical
Publication of US1043376A publication Critical patent/US1043376A/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
    • B64B1/40Balloons

Definitions

  • My invention relates to a combined equilibrator and ballast, more applicable to aeronautic devices, and an object of my invention is to provide a means for quickly raising water-ballast to the aeronautic ship while sailing over water, and which may, if desired, be used as a drag.
  • a further object of my invention is to provide a device of the above-indicated character, which, in passing through the water, will offer a minimum resistance to the move ments of the aeronautic ship.
  • Figure 1 is a side elevation of the rear portion of an airship, showing a preferred embodiment of my invention depending therefrom;
  • Fig. 2 is an enlarged side elevation of my equilibrator;
  • Fig. 3 is an enlarged longitudinal transverse section, showing the upper bucket and the top of the next adjacent bucket;
  • Fig. 4 is a view similar to Fig. 3, showing the lowermost bucket and the lower part of the next adjacent bucket;
  • Fig. 5 is a transverse sectional view, taken on the line 5-5 of Fig. 3, looking in the direction of the arrow;
  • Fig. 6 is an end View of the lowermost bucket, looking upward on Fig. 4;
  • Fig. 7 is an end view, looking downward on Fig. 3.
  • lindrical buckets 8 in this case shown to be six in number.
  • the upper bucket 9 has a conical or tapered nose 10 at its upper or forward end, and the end opposite the nose is formed into a concaved substantially semi-spherical depression 11.
  • the central portion of the depression 11 has an external pocket 12, open ing into the depression 11.
  • a cylin drical metallic tube 14 formed integral with the metal of thenose and the metal forming the end 11.
  • the conical nose, adjacent the point 13 has within the bucket a reinforcing metallic plate 15, conforming in configuration to and in contact with the inner wall of the nose 10.
  • Apertures 16 extend through the nose 10 and through the reinforcing plate 15, by means of which apertures water is admitted to the interior of the bucket.
  • Disposed in alinement in rear of the upper or forward bucket 9 are a series of similarly-shaped buckets 17 but one of which will be described in detail, it being understood that the same description will apply to the several intermediate buckets.
  • These buckets are similar in construction to the bucket 9, described in detail, with the exception that, instead of the conical nose 10, the upper ends of the intermediate buckets have their ends formed into a semi-spherical head 18, conforming substantially to the configuration of the depression 11, so that, in effect, a ball-and-socket joint is afforded between theupper end 18 of one bucket and the depression 11 of the next adjacent bucket.
  • a series of apertures 19 extend through thehead 18 at a point where the head meets the conical sides of the bucket and through the reinforcing plate 15. The lower ends of each of the intermediate buckets 17 corre-.
  • a tube 20, similar to the tube 14 extends centrally through each of the buckets 17, with the exception that the upper end of each of these tubes is formed into a funnel end 21, the outer open end 22 of which is of a diameter slightly greater than the diameter of the pocket 12.
  • the lowermost bucket 23 is similar in construction to the buckets 17, with the exception that the lower or rear end has a conical nose 24, similar in construction to the nose 10.
  • the nose 24 terminates in a blunt end 25, centrally extending inward from which is the centrally-disposed tube 20 leading to the funnel end 21 at the opposite extremity of the bucket 28.
  • the lift D passes through the alined tubes 14 and 20 in the central buckets, and terminates in a stop 26 bearing upon the blunt end 25.
  • a clasp 27 of any suitable construction, rigidly aflixed to the lift D, and so positioned with reference to the clasp in the next adjacent pocket 12 that the several buckets are maintained in their relative position, but at the same time flexion is permitted between the several buckets, so that the buckets may take a position, while moving through the water, to offer a minimum resistance to the water.
  • this equilibrator may be lowered into the water to offer a drag, if desired, or the device may be used as a water-lift to raise water-ballast to suitable tanks within the air-ship.
  • a bucket of general cylindrical form having one end shaped to form a semi-spherical depression, the opposite end having a conical nose, a tube extending from said nose of said depressed end, a flexible lift passing through said tube, and means maintaining said bucket on said lift.
  • a bucket of general cylindrical shape having one end depressed in the form of a semi-sphere, a pocket in said depressed end, and a flexible lift passing through said bucket having a clamp rigidly aflixed thereto and positioned within said pocket.
  • a bucket of general cylindrical shape having a conical nose'at one end, and a reinforcing plate within said conical nose conforming in configuration to and in contact with the inner wall of said nose, said reinforcing plate and said nose having apertures extending therethrough affording an entrance to said bucket.
  • An equilibrator comprising a series of buckets in longitudinal alinement, the adja cent ends of said buckets shaped to afford a ball and socket connection between them, a centrally disposed tube in each of said buckets and in alinement, one end of each of said tubes enlarged to form a funnel end, and a flexible connection passing between said tubes, said funnel ends preventing said flexible connection from interfering with the relative movements between said buckets.

Landscapes

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

Description

M. VANIMAN, DEGD.
I L. VANIMAN, ADMINISTRATRIX.
BQUILIBRATOR.
APPLICATION FILED 001218, 1911.
1 ,043376, Patented Nov. 5, 1912.
COLUMBIA PLANOGRAPH COUWAISHINGTON. D. C
UNITED STATES PATENT onnron.
MELVIN VANIMAN, OF ATLANTIC CITY, NEW JERSEY; IDA L. VANIMAN, ADMINIS- TRATRIX OF SAID MELVIN VANIMAN, DECEASED, ASSIGNOR TO INTERNATIONAL AERONAUTICAL CONSTRUCTION COMPANY," A CORPORATION OF MAINE.
EQUILIBRATOR.
Specification of Letters Patent.
Application filed October 18, 1911.
Patented Nov. 5, 1912.
Serial No. 655,401.
To all whom it may concern:
Be it known that I, MELVIN VANIMAN, a citizen of the United States, and a resident of Atlantic City, in the county of Atlantic and State of New Jersey, have invented a new and Improved Equilibrator, of which the following is a full, clear, and exact description.
My invention relates to a combined equilibrator and ballast, more applicable to aeronautic devices, and an object of my invention is to provide a means for quickly raising water-ballast to the aeronautic ship while sailing over water, and which may, if desired, be used as a drag.
A further object of my invention is to provide a device of the above-indicated character, which, in passing through the water, will offer a minimum resistance to the move ments of the aeronautic ship.
I attain the above-outlined objects by disposing a series of hollow buckets on the end of a flexible lift, depending from the aeronautic ship.
Reference is to be had to the accompanying drawings forming a part of'this specification, in which similar characters of reference indicate corresponding parts in all the views, and in which Figure 1 is a side elevation of the rear portion of an airship, showing a preferred embodiment of my invention depending therefrom; Fig. 2 is an enlarged side elevation of my equilibrator; Fig. 3 is an enlarged longitudinal transverse section, showing the upper bucket and the top of the next adjacent bucket; Fig. 4 is a view similar to Fig. 3, showing the lowermost bucket and the lower part of the next adjacent bucket; Fig. 5 is a transverse sectional view, taken on the line 5-5 of Fig. 3, looking in the direction of the arrow; and Fig. 6 is an end View of the lowermost bucket, looking upward on Fig. 4; and Fig. 7 is an end view, looking downward on Fig. 3.
I have shown an air-ship A, shown in its passage over the water B, within which water is the equilibrator C more particularly forming the subject-matter of this invention, which equilibrator is attached to the air-ship by a flexible lift D, by means of which lift the equilibrator may be'raised or lowered relative to the ship, the equilibrator comprising a series of hollow, metallic, cy-
lindrical buckets 8, in this case shown to be six in number.
The upper bucket 9 has a conical or tapered nose 10 at its upper or forward end, and the end opposite the nose is formed into a concaved substantially semi-spherical depression 11. The central portion of the depression 11 has an external pocket 12, open ing into the depression 11.
Extending from the center of the pocket 12 to the point 13 of the nose 10 is a cylin drical metallic tube 14, formed integral with the metal of thenose and the metal forming the end 11. The conical nose, adjacent the point 13 has within the bucket a reinforcing metallic plate 15, conforming in configuration to and in contact with the inner wall of the nose 10.
Apertures 16 extend through the nose 10 and through the reinforcing plate 15, by means of which apertures water is admitted to the interior of the bucket. Disposed in alinement in rear of the upper or forward bucket 9 are a series of similarly-shaped buckets 17 but one of which will be described in detail, it being understood that the same description will apply to the several intermediate buckets. These buckets are similar in construction to the bucket 9, described in detail, with the exception that, instead of the conical nose 10, the upper ends of the intermediate buckets have their ends formed into a semi-spherical head 18, conforming substantially to the configuration of the depression 11, so that, in effect, a ball-and-socket joint is afforded between theupper end 18 of one bucket and the depression 11 of the next adjacent bucket.
A series of apertures 19 extend through thehead 18 at a point where the head meets the conical sides of the bucket and through the reinforcing plate 15. The lower ends of each of the intermediate buckets 17 corre-.
spond in construction to the construction described in detail for the lower end of the upper or forward bucket 9.
A tube 20, similar to the tube 14 extends centrally through each of the buckets 17, with the exception that the upper end of each of these tubes is formed into a funnel end 21, the outer open end 22 of which is of a diameter slightly greater than the diameter of the pocket 12. The lowermost bucket 23 is similar in construction to the buckets 17, with the exception that the lower or rear end has a conical nose 24, similar in construction to the nose 10. The nose 24 terminates in a blunt end 25, centrally extending inward from which is the centrally-disposed tube 20 leading to the funnel end 21 at the opposite extremity of the bucket 28. v
The lift D passes through the alined tubes 14 and 20 in the central buckets, and terminates in a stop 26 bearing upon the blunt end 25. Preferably, there is positioned within each of the pockets 12 a clasp 27 of any suitable construction, rigidly aflixed to the lift D, and so positioned with reference to the clasp in the next adjacent pocket 12 that the several buckets are maintained in their relative position, but at the same time flexion is permitted between the several buckets, so that the buckets may take a position, while moving through the water, to offer a minimum resistance to the water.
It is to be understood that this equilibrator may be lowered into the water to offer a drag, if desired, or the device may be used as a water-lift to raise water-ballast to suitable tanks within the air-ship.
Many changes could be made in the above construction, and many apparently widely diflerent embodiments of this invention could be made without departing from the scope thereof.
It is intended that all matters contained herein in the above description or shown in the accompanying drawings, shall be interpreted as illustrative and not in a limiting sense. It is also to be understood that the language used in the following claims is merely intended to cover all the generic and specific features of the invention herein described and all statements of the scope of the invention, which, as a matter of language, might be said to fall therebetween, and that materials, sizes and relativities of parts are nonessential, except as called for in the claims.
Having thus described my invention, what I claim as new and desire to secure by Letters Patent is 1. In an equilibrator for air ships, a series of meshing buckets arranged in longitudinal alinement, and flexible means maintaining said buckets in engagement.
2. In an equilibrator, a series of cylindrical buckets disposed in longitudinal alinement, a ball and socket connection between adjacent buckets, and flexible means maintaining said buckets in alinement.
3. In an equilibrator, a bucket of general cylindrical form having one end shaped to form a semi-spherical depression, the opposite end having a conical nose, a tube extending from said nose of said depressed end, a flexible lift passing through said tube, and means maintaining said bucket on said lift.
4. In an equilibrator, a bucket of general cylindrical shape having one end depressed in the form of a semi-sphere, a pocket in said depressed end, and a flexible lift passing through said bucket having a clamp rigidly aflixed thereto and positioned within said pocket.
5. In an equilibrator, a bucket of general cylindrical shape having a conical nose'at one end, and a reinforcing plate within said conical nose conforming in configuration to and in contact with the inner wall of said nose, said reinforcing plate and said nose having apertures extending therethrough affording an entrance to said bucket.
6. An equilibrator comprising a series of buckets in longitudinal alinement, the adja cent ends of said buckets shaped to afford a ball and socket connection between them, a centrally disposed tube in each of said buckets and in alinement, one end of each of said tubes enlarged to form a funnel end, and a flexible connection passing between said tubes, said funnel ends preventing said flexible connection from interfering with the relative movements between said buckets.
In testimony whereof I have signed my name to this specification in the presence of two subscribing witnesses.
MELVIN VANIMAN.
Witnesses:
EVERARD B. MARSHALL, ARTHUR WRIGHT.
Gopies of this patent may be obtained for five cents each, by addressing the Commissioner of Patents,
Washington, D. G.
US65540111A 1911-10-18 1911-10-18 Equilibrator. Expired - Lifetime US1043376A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US65540111A US1043376A (en) 1911-10-18 1911-10-18 Equilibrator.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US65540111A US1043376A (en) 1911-10-18 1911-10-18 Equilibrator.

Publications (1)

Publication Number Publication Date
US1043376A true US1043376A (en) 1912-11-05

Family

ID=3111650

Family Applications (1)

Application Number Title Priority Date Filing Date
US65540111A Expired - Lifetime US1043376A (en) 1911-10-18 1911-10-18 Equilibrator.

Country Status (1)

Country Link
US (1) US1043376A (en)

Similar Documents

Publication Publication Date Title
US1222996A (en) Toy.
US666022A (en) Puzzle.
US826908A (en) Anchor for air-ships.
US1883598A (en) Holder for hogs and other animals
US1191621A (en) Hose-nozzle.
US1051004A (en) Toy balloon.
US870047A (en) Toy air-ship.
US753029A (en) astarita
US261398A (en) Chimney-top
US462487A (en) Leox humbert
US828586A (en) Curtain-rod.
US612996A (en) Helm hans von siegsfeld
US754029A (en) Umbrella.
US57996A (en) Improvement in marine balloons
US1529568A (en) Pinwheel toy
DE102024116597B4 (en) PiƱata
US54878A (en) Improvement in churns
US192557A (en) Improvement in ventilators
US36109A (en) Improved rudder
US1061961A (en) Airship-propeller.
US255873A (en) Joseph
DE307038C (en)
US769778A (en) Socket member.
US771705A (en) Whirling toy.
US74995A (en) Rt c r a w f