US1771365A - Aeroplane propeller - Google Patents

Aeroplane propeller Download PDF

Info

Publication number
US1771365A
US1771365A US222810A US22281027A US1771365A US 1771365 A US1771365 A US 1771365A US 222810 A US222810 A US 222810A US 22281027 A US22281027 A US 22281027A US 1771365 A US1771365 A US 1771365A
Authority
US
United States
Prior art keywords
plates
propeller
blades
aeroplane
shaft
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
US222810A
Inventor
Woll Joseph
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 US222810A priority Critical patent/US1771365A/en
Application granted granted Critical
Publication of US1771365A publication Critical patent/US1771365A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft

Definitions

  • This invention relates to a propeller primarily adapted for aeroplane use.
  • Another object is to provide a particular 7 construction wherein the propeller substan tially forms a triangle with the blades extending at least one-half the length of a side of the triangle so as to give maximum wind pressure and have two ways of forcing or impinging against the wind.
  • Figure 1 is a view of:the propeller in front elevation
  • Figure 2 is an edge view thereof, with parts partly broken away a-nd in section to disclose details;
  • Figure 3 is an elevation similar to Figure 1 but with the fastening elements partly removed and in section;
  • Figure 4 is a sectional view taken on the line IT-4 of Figure 1, and
  • Figure 5 is an edge view of one of the blades.
  • the propeller is made up ofthree or more blade elements 10 each comprising attaching plate portions 11 and blades proper 12, integral therewith. It will be noted that the blades 12 are disposed at an angle of 45 with respect tothe plates 11 and are approximately twice as long as the plates.
  • the blade members In assembling the blade members, they are arranged with the plates 11 in the same plane as shown particularly in Figure 3 so as to form triangle and the blades 12 extend at 7 least half way along the sides of said triangle'.
  • the meeting edges of the plates 11 are in diverging relation as shown particularly in Figure 3.
  • triangular securing plates 13 are provided and'they are secured together and to the plates 11 by means of removable bolts 14.
  • a shaft 15 Extending through the securing plates 13 and at the center of the triangle formed by plates 11, is a shaft 15, such shaft having a shoulder at 16 against which a hub 17 on one of the securng plates 13 abuts.
  • a hub 18 is provided on the other securing plate and a detachable key 19 extends through a slot 20 therein and through the hub 18, whereby the propeller is connected to the shaft against 6 relative turning movement.
  • Nuts 21 are threaded on the shaft 15beyond the hub 18 and one serves as a lock for the other.
  • the portions of the plates 11 engaging the shaft 15 are arcuate as at 22 in order to fit the same. While the triangular formation illustrate is preferred, it is to be understood that I do not limit myself to the use of three of the members 10 since any desired number maybe provided with the plates 13 shaped accordingly.
  • a propeller having one-piece blade members, each blade member consisting of an attaching plate and ablade longer than the same disposed at an angle to the plane thereof and at one'sideedge thereof, and
  • edges contact and in substantially the same 1 plane, said edges having arcuate portions to accommodate a shaft.
  • a propeller comprising one-piece blade members, said members comprising attaching plates and blades straight throughout and longer than said plates and disposed at an angle thereto, said blades being arran ed tangentially with respect to a circle descri ed from the center of the propeller, said plates extending laterally from said blades and “having diverging edges, said edges being arranged in contact, securing plates disposed against the first mentioned plates, fastening 7 elements detachably connecting the first mentioned plates and securing plates.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

July 22; 1930. WOLL 1,771,365
AEROPLANE PROPELLER Filed Sept. 29, 1927 Patented July 22, 1930 UNITED STATES JOSEPH WOLL, OF WOODVILLE, PENNSYLVANIA AEROPLANE PRQI'ELLER Application filed September 29, 1927. Serial No. 222,810.
I This invention relates to a propeller primarily adapted for aeroplane use.
It is'aimed to pi'ovide an exceedingly simple construction, which is efllcient and dur- 5 able and wherein the blades may be readily removed and replaced.
Another object is to provide a particular 7 construction wherein the propeller substan tially forms a triangle with the blades extending at least one-half the length of a side of the triangle so as to give maximum wind pressure and have two ways of forcing or impinging against the wind.
7 The more specific objects and advantages will become apparent from a consideration of thedescription following taken in connection with accompanying drawings illustrating an operative embodiment.
In said drawings Figure 1 is a view of:the propeller in front elevation;
Figure 2 is an edge view thereof, with parts partly broken away a-nd in section to disclose details; 1 Figure 3 is an elevation similar to Figure 1 but with the fastening elements partly removed and in section;
Figure 4 is a sectional view taken on the line IT-4 of Figure 1, and
Figure 5 is an edge view of one of the blades. p
Referring specifically to the drawings, the propeller is made up ofthree or more blade elements 10 each comprising attaching plate portions 11 and blades proper 12, integral therewith. It will be noted that the blades 12 are disposed at an angle of 45 with respect tothe plates 11 and are approximately twice as long as the plates.
In assembling the blade members, they are arranged with the plates 11 in the same plane as shown particularly in Figure 3 so as to form triangle and the blades 12 extend at 7 least half way along the sides of said triangle'. The meeting edges of the plates 11 are in diverging relation as shown particularly in Figure 3. On oppositesides of the plates 11, triangular securing plates 13 are provided and'they are secured together and to the plates 11 by means of removable bolts 14.
Extending through the securing plates 13 and at the center of the triangle formed by plates 11, is a shaft 15, such shaft having a shoulder at 16 against which a hub 17 on one of the securng plates 13 abuts. A hub 18 is provided on the other securing plate and a detachable key 19 extends through a slot 20 therein and through the hub 18, whereby the propeller is connected to the shaft against 6 relative turning movement. Nuts 21 are threaded on the shaft 15beyond the hub 18 and one serves as a lock for the other. V
The portions of the plates 11 engaging the shaft 15 are arcuate as at 22 in order to fit the same. While the triangular formation illustrate is preferred, it is to be understood that I do not limit myself to the use of three of the members 10 since any desired number maybe provided with the plates 13 shaped accordingly.
Various changes may be resorted to provided they fall within the spirit and scope of the invention. 7
I claim as my invention 1. A propeller having one-piece blade members, each blade member consisting of an attaching plate and ablade longer than the same disposed at an angle to the plane thereof and at one'sideedge thereof, and
means securing the attaching plates in edge. contact and in substantially the sameplane.
edge contact and in substantially the same 1 plane, said edges having arcuate portions to accommodate a shaft.
3. A propeller comprising one-piece blade members, said members comprising attaching plates and blades straight throughout and longer than said plates and disposed at an angle thereto, said blades being arran ed tangentially with respect to a circle descri ed from the center of the propeller, said plates extending laterally from said blades and "having diverging edges, said edges being arranged in contact, securing plates disposed against the first mentioned plates, fastening 7 elements detachably connecting the first mentioned plates and securing plates.
In testimony whereof I aflix my signature.
SErH WO
US222810A 1927-09-29 1927-09-29 Aeroplane propeller Expired - Lifetime US1771365A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US222810A US1771365A (en) 1927-09-29 1927-09-29 Aeroplane propeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US222810A US1771365A (en) 1927-09-29 1927-09-29 Aeroplane propeller

Publications (1)

Publication Number Publication Date
US1771365A true US1771365A (en) 1930-07-22

Family

ID=22833783

Family Applications (1)

Application Number Title Priority Date Filing Date
US222810A Expired - Lifetime US1771365A (en) 1927-09-29 1927-09-29 Aeroplane propeller

Country Status (1)

Country Link
US (1) US1771365A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2579119A (en) * 1950-03-02 1951-12-18 Singer Mfg Co Air impeller
US5183384A (en) * 1988-05-16 1993-02-02 Trumbly Joe H Foldable propeller assembly

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2579119A (en) * 1950-03-02 1951-12-18 Singer Mfg Co Air impeller
US5183384A (en) * 1988-05-16 1993-02-02 Trumbly Joe H Foldable propeller assembly

Similar Documents

Publication Publication Date Title
RU2016103594A (en) INSTALLED WING FINISHING DEVICE FOR INSTALLATION ON THE WIND TURBINE ROTOR BLADE
US1771365A (en) Aeroplane propeller
US2116055A (en) Propeller
US1779026A (en) Multiple-blade propeller
US978677A (en) Screw-propeller.
GB231919A (en) Improvements in the construction of screw propellers
JP2019069751A5 (en)
US2116054A (en) Propeller
US1809131A (en) Propeller
US2101535A (en) Reversible propeller
US1725482A (en) Propeller
US1241166A (en) Noiseless fan.
GB352507A (en) Improvements in and relating to screw propellers with flexible blades
US1977031A (en) Panelboard
US1634393A (en) Propeller
US2357084A (en) Paddle wheel structure
US2014242A (en) Propeller
US1733251A (en) Propeller
US1801216A (en) Winged screw propeller for aircraft
US1954309A (en) Propeller
GB303452A (en) Improvements in impeller screws such as those employed as rotary fans or pumps
US2134921A (en) Propeller
US1243885A (en) Propeller for aircraft.
GB312482A (en) Improvements in screw propellers
US2340709A (en) Propeller structure