US1874545A - Propeller - Google Patents

Propeller Download PDF

Info

Publication number
US1874545A
US1874545A US507729A US50772931A US1874545A US 1874545 A US1874545 A US 1874545A US 507729 A US507729 A US 507729A US 50772931 A US50772931 A US 50772931A US 1874545 A US1874545 A US 1874545A
Authority
US
United States
Prior art keywords
propeller
blades
sections
hub
blade
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
US507729A
Inventor
Lynn J Koch
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 US507729A priority Critical patent/US1874545A/en
Application granted granted Critical
Publication of US1874545A publication Critical patent/US1874545A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H5/00Arrangements on vessels of propulsion elements directly acting on water
    • B63H5/07Arrangements on vessels of propulsion elements directly acting on water of propellers
    • B63H5/08Arrangements on vessels of propulsion elements directly acting on water of propellers of more than one propeller
    • B63H5/10Arrangements on vessels of propulsion elements directly acting on water of propellers of more than one propeller of coaxial type, e.g. of counter-rotative type
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H5/00Arrangements on vessels of propulsion elements directly acting on water
    • B63H5/07Arrangements on vessels of propulsion elements directly acting on water of propellers
    • B63H5/08Arrangements on vessels of propulsion elements directly acting on water of propellers of more than one propeller
    • B63H5/10Arrangements on vessels of propulsion elements directly acting on water of propellers of more than one propeller of coaxial type, e.g. of counter-rotative type
    • B63H2005/103Arrangements on vessels of propulsion elements directly acting on water of propellers of more than one propeller of coaxial type, e.g. of counter-rotative type of co-rotative type, i.e. rotating in the same direction, e.g. twin propellers

Definitions

  • a very important object of the present invention is to provide a propeller which is capable of great pulling efiect with minimum motor speed.
  • a still further object of the invention is to provide a propeller of such a form in construction to be hereinafter more fully described, as will eliminate the spreading of water over the circumference of the propeller wheel area.
  • a still further object of the invention is to provide a propeller including a plurality of sections each of which is a complete propeller in itself, and the sections so arranged as to create in operation, equal pressure to all the sections or parts thereof in parallel direction of motion for discharging an equal amount of water at the rear of each unit as is taken in by the unit at the forward end thereof such a discharge being parallel throughout.
  • a still further object of the invention is to provide a propeller of the above mentioned character, and wherein each unit is of such a construction as to provide for an equal strain throughout the entire unit.
  • Figure 1 is a side elevational view of a sectional propeller, showing the same as applieo to a marine vessel.
  • Figure 2 is an end elevational view of the propeller unit.
  • Figure 3 is a plan view thereof.
  • Figures 4 and 5 are transverse sectional views taken substantially on the lines H and 5-5 respectively of Figure 2.
  • Figure 6 is an end view of the propell clearly illustrating the relative positions of the several units.
  • the propeller may be composed of any desired number of sections, respectively including a hub'having secured or formed integral therewith the propeller blades 6.
  • Each of the sections is provided with two blades extending oppositely from the hub, and it is 'to be noted that theblades join the hub tangentially as shown, the roots or inner edges of the blade being diametrically oposite one another.
  • the blades are 0 2 0 positely curved longitudinally and in the direction of rotation of the propeller, the front surfaces of the blades being concave, and the rear surfaces being convened.
  • the leadingedges 9 of the blades are concaved, and the rear or trailing edges 10 convex.
  • Each blade increases in width from the root 40f the blade to the outer end or. tip of the blade, the forward or leading edge-9 of the blade being curved a greater degree than the trailing or rear edge 10 of the blade so that as will be noted, the blades are of greater wic th adjacent their tips than adjacent the roots of the'blades.
  • each blade is brought to an edge by beveling away the material from the front or convex side 7 as at-ll instead of from the rear or concaved side 8 of the blade.
  • each blade Adjacent its trailing edge each blade. is beveled on its concave or rear side -8 as at 12.
  • Each of said blades at its root 4.- joins the hub of the propeller that the blades extend from the hub obliquely to the axes of the hub with the leading edge of the blade at the root 4 terminating flush with the forward end of the hub, and the trailing edge of said root terminating flush with the rear end of the hub,-tl1e leading and trailing edges respectively of the blades springing from the hub at said roots tangential to the hub.
  • each propeller section is a unit in itself independent of the remaining sections'of the propeller, and that the additi'on'or removal of one or more sections will not weaken the remaining sections of the propeller; further the number of sectionscontituting the propeller maybe varied at will.
  • a propeller comprising-a :pluralityof units hvingfhubs'and oppositely projecting blades secured toLthe hub and having the inner portions thereof overlapping, said blades being longitudinally curved inopposite directions,

Description

L. J. KOCH Aug. 30, 1932.
PROPELLER Filed Jan. 9, 1931 2 Sheets-Sheet Aug. 30, 1932. J. KOCH 1,874,545
PROPELLER Filed Jan. 9, 1931 2 Sheets-Sheet 2 l 1 CONVEX 4; r
CONVEX I I l CONCAVE Attorney Inventor Patented Aug. 30, 1932 UNITE LYNN J. KOCH, OF ALLENTOWN, PEfi NSYLVANIA PROPELLER This invention relates to certain new and useful improvements in propellers, and the primary object of this invention is to provide a propeller for use in propelling a marine vessel or an airship as may be found desirable.
A very important object of the present invention is to provide a propeller which is capable of great pulling efiect with minimum motor speed.
A still further object of the invention is to provide a propeller of such a form in construction to be hereinafter more fully described, as will eliminate the spreading of water over the circumference of the propeller wheel area.
A still further object of the invention is to provide a propeller including a plurality of sections each of which is a complete propeller in itself, and the sections so arranged as to create in operation, equal pressure to all the sections or parts thereof in parallel direction of motion for discharging an equal amount of water at the rear of each unit as is taken in by the unit at the forward end thereof such a discharge being parallel throughout.
A still further object of the invention is to provide a propeller of the above mentioned character, and wherein each unit is of such a construction as to provide for an equal strain throughout the entire unit.
Other objects and advantages of the invention will become apparent from a study of the following description, taken in connection with the accompanying drawings where- Figure 1 is a side elevational view of a sectional propeller, showing the same as applieo to a marine vessel.
Figure 2 is an end elevational view of the propeller unit.
Figure 3 is a plan view thereof.
Figures 4 and 5 are transverse sectional views taken substantially on the lines H and 5-5 respectively of Figure 2.
Figure 6 is an end view of the propell clearly illustrating the relative positions of the several units.
With reference more in detail to the drawings, it will be apparent that the propeller may be composed of any desired number of sections, respectively including a hub'having secured or formed integral therewith the propeller blades 6. I
Each of the sections is provided with two blades extending oppositely from the hub, and it is 'to be noted that theblades join the hub tangentially as shown, the roots or inner edges of the blade being diametrically oposite one another. The blades are 0 2 0 positely curved longitudinally and in the direction of rotation of the propeller, the front surfaces of the blades being concave, and the rear surfaces being convened.
The leadingedges 9 of the blades are concaved, and the rear or trailing edges 10 convex. Each blade increases in width from the root 40f the blade to the outer end or. tip of the blade, the forward or leading edge-9 of the blade being curved a greater degree than the trailing or rear edge 10 of the blade so that as will be noted, the blades are of greater wic th adjacent their tips than adjacent the roots of the'blades.
The cutting or leading edge 9 of each blade is brought to an edge by beveling away the material from the front or convex side 7 as at-ll instead of from the rear or concaved side 8 of the blade. r
Adjacent its trailing edge each blade. is beveled on its concave or rear side -8 as at 12. Each of said blades at its root 4.- so joins the hub of the propeller that the blades extend from the hub obliquely to the axes of the hub with the leading edge of the blade at the root 4 terminating flush with the forward end of the hub, and the trailing edge of said root terminating flush with the rear end of the hub,-tl1e leading and trailing edges respectively of the blades springing from the hub at said roots tangential to the hub.
In Figure. 1 I have shown the propeller wheel-as applied to .a marine vessel designated generally 'by the reference character V. In this instance the propeller wheel 'consists of two of such sections herein described in detail the said sections being suitably keyed to the propeller shaft S. In Figure 6 I have shown the propeller wheel as consisting of three of such sections, and as is s'rares PATENT OFF CE apparent, irrespective of the number of sections to be used, it will be noted that when the sections are assembled on the propeller shaft S, each unit is set a fraction of a turn relative to the next preceding unit so that the blades extend fanwise from diametrically opposite sides of the shaft Sso that the concave surtfaces confer-into a continuous rotary surface as shown.
The concave surfaces providing the propolling surface for the propeller, it will 'be apparent that when the fluid element is gathered in by the blades, it will be forced not only rearwardly but also inwardly toward the axes of the propeller, the hollow sides of the blades holding the water in circumferonce or pipeline formation thereby delivering-the full force of water against the rear body of water by each unit instead of only part of the water being held to the rear, and the remaining part being forced radially outwardly toward the circumference of the wheel. Y
A still further advantage of an invention of thischaracter will 'be, that when not inuse, the sections may be readily stored, and furthenlth at in the event of breakage 'to oneofthe'units, the same may be replaced with facility.
It will be also noted that each propeller section is a unit in itself independent of the remaining sections'of the propeller, and that the additi'on'or removal of one or more sections will not weaken the remaining sections of the propeller; further the number of sectionscontituting the propeller maybe varied at will. I
:In making the propeller sectional, and each section or unit being practically an exact replica of the othersection, eliminates expensive individual patterns and reduces cost 7 of manufacture.
Even though I have herein shown and described the preferred'enibodiment of the in- Wention, it is to be understood that'the same is susceptible of changes, modifications and improvements coming within the scope of the appended claim.
Havingfthus described my invention, what claim as new is: p r
A propeller comprising-a :pluralityof units hvingfhubs'and oppositely projecting blades secured toLthe hub and having the inner portions thereof overlapping, said blades being longitudinally curved inopposite directions,
theiblndesoncorresponding sides of the hubs baiiag soarranged relative to one another as to extend fanwise from the propeller shaft with-thertips of the blade-edge to edge. I
testimony whereof I aflix my signa- LYNN J. KOCH.
US507729A 1931-01-09 1931-01-09 Propeller Expired - Lifetime US1874545A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US507729A US1874545A (en) 1931-01-09 1931-01-09 Propeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US507729A US1874545A (en) 1931-01-09 1931-01-09 Propeller

Publications (1)

Publication Number Publication Date
US1874545A true US1874545A (en) 1932-08-30

Family

ID=24019870

Family Applications (1)

Application Number Title Priority Date Filing Date
US507729A Expired - Lifetime US1874545A (en) 1931-01-09 1931-01-09 Propeller

Country Status (1)

Country Link
US (1) US1874545A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4687416A (en) * 1981-02-13 1987-08-18 Spranger Guenther Method and device for decreasing the flow resistance on wings particularly aerofoils and blades of turbomachines exposed to gas flux such as air
AT502673B1 (en) * 2006-06-01 2007-05-15 Talamoni Marco Variable pitch-propeller for e.g. ship, has individual propellers rotating relative to each other such that different helical flow channels are formed, where shape of channels is changed relative to each other
ITTO20130260A1 (en) * 2013-03-29 2014-09-30 Ship And Ocean Ind R & D C Enter ELICA SUITABLE FOR ALL SPEEDS WITH AIMS.
US20190185143A1 (en) * 2017-12-19 2019-06-20 Wing Aviation Llc Fiber Sheet Stacked Rotor Design

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4687416A (en) * 1981-02-13 1987-08-18 Spranger Guenther Method and device for decreasing the flow resistance on wings particularly aerofoils and blades of turbomachines exposed to gas flux such as air
AT502673B1 (en) * 2006-06-01 2007-05-15 Talamoni Marco Variable pitch-propeller for e.g. ship, has individual propellers rotating relative to each other such that different helical flow channels are formed, where shape of channels is changed relative to each other
WO2007137859A2 (en) 2006-06-01 2007-12-06 Marco Talamoni Arrangement with several corotating propellers which are variable relative to each other
WO2007137859A3 (en) * 2006-06-01 2008-07-10 Marco Talamoni Arrangement with several corotating propellers which are variable relative to each other
ITTO20130260A1 (en) * 2013-03-29 2014-09-30 Ship And Ocean Ind R & D C Enter ELICA SUITABLE FOR ALL SPEEDS WITH AIMS.
US20190185143A1 (en) * 2017-12-19 2019-06-20 Wing Aviation Llc Fiber Sheet Stacked Rotor Design
US10689095B2 (en) * 2017-12-19 2020-06-23 Wing Aviation Llc Fiber sheet stacked rotor design
US11214356B2 (en) * 2017-12-19 2022-01-04 Wing Aviation Llc Fiber sheet stacked rotor design

Similar Documents

Publication Publication Date Title
US1041913A (en) Aerial propeller.
US4741670A (en) Propeller combination for a boat propeller unit
US2259247A (en) Propeller blade
US1758560A (en) Aircraft propeller
US2013473A (en) Fluid propeller
US1874545A (en) Propeller
US2116055A (en) Propeller
US1371610A (en) Screw-propeller
US2023454A (en) Propeller
US2086307A (en) Screw propeller and the like
US1977072A (en) Aircraft propeller
US2327453A (en) Helical marine propeller
US2359466A (en) Air impeller
US1949611A (en) Propeller blade
US2754919A (en) Propeller
US652123A (en) Screw-propeller.
US2116054A (en) Propeller
US1855660A (en) Fan
US1834888A (en) Propeller
US2087243A (en) Propeller
US1889717A (en) Aircraft propeller
US2134921A (en) Propeller
US1515268A (en) Propeller
US2111947A (en) Propeller
US2161932A (en) Propeller