US923459A - Pneumatic-despatch-tube system. - Google Patents

Pneumatic-despatch-tube system. Download PDF

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Publication number
US923459A
US923459A US38472507A US1907384725A US923459A US 923459 A US923459 A US 923459A US 38472507 A US38472507 A US 38472507A US 1907384725 A US1907384725 A US 1907384725A US 923459 A US923459 A US 923459A
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United States
Prior art keywords
carrier
goose
neck
tube
pneumatic
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Expired - Lifetime
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US38472507A
Inventor
Charles F Stoddard
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AMERICAN PNEUMATIC SERVICE CO
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AMERICAN PNEUMATIC SERVICE CO
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Priority to US38472507A priority Critical patent/US923459A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65GTRANSPORT OR STORAGE DEVICES, e.g. CONVEYORS FOR LOADING OR TIPPING, SHOP CONVEYOR SYSTEMS OR PNEUMATIC TUBE CONVEYORS
    • B65G51/00Conveying articles through pipes or tubes by fluid flow or pressure; Conveying articles over a flat surface, e.g. the base of a trough, by jets located in the surface
    • B65G51/04Conveying the articles in carriers having a cross-section approximating that of the pipe or tube; Tube mail systems
    • B65G51/20Braking arrangements

Definitions

  • My invention relates to new and useful 5 improvements in terminals for pneumatic? despatch tube apparatus and especially to E such apparatus wherein large carriers are used for the transmission of mail matter, merchandise and the like.
  • the object of my invention is to produce a machine simple in construction and ellicient in operation and which is constructed so as to occupy very small floor space.
  • Figure l is a plan view of the receiving terminal.
  • Fig. 2 is a side elevation of same.
  • Fig. 3 is an end elevation of same.
  • Fig. 4 is a plan view of a portion of the goose neck with-part of the upper portion cut away and showing a carrier in position.
  • Fig. 5 is an elevation of a portion of the goose neck showing a carrier in position.
  • Fig. 6 represents the section of the goose neck.
  • the object of the present invention is to construct a goose neck of such a shaped section that the radius can be made very l small and therefore very little floor space occupied.
  • the operation is as follows:
  • the current of air coming up through the transmission tube A is the source of supply for the com pressor operating the return line, these tubes always being placed in pairs.
  • This current of air passes from the transmission tube A, through the slotted casing A into the return tube A to the compressor above men tioned.
  • a carrier coming into the receiving machine from the transmission tube A passes through the slotted casing A into the bend A where it is turned into a horizontal position and enters the goose neck B passing around same and losing most of its momentum, it reaches the end of the goose neck B and strikes the buffer C and then rolls down on to the table D.
  • the horizontally disposed gooseneck is curved to a comparatively short radius and has an open inner face.
  • the main part of the goose-neck B has a cross-area sufliciently large to receive and carry the rings E on the carrier E.
  • the chamber or passage B In the back or convex side of the goose-neck is the chamber or passage B the curve of which is made on a greater radius than that of the main part of the goose-neck.
  • This chamber or passage is sufliciently large in crosssection to receive and clear the ends of the carrier, which overhang the rings E as the carrier moves around the curve of the goose-neck.
  • the dash line E represents the periphery at the end of the overhanging portion E of the carrier E.
  • the carrier E slides on the rings E
  • the dot and dash line B represents what would be the wall B of the goose neck 13 were same carried around in the usual manner.
  • the dash line E and the dot and dash line B are taken in the same plane. It will be seen in Fig. 5 that the dash line E overhangs the dot and dash line B and if the goose neck were constructed in the usual manner the periphery of the end of the overhang of the carrier would rub against the back wall of the goose neck. In order to avoid this, the goose neck is constructed with the chambered portion B and as the carrier is passing around the goose neck the overhang portion extends into this chamber B and the carrier slides on the rings E Having thus described the nature of my invention and set forth a construction embodying the same, what I claim as new and desire to secure by Letters Patent of the United States is:
  • a transmission tube for carriers and an open curved goose-neck located at the end of said transmission tube to receive the carriers, said goose-neck having a main part with a cross-area sui'ticiently large to receive the rings of the carrier and provided with a passage in its convex side curved to a greater radius than the main part of the goose-neck and having a crossarea sufliciently large to receive and clear the ends of the carrier as the latter moves around the curve of the goose-neck.
  • a transmission tube In a receiving terminal for pneumatic tube apparatus, a transmission tube; an open horizontally disposed gooseneck connected with said tube, curved to a comparatively short radius, having a main part with a cross-area sufliciently large to receive the rings of the carrier, and provided with a passage in its convex side curved to a greater radius than the main part with a cross-area suiticiently large to receive and clear the ends of the carrier as the latter moves around the curve of the goose-neck; and a table at the end of said gooseneck opening into the same.

Description

0. F. STODDARDQ- PNEUMATIC DESPATOH TUBE SYSTEM. APPLIGATIQN FILED JULY 20, 1907.
Patented June 1, 1909.
2 SHEETS-SHEET 1.
WITNESSES:
ATTORNEYJ G. F. STODDARD.
PNEUMATIC DESPATOH TUBE SYSTEM.
APPLICATION FILED JULY 20, 1907.
Patented June 1, 1909.
2 SHEETS-SHEET 2.
A TTORNEYQ I rs: mmms PETERS 60., wnsumcron. n. c.
UNITED STATES FFEQE.
CHARLES F. STODDARD, OF BOSTON, MASSACHUSETTS, ASSIGNOR TO AMERICAN PNEU- MATIC SERVICE COMPANY, OF DOVER, DELAWARE, A CORPORATION OF DELAWARE.
PNEUMATIO-DESPATCH-TUBE SYSTEM.
Specification of Letters Patent.
Patented June 1, 1909.
Application filed July 20, 1907. Serial No. 384,725.
0 all whom it may concern: 1
Be it known that I, CHARLES F. Sronnum, i of Dorchester, Boston, in the county of j Suffolk and State of Massachusetts, have; invented certain new and useful Improvements in Pneumatic-Despatch-Tube Systems, of which the following is a specifica- 1 tion.
My invention relates to new and useful 5 improvements in terminals for pneumatic? despatch tube apparatus and especially to E such apparatus wherein large carriers are used for the transmission of mail matter, merchandise and the like.
The object of my invention is to produce a machine simple in construction and ellicient in operation and which is constructed so as to occupy very small floor space.
My invention consists in certain novel to: tures hereinafter described and particularly pointed out in the claims.
Tn the accompanying drawings are illustrated a construction embodying my invention.
Figure l is a plan view of the receiving terminal. Fig. 2 is a side elevation of same. Fig. 3 is an end elevation of same. Fig. 4 is a plan view of a portion of the goose neck with-part of the upper portion cut away and showing a carrier in position. Fig. 5 is an elevation of a portion of the goose neck showing a carrier in position. Fig. 6 represents the section of the goose neck.
'Like letters of reference refer to like parts throughout the several views. I
In a pneumatic despatch system working i under pressure, the air is compressed at one end of the tube and gradually expands until i it reaches atmospheric pressure at the other end, and it is at this end of the tube where the air has reached atmospheric pressure that the terminal herein described is to be placed. In large tubes where the carriers 5 have considerable weight, it is necessary to provide some means for bringing them to a stop in a manner which will be safe and cause no damage to them. Numerous means are at present in use, such as cushioning the carrier in the dead end of the tube and then opening the dead end and discharging the carrier on to a suitable receiving table. Another means is to allow the carrier to 1 come out of the end of the tube at full speed into the goose neck. On account of the peculiar construction of carriers used in large tube service, it is necessary to build this goose neck with a radius so large that the over-hanging ends of the carrier will not come in contact with the wall of the goose neck. The object of the present invention is to construct a goose neck of such a shaped section that the radius can be made very l small and therefore very little floor space occupied.
The operation is as follows: The current of air coming up through the transmission tube A is the source of supply for the com pressor operating the return line, these tubes always being placed in pairs. This current of air passes from the transmission tube A, through the slotted casing A into the return tube A to the compressor above men tioned. A carrier coming into the receiving machine from the transmission tube A passes through the slotted casing A into the bend A where it is turned into a horizontal position and enters the goose neck B passing around same and losing most of its momentum, it reaches the end of the goose neck B and strikes the buffer C and then rolls down on to the table D. The horizontally disposed gooseneck is curved to a comparatively short radius and has an open inner face. The main part of the goose-neck B has a cross-area sufliciently large to receive and carry the rings E on the carrier E. In the back or convex side of the goose-neck is the chamber or passage B the curve of which is made on a greater radius than that of the main part of the goose-neck. This chamber or passage is sufliciently large in crosssection to receive and clear the ends of the carrier, which overhang the rings E as the carrier moves around the curve of the goose-neck. In Fig. 5 the dash line E represents the periphery at the end of the overhanging portion E of the carrier E. The carrier E slides on the rings E The dot and dash line B represents what would be the wall B of the goose neck 13 were same carried around in the usual manner. The dash line E and the dot and dash line B are taken in the same plane. It will be seen in Fig. 5 that the dash line E overhangs the dot and dash line B and if the goose neck were constructed in the usual manner the periphery of the end of the overhang of the carrier would rub against the back wall of the goose neck. In order to avoid this, the goose neck is constructed with the chambered portion B and as the carrier is passing around the goose neck the overhang portion extends into this chamber B and the carrier slides on the rings E Having thus described the nature of my invention and set forth a construction embodying the same, what I claim as new and desire to secure by Letters Patent of the United States is:
1. In a receiving terminal for pneumatic tube apparatus, a transmission tube for carriers, and an open curved goose-neck located at the end of said transmission tube to receive the carriers, said goose-neck having a main part with a cross-area sui'ticiently large to receive the rings of the carrier and provided with a passage in its convex side curved to a greater radius than the main part of the goose-neck and having a crossarea sufliciently large to receive and clear the ends of the carrier as the latter moves around the curve of the goose-neck.
2. In a receiving terminal for pneumatic tube apparatus, a transmission tube; an open horizontally disposed gooseneck connected with said tube, curved to a comparatively short radius, having a main part with a cross-area sufliciently large to receive the rings of the carrier, and provided with a passage in its convex side curved to a greater radius than the main part with a cross-area suiticiently large to receive and clear the ends of the carrier as the latter moves around the curve of the goose-neck; and a table at the end of said gooseneck opening into the same.
In testimony whereof, I have signed my name to this specification in the presence 01 two subscribing witnesses, this 18th day of July A. D. 1907.
CHARLES I SIODDARD.
IVitnesses L. G. BARTLETT, A. L. i InssnR.
US38472507A 1907-07-20 1907-07-20 Pneumatic-despatch-tube system. Expired - Lifetime US923459A (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3298632A (en) * 1965-11-03 1967-01-17 Midwest Bank Builders Inc Drive-in banking system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3298632A (en) * 1965-11-03 1967-01-17 Midwest Bank Builders Inc Drive-in banking system

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