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US1689807A - Hydroplane - Google Patents

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Publication number
US1689807A
US1689807A US151058A US15105826A US1689807A US 1689807 A US1689807 A US 1689807A US 151058 A US151058 A US 151058A US 15105826 A US15105826 A US 15105826A US 1689807 A US1689807 A US 1689807A
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US
United States
Prior art keywords
supplementary
runners
pontoons
aeroplane
attached
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
US151058A
Inventor
Carl H Traver
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
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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 US151058A priority Critical patent/US1689807A/en
Application granted granted Critical
Publication of US1689807A publication Critical patent/US1689807A/en
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Expired - Lifetime legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C35/00Flying-boats; Seaplanes

Definitions

  • This invention relates toimprovements in aeroplanes and in particular. to adjustable devices so as to render the aeroplane more useful. 7 a
  • the object of the invention is to provide a means of permitting the aeroplane to land on waterg-snow, ice or the like.
  • Fig. 1 shows a side elevational view of an aeroplane equipped with my improved device.
  • Fig. 2 shows a front elevational view thereof.
  • y y I Fig. 3 shows a top plan view thereof.
  • Fig. 4 shows an enlarged longitudinal detail sectional view of my improveddevice.
  • Fig. 5 shows an enlarged transverse sec-' tional view taken on the line 55 of Fig. 4.
  • Fig. 6 shows a further development of my improved device.
  • the fuselage 10 the body 11, the motor 12,
  • the controls 15, the fuel tank 16 are the general elements of an acreplane, such as commonly used for flying. It
  • the struts 16 extend downwardly from the body 11 and are hinged, as at 18, to the pontoons 19, which extend longitudinally to the body 11.
  • the pontoons 19 are formed or shaped so'as to provide a V shaped section, terminatingin a pointed element 20.
  • the above described construction being such as will permit the pontoons 19 to be 'displaced'from the body 11, so as to provide a better means of landing on the said pontoons. Itbeing.understoodthat the struts 16, may be hinged to the lugs 21, for the purpose as here stated;
  • a means of extending the supplerotatively mounted in suitable supports attached to the pontoon 22 The bevel pinions 30 and 31 are attached to the shafts 28 and 29, respectively and mesh with the bevel pinions 32 and 33., respectively, attached to the worm wheels 34 and 35, respectively.
  • the worm wheels 34 and 35 are rotatively mount-- ed in the pontoon 19 and mesh with Worm racks 36 and 37, slidablymounted in the run 1101' 22.
  • the supplementary runner 22 is of convex construction andv extends the entire length of the runner 20.
  • runners attached to pontoons, and a means of extending the said supplementary runners.
  • An aeroplane comprising pontoons, supplementary runners attached to the said pontoons and a means of'extending the said supplementary runners.
  • An aeroplane comprising pontoons, supplementary runners mounted in the said pontoons, and a means of extending the said supplemenary runners.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tents Or Canopies (AREA)

Description

Oct. 30, 1928 1,689,807
c. H. TRAVER HYDRO-PLANE Original Fil ed Nov. 27, 1926 2 sheets-sheet 1 IN VENT OR T BY C df/ HjFaver ATTORNEY Get. 30, 1928.
C. H. TRAVER HYDROPLANE Original Filed Nov. 27, 1926 2 Sheets-Sheet INVENTOR Car/ H. Tmver' A TTORNEY Patented Oct. 30, 1928.
UNITED STATES PATENT OFFICE.
CARL TRAVER, OF BINGHAMTON, NEW YORK.
' nxnnornnnn.
Application filed November 27, 1926, Serial No. 151,058. Renewed April 18, 1928.v
This invention relates toimprovements in aeroplanes and in particular. to adjustable devices so as to render the aeroplane more useful. 7 a
The object of the invention is to provide a means of permitting the aeroplane to land on waterg-snow, ice or the like. I p
In the accompanying drawings:
Fig. 1 shows a side elevational view of an aeroplane equipped with my improved device.
Fig. 2 shows a front elevational view thereof. y y I Fig. 3 shows a top plan view thereof.
Fig. 4 shows an enlarged longitudinal detail sectional view of my improveddevice.
Fig. 5 shows an enlarged transverse sec-' tional view taken on the line 55 of Fig. 4.
Fig. 6 shows a further development of my improved device. t
The fuselage 10, the body 11, the motor 12,
operatively connected to the propeller 13, the
operators seat 14, the controls 15, the fuel tank 16 are the general elements of an acreplane, such as commonly used for flying. It
being understood that I do not necessarily limit the use of'my invention to monoplanes such as here illustrated, but to biplanes and all types and classes of aeroplanes such as are manufactured and used for all purposes.
Referring in particular to Fig. 6 of the accompanying drawings in which the undercarriage comprises a plurality of struts 16,
hinged, as at 17, to the body 11. The struts 16, extend downwardly from the body 11 and are hinged, as at 18, to the pontoons 19, which extend longitudinally to the body 11. The pontoons 19 are formed or shaped so'as to provide a V shaped section, terminatingin a pointed element 20. The above described construction being such as will permit the pontoons 19 to be 'displaced'from the body 11, so as to provide a better means of landing on the said pontoons. Itbeing.understoodthat the struts 16, may be hinged to the lugs 21, for the purpose as here stated;
Referring in particular to Figs; 4 and 5 of the accompanying drawings in which I have provided a means of extending the supplerotatively mounted in suitable supports attached to the pontoon 22. The bevel pinions 30 and 31 are attached to the shafts 28 and 29, respectively and mesh with the bevel pinions 32 and 33., respectively, attached to the worm wheels 34 and 35, respectively. The worm wheels 34 and 35 are rotatively mount-- ed in the pontoon 19 and mesh with Worm racks 36 and 37, slidablymounted in the run 1101' 22. The supplementary runner 22 is of convex construction andv extends the entire length of the runner 20. {The worm racks 36 and 37 are attached at'their lower extremities to the supplementary runners 22. The above described construction being such as will permi tthe hand wheel 23, when turned or rotated, to lower or extend the supplementary I runner 22, for the purpose as hereinbefore set forth. v Having thus described my invention, what I claim asnew'and desire to protect by Let ters Patent of theUnited States is as follows: i
1. In an aeroplane, runners attached to pontoons, and a means of extending the said supplementary runners.
2. An aeroplane comprising pontoons, supplementary runners attached to the said pontoons and a means of'extending the said supplementary runners.
An aeroplane comprising pontoons, supplementary runners mounted in the said pontoons, and a means of extending the said supplemenary runners.
- 4. In an aeroplane, a means of extending runners attached to pontoons, a hand-wheel operatively connected to the said supplementively connected to supplementary runners,
asa means of extending the said supplementary runners, said supplementary runners mounted in pontoons.
supplementary runners, said supplementary In testimony whereof I have affixed my signature.
CARL H. TBAVEE:
US151058A 1926-11-27 1926-11-27 Hydroplane Expired - Lifetime US1689807A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US151058A US1689807A (en) 1926-11-27 1926-11-27 Hydroplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US151058A US1689807A (en) 1926-11-27 1926-11-27 Hydroplane

Publications (1)

Publication Number Publication Date
US1689807A true US1689807A (en) 1928-10-30

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Family Applications (1)

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US151058A Expired - Lifetime US1689807A (en) 1926-11-27 1926-11-27 Hydroplane

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2544794A (en) * 1950-03-14 1951-03-13 Bell Aircraft Corp Helicopter amphibious landing gear

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2544794A (en) * 1950-03-14 1951-03-13 Bell Aircraft Corp Helicopter amphibious landing gear

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