US1036834A - Propeller. - Google Patents

Propeller. Download PDF

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Publication number
US1036834A
US1036834A US64805111A US1911648051A US1036834A US 1036834 A US1036834 A US 1036834A US 64805111 A US64805111 A US 64805111A US 1911648051 A US1911648051 A US 1911648051A US 1036834 A US1036834 A US 1036834A
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Prior art keywords
arm
blades
shaft
propeller
secured
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Expired - Lifetime
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US64805111A
Inventor
Charles R Haas
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Individual
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Priority to US64805111A priority Critical patent/US1036834A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30Blade pitch-changing mechanisms
    • B64C11/32Blade pitch-changing mechanisms mechanical
    • B64C11/34Blade pitch-changing mechanisms mechanical automatic
    • B64C11/343Blade pitch-changing mechanisms mechanical automatic actuated by the centrifugal force or the aerodynamic drag acting on the blades

Definitions

  • My invention relates to propellers
  • l0 more particularly to propellers to be usedin connectlon with air-ships, and has for its object to provide one with an arm to which the blades are pivoted, resilient means be ing provided for holding the blades in a predetermined position relatively to the arm.
  • FIG. 1 is a side elevation .of the propeller, showing its position when in motion
  • Fig. 2 is an end View of the propeller, showing the position of the blades when in motion
  • Fig. 3 is va side elevation showing the position of the blades when the propelleris' at rest.
  • a shaft 5 is provided to which is 5 secured a radially disposed arm 6 extendlng 1n opposite directions from said shaft.
  • Two resilient blades 7 are provided, the blades being preferably rectangular in shape, as shown in Fig. 3 of the drawings.
  • Each of these blades 7 has a plurality of sleeves 8 spaced apart, the arm 6 being disf posed in the said sleeves.
  • brace members 13 are secured to the shaft 5, these brace members extending outwardly andbeing secured to the outer ends of the arm 6. Wing nuts 1l engage the threaded terminals 15 of the shaft 5, for preventing the blades 7 from slipping therefrom.
  • the blades 7 are radially .disposed with their flat faces lying substantially in the same plane, one at each side of the shaft 5. I/Vhen the propeller is rotated, the springs 9 permit the blades to' bend, but as the inner ends of the blades are secured by the tie members 11, the inner ends of the blades are permitted very little movement relatively to the arm '6, although the ends of the blades at a distance from the shaft 5 are permitted to move a relatively considerable distance. .
  • the brace members 13 act as a check for the blades and limit their movement by the springs 9..
  • a shaft a radially disresilient ⁇ means for moving the blade in one direction blade mounted torotate on the arm, a tie member connecting the blade at a distance from the arm with the shaft, and a brace member. connecting the arm lwith the shaft and adapted to check the movementof the blade.
  • a shaft In a propeller, a shaft, a radially-disposed arm secured to the shaft, a blade mounted ⁇ to rotate on the arm, a tie memto the shaft, a blade ber connecting the blade at a. distance from name to this specification in the presence of lheledarm ilwlitl) the shaft, resilient means for two subscribing Witnesses.

Description

C. R. HAAS.
PROPELLER.
APPLIGATION rILBn s112127, 1911.
N. l M
AHORA/EVS Patented Aug. 27, i912- By l CHARLESR. HAAS, BRIGHTWATER, BRITISH COLUMBIA, CANADA.
PROPELLER.
Specieationof Letters Patent.
Patented Aug. er, 191e.
Application led September 7, 1911. Serial No. 648,051.
ATo all whom t may concern.'
Be 1t known that I, CHARLES R. HAA'S, a subject of the King of Great Britain, and 'a resident of Brightwater, in the Province of 5 British Columbia, Dominion of Canada,
have invented a new and Improved Propeller, of which the following'is a full, clear, and exactdescription.
My invention relates to propellers, and
l0 more particularly to propellers to be usedin connectlon with air-ships, and has for its object to provide one with an arm to which the blades are pivoted, resilient means be ing provided for holding the blades in a predetermined position relatively to the arm.
Additional objects of the invention areset forth in the following specification, in which the preferred form of my invention is described.
Reference is to be had to the accompanying drawings forming' a part of this speciication, in which similar characters of reference indicate corresponding parts'in all `theligures, and in which-w 1 Figure 1 is a side elevation .of the propeller, showing its position when in motion; Fig. 2 is an end View of the propeller, showing the position of the blades when in motion; and Fig. 3 is va side elevation showing the position of the blades when the propelleris' at rest.
By referring to the drawings, it will be seen that a shaft 5 is provided to which is 5 secured a radially disposed arm 6 extendlng 1n opposite directions from said shaft. Two resilient blades 7 are provided, the blades being preferably rectangular in shape, as shown in Fig. 3 of the drawings.
40 Each of these blades 7 has a plurality of sleeves 8 spaced apart, the arm 6 being disf posed in the said sleeves. On the arm 6 y between the sleeves 8 there are disposed rlcoiled springs 9, one tcrminalof each of these 4coiled springs being secured tothe arm 6, the other terminals extending outwardly from the arm' 6 and being secured to the blades at 10 at a distance from the arm 6. To the inner side of the blades, at a distance4 from the arm 6, are secured tie niembers 11, thel other ends ofthese' tie members 1l being secured to thehub 12 mounted on the shaft 5 to which the arm 6 is also secured. Some distance from the hub 12 brace members 13 are secured to the shaft 5, these brace members extending outwardly andbeing secured to the outer ends of the arm 6. Wing nuts 1l engage the threaded terminals 15 of the shaft 5, for preventing the blades 7 from slipping therefrom. When the propeller is not in use, the blades 7 are radially .disposed with their flat faces lying substantially in the same plane, one at each side of the shaft 5. I/Vhen the propeller is rotated, the springs 9 permit the blades to' bend, but as the inner ends of the blades are secured by the tie members 11, the inner ends of the blades are permitted very little movement relatively to the arm '6, although the ends of the blades at a distance from the shaft 5 are permitted to move a relatively considerable distance. .The brace members 13 act as a check for the blades and limit their movement by the springs 9..
Having thus described my invent-ion, I claim as new and desire to secure by Letters Patent 1. lIn a propeller, posed arm secured mounted to rotate on the arm,
a shaft, a radially disresilient `means for moving the blade in one direction blade mounted torotate on the arm, a tie member connecting the blade at a distance from the arm with the shaft, and a brace member. connecting the arm lwith the shaft and adapted to check the movementof the blade.
4. In a propeller, a shaft, a radially-disposed arm secured to the shaft, a blade mounted `to rotate on the arm, a tie memto the shaft, a blade ber connecting the blade at a. distance from name to this specification in the presence of lheledarm ilwlitl) the shaft, resilient means for two subscribing Witnesses.
o ing t e ladein a. predetermined osition relatively to the arm, and a brace Iem- CHARLES R' HAAb' 5 ber connecting the arm with the shaft and Witnesses:
adapted to check the movement of the blade. G. WHITEHEAD,
-In testimony whereof I have signed my JOHN KIRKPATRICK.
US64805111A 1911-09-07 1911-09-07 Propeller. Expired - Lifetime US1036834A (en)

Priority Applications (1)

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US64805111A US1036834A (en) 1911-09-07 1911-09-07 Propeller.

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US64805111A US1036834A (en) 1911-09-07 1911-09-07 Propeller.

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US1036834A true US1036834A (en) 1912-08-27

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US64805111A Expired - Lifetime US1036834A (en) 1911-09-07 1911-09-07 Propeller.

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2974731A (en) * 1958-06-02 1961-03-14 John Spargo Combined impeller and closure

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2974731A (en) * 1958-06-02 1961-03-14 John Spargo Combined impeller and closure

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