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US1060531A - Folding pontoon. - Google Patents

Folding pontoon. Download PDF

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Publication number
US1060531A
US1060531A US71306312A US1912713063A US1060531A US 1060531 A US1060531 A US 1060531A US 71306312 A US71306312 A US 71306312A US 1912713063 A US1912713063 A US 1912713063A US 1060531 A US1060531 A US 1060531A
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US
United States
Prior art keywords
lazy
tongs
ribs
pontoon
levers
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
US71306312A
Inventor
William J Bond
Frederick A Bond
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.)
HENRY ENEU JOHNSON
Original Assignee
HENRY ENEU JOHNSON
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 HENRY ENEU JOHNSON filed Critical HENRY ENEU JOHNSON
Priority to US71306312A priority Critical patent/US1060531A/en
Application granted granted Critical
Publication of US1060531A publication Critical patent/US1060531A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/02Undercarriages
    • B64C25/08Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/14Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like fore-and-aft

Definitions

  • Our invention relates to improvements in pontoons and more particularly toimprovements in pontoons for use in connection with aeroplanes, the object of our invention being to furnish a folding pontoon which can e extended by an operator in an aeroplane to form a float for supporting the same upon the water, and which may be folded so as to fi'era minimum resistance to the air when the aeroplane is in flight.
  • Figure 1 is a plan view of our pontoon closed; Fig. 2, a plan view of one side of the pontoon when opened; Fig. 3, a transverse section of Fig. 1 on line A-A; Fig. 4-, a similar section showing the pontoon opened; Fig. ri aside elevation of the pontoon; Figffifa viewof the ends of ,a painof ribs showing the method of connecting them; Fig. 7 a perspective view of metal connection for pivotally securing ribs to ends of lazy-tongs.
  • the extensible and collapsible framework of our pontoon consists of a suitable number of arms 12 of equal, or substantially equal, length pivoted together in pairs at their middles by pivots 3 and at their ends by pivots 4, the above forming a la zy-tongs structure.
  • the lazy-tongs of whichthere may be two or more, are placed parallel to one another and at right. angles, or transthe longitudinal axis of the aeroplane.
  • ribs at the tops and bottoms and at right angles to the lazy-tong levers are pivotally secured to the arms l-2 at the outer ends of the latter and the ends of each pair of ribs are bent toward and secured to one another at their endsl
  • the connection between the ends of the ribs flexible one, for instance, two pieces of wire 7 forming eyes 8 which interlock as shown best in Fig. 6, one wire being carried by one rib the other by the other.
  • the lazy-tongs are connected to one another at their middles by bars 9. i
  • each set of lazy-tongs carry pivotally a rib 14 which rib, like the ribs 56, is preferably made of'a narrow thin strip of tough flexible wood.
  • the means for pivotally attaching the ribs to theends of the arms of the lazy-tongs can be simply a piece of fiat metal 16 lashed or otherwise secured to the ribs, bent at right angles so as to enter between the ends of the arms 12 and perforated at 15 for the passage of the pin or rivet 4 which secures together the. ends of the arms-a perspective view of one of these fastenings is shown in Fig. 7.
  • the ribs. are covered with a flexible waterproof covering 17 so made that when the lazy-tongs are extended it will present a practically smooth surface and when these lazy-tongs are collapsed will fold in between hem in a bellows fashion as shown in Fig. 3.
  • the covering 17 is preferably made in two parts leaving the inner ends of the central arms uncovered as shown best in Fig. 4; the coverings, at their inner ends, passing HEIGHTS, PENNSYLVANIA,
  • the coverings may be secured to an elastic cord or spring 18,
  • the pontoon is connected to the body of the aeroplane, which is not shown, by struts 19 which are secured to the keel 10, or some other suitable part of the structure and it'may be opened or closed by lifting or depressing a rod 20 the lower end of which is connected to the ends of one of the sets of arms 1- 2, or in any other suitable and convenient manner.
  • 21 is a guard secured to keel 10 and extending out at right angles from each side thereof the purpose of which is to form a .should it be necessary to bring the machine to the ground.
  • a pontoon in combination, two or more sets of lazy-tong levers placed in parallel, ribs at right angles to and pivotally secured to the ends of said arms forming 40 said levers, said ribs being arranged in pairs one at the top and the other at thebottom of said levers, a connection joining the ends of each pair of ribs, a-flexible covering inclosi ng saidribs and levers, and means for distending or collaijgisingsaidlevers.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Bridges Or Land Bridges (AREA)

Description

W. J. & P. A. BOND.
FOLDING PONTOON.
APPLICATION FILED AUG. 3, 1912.
1 60,531 Patented Apr. 29, 1913.
2 SHEETS-SHEET 1.;
W W w HTHI ll V |NVENTOR\ W J. & F. A. BOND. FOLDING PONTOON.
APPLICATION FILED AUG.3, 1912.
1,060,531, Patented Apr. 29,1913.
2 SHEETS-SHEET 2.
WITNESSES ATTORN EY WILLIAM J. BONED AND FREDERICK A, BOND, OF CLIFTON ASSIGNORS F ONE-FIFTH T0 HENRY ENEU JOHNSON, 0F LANSDOWNE, PENNSYL- VANIA.
ronnme IONTOON.
Specification of Letters Patent.
Patented Apr. 29, 1913.
\ To all whom it may concern:
" versely, to
is preferably a Be it known that we, WILLIAM J. Bonnand FREDERICK A. Bo1 n), citizens of the United ,States, "and residents of Clifton Heights, Delaware county, Pennsylvania, have invented certain new and useful Improvements in Folding Pontoons, of which the following is a specification.
Our invention relates to improvements in pontoons and more particularly toimprovements in pontoons for use in connection with aeroplanes, the object of our invention being to furnish a folding pontoon which can e extended by an operator in an aeroplane to form a float for supporting the same upon the water, and which may be folded so as to fi'era minimum resistance to the air when the aeroplane is in flight.
In the accompanying drawings forming part of this specification, and in which similarlettersof reference indicate similar parts throughout the several views :Figure 1, is a plan view of our pontoon closed; Fig. 2, a plan view of one side of the pontoon when opened; Fig. 3, a transverse section of Fig. 1 on line A-A; Fig. 4-, a similar section showing the pontoon opened; Fig. ri aside elevation of the pontoon; Figffifa viewof the ends of ,a painof ribs showing the method of connecting them; Fig. 7 a perspective view of metal connection for pivotally securing ribs to ends of lazy-tongs.
The extensible and collapsible framework of our pontoon consists of a suitable number of arms 12 of equal, or substantially equal, length pivoted together in pairs at their middles by pivots 3 and at their ends by pivots 4, the above forming a la zy-tongs structure. The lazy-tongs, of whichthere may be two or more, are placed parallel to one another and at right. angles, or transthe longitudinal axis of the aeroplane.
5-6 are ribs at the tops and bottoms and at right angles to the lazy-tong levers. These ribs are pivotally secured to the arms l-2 at the outer ends of the latter and the ends of each pair of ribs are bent toward and secured to one another at their endsl The connection between the ends of the ribs flexible one, for instance, two pieces of wire 7 forming eyes 8 which interlock as shown best in Fig. 6, one wire being carried by one rib the other by the other. For purposes of rigidity the lazy-tongs are connected to one another at their middles by bars 9. i
10 is a keel midway of and at right angles to the lazy-tongs; 11 a bar between the lazyton'gs which is secured to the keel 10 and, near its end, pivotally attached to the ends of the middle link of the lazy-tongs. The end links of each set of lazy-tongs carry pivotally a rib 14 which rib, like the ribs 56, is preferably made of'a narrow thin strip of tough flexible wood. The means for pivotally attaching the ribs to theends of the arms of the lazy-tongs can be simply a piece of fiat metal 16 lashed or otherwise secured to the ribs, bent at right angles so as to enter between the ends of the arms 12 and perforated at 15 for the passage of the pin or rivet 4 which secures together the. ends of the arms-a perspective view of one of these fastenings is shown in Fig. 7.
The ribs. are covered with a flexible waterproof covering 17 so made that when the lazy-tongs are extended it will present a practically smooth surface and when these lazy-tongs are collapsed will fold in between hem in a bellows fashion as shown in Fig. 3.
To permit the manipulation of the lazytongs the covering 17 is preferably made in two parts leaving the inner ends of the central arms uncovered as shown best in Fig. 4; the coverings, at their inner ends, passing HEIGHTS, PENNSYLVANIA,
around the two inner bars 9 which secure 1 the two sets of lazy-tongs together. Midway between the ribs 14 the coverings may be secured to an elastic cord or spring 18,
which is also secured to bar 9, or to the opposite side of the covering, the purpose of which is to draw the covering in between the arms 1-2, as shown in Fig. 3, when the latter are folded. The pontoon is connected to the body of the aeroplane, which is not shown, by struts 19 which are secured to the keel 10, or some other suitable part of the structure and it'may be opened or closed by lifting or depressing a rod 20 the lower end of which is connected to the ends of one of the sets of arms 1- 2, or in any other suitable and convenient manner.
21 is a guard secured to keel 10 and extending out at right angles from each side thereof the purpose of which is to form a .should it be necessary to bring the machine to the ground.
Having thus described our invention we claim as new and desire to secure by Letters Patentz-- 1. The combination with an aeroplane, of downwardly projecting struts carried by the frame of the machine, two or more sets of lazy-tongs carried by said struts at right angles to the longitudinal axis of the aeroplane, a flexible covering inclosing saidlazy-tongs, and means operative from said aeroplane for extending or collapsing said lazy-tongs and covering.
2. The combination with an aeroplane, of two or more downwardly projecting struts carried by its frame, two or more sets of lazy-tongs, one for .each strut, extending transversely at right angles to the longitudinal axis of the machine, one pair of adjoining arms of each lazy-tongs pivoted to a strut, a flexible covering inclosing said lazy-tongs, and rods connected to said lazytongs and operative from said aeroplane for extending or collapsing said lazy-tongs and flexible covering.
3. The combination with an aeroplane, of two or more downwardly projecting struts carried by its frame, a keel to which the lower ends of said struts are secured, a set oi lazy-tong, levers arranged at right angles to the keel and pivoted one to each strut, a"
flexible covering inclosing said lazy-tongs,
- or extended.
4. In a pontoon, in combination, two or more sets of lazy-tong levers placed in parallel, ribs at right angles to and pivotally secured to the ends of said arms forming 40 said levers, said ribs being arranged in pairs one at the top and the other at thebottom of said levers, a connection joining the ends of each pair of ribs, a-flexible covering inclosi ng saidribs and levers, and means for distending or collaijgisingsaidlevers.
5. In a pontoon, in combination two or more sets of lazy-tong levers placed parallel to one another, bars connecting the opposite ried in pairs by the tops and bottoms respectively of said levers, a connection joining the ends of each pair of ribs, a flexible covering inclosing said ribs and levers, and
centers of said levers, ribs pivotally carmeans whereby said levers may be collapsed 5E FREDERICK A. BOND. Y
, WILLIAM J. B
US71306312A 1912-08-03 1912-08-03 Folding pontoon. Expired - Lifetime US1060531A (en)

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US71306312A US1060531A (en) 1912-08-03 1912-08-03 Folding pontoon.

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US71306312A US1060531A (en) 1912-08-03 1912-08-03 Folding pontoon.

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2643835A (en) * 1950-07-11 1953-06-30 All American Eng Co Water planing undercarriage with flotation means for aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2643835A (en) * 1950-07-11 1953-06-30 All American Eng Co Water planing undercarriage with flotation means for aircraft

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