US1979616A - Propeller control - Google Patents

Propeller control Download PDF

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Publication number
US1979616A
US1979616A US722983A US72298334A US1979616A US 1979616 A US1979616 A US 1979616A US 722983 A US722983 A US 722983A US 72298334 A US72298334 A US 72298334A US 1979616 A US1979616 A US 1979616A
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United States
Prior art keywords
propeller
casing
tubes
barrel
propeller control
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Expired - Lifetime
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US722983A
Inventor
Haidle Fred
Haidle Balthaser
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Individual
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Individual
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Priority to US722983A priority Critical patent/US1979616A/en
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Publication of US1979616A publication Critical patent/US1979616A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D7/00Controlling wind motors 
    • F03D7/02Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/022Adjusting aerodynamic properties of the blades
    • F03D7/0224Adjusting blade pitch
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/70Adjusting of angle of incidence or attack of rotating blades
    • F05B2260/74Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/70Adjusting of angle of incidence or attack of rotating blades
    • F05B2260/75Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism not using auxiliary power sources, e.g. servos
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/70Adjusting of angle of incidence or attack of rotating blades
    • F05B2260/77Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism driven or triggered by centrifugal forces
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

Definitions

  • This'invention appertains to new and useful improvements in propellers particularly adapted for wind electric plants, the principal object being to provide a propeller which automatically serves to keep the generator driven at a steady rate of speed in any wind velocity.
  • Another important object of the present invention is to provide a propeller for wind driven electric plants, wherein the propeller will automatically adjust itself under varying wind conditions so as to act in itself automatically as a governor for the generator which is drives.
  • Figure 1 represents a fragmentary front elevational view of the novel propeller.
  • Figure 2 represents a sectional view taken substantially on line 2-2 of Figure 1, fragmentarily showing the propeller blades.
  • Figure 3 represents an enlarged fragmentary vertical sectional view through the hub portion of the propeller.
  • Figure 4 represents a sectional view taken substantially on line 4-4 of Figure 3.
  • the propeller consists of the well casing 5 having the barrel fi'extending therethrough for the drive shaft 7.
  • the plate 5 has a hub 5 and is rotatable on the barrel 6.
  • Each of the tubes 8 is provided with a spirally disposed slot 10 through which extends a pintle 11. However, as shown in Figure 3, there may be two of these slots for each of the tubes to accommodate two pintles 11.
  • a coiled compressible spring 12 is located on each of the tubes 8 and is interposed between the corresponding pintles 11 and the corresponding adjusting nuts 9. These conditions, the springs 12 will maintain the shanks 13 in retracted position with the pintles 11 at the innermost ends of the slots 10.
  • a propeller comprising a casing open at its front side, a barrel extending through the casing a closureplate at the front of the casing rotatably mounted on the barrel, a drive shaft extending into the barrel and being keyed thereto, tubes radiating from the barrel in the casing and being provided at their outer ends with adjusting nuts, said tubes being provided with spiral grooveways, propeller blades having shanks disposed into the casing and into the said tubes, each of the said shanks being provided with a pintle disposed into the corresponding tube grooveway, a coiled compressible springon each of the tubes interposed between the corresponding adjusting nut and the corresponding propeller shank pin, and pivotal tie rods between the propeller and the rotatable closure plate whereby the blades will adjust themselves in unison.
  • pintles 11 project laterally from the shank 13 of each of the propellers 14.
  • Each of the propellers 14 has a stub 15 projecting laterally and forwardly thereof and provided with a ball 16 at its end for disposition into the socket end 17 of an arm 18.
  • Each of these arms 18 is pivotally connected to the removable front.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wind Motors (AREA)

Description

Nov. 6, 1934. F. HAlDLE ET AL 1,979,516
PROPELLER CONTROL Filed April 28, 1934 2 Sheets-Sheet 1 f l /7 8 i Y'QQ/ ea die F I I I Z?Z2%a5w' 14 01 476 Inventors Home y Nov. 6, 1934. F. HAIDLE ET AL 1,979,616
PROPELLEB CONTROL Filed April 28, 1934 2 Sheets-Sheet 2 Inventors Patented Nov. 6, 1934 UNITED STATES PATENT OFFICE 1 Claim.
This'invention appertains to new and useful improvements in propellers particularly adapted for wind electric plants, the principal object being to provide a propeller which automatically serves to keep the generator driven at a steady rate of speed in any wind velocity.
Another important object of the present invention is to provide a propeller for wind driven electric plants, wherein the propeller will automatically adjust itself under varying wind conditions so as to act in itself automatically as a governor for the generator which is drives.
Other important objects and advantages of the invention will become apparent to the reader of the following specification.
In the drawings:
Figure 1 represents a fragmentary front elevational view of the novel propeller.
Figure 2 represents a sectional view taken substantially on line 2-2 of Figure 1, fragmentarily showing the propeller blades.
Figure 3 represents an enlarged fragmentary vertical sectional view through the hub portion of the propeller.
Figure 4 represents a sectional view taken substantially on line 4-4 of Figure 3.
Referring to the drawings wherein like numerals designate like parts, it can be seen that the propeller consists of the well casing 5 having the barrel fi'extending therethrough for the drive shaft 7.
Radiating from the barrel 6 are the tubes 8.
which meet the peripheral wall of the casing 5 and are threaded adjacent the outer ends to accommodate nuts 9 which can be adjusted thereon by removing the front plate 5 v of the casing 5. The plate 5 has a hub 5 and is rotatable on the barrel 6.
Each of the tubes 8 is provided with a spirally disposed slot 10 through which extends a pintle 11. However, as shown in Figure 3, there may be two of these slots for each of the tubes to accommodate two pintles 11. A coiled compressible spring 12 is located on each of the tubes 8 and is interposed between the corresponding pintles 11 and the corresponding adjusting nuts 9. These conditions, the springs 12 will maintain the shanks 13 in retracted position with the pintles 11 at the innermost ends of the slots 10. When the propeller simply begins to rotate at an excessive speed, centrifugal force pulls outwardly on the propeller and consequently on the shanks l3 and as the shanks move outwardly, the pins 11, in riding in the slots 10, cause the partial rotation of the propellers so as to bring the propellers into anon-resisting position with respect to the wind. This continual centrifugal action causes an average speed safe for the generator being driven.
While the foregoing specification sets forth the invention in specific terms, it is to be understood that numerous changes in the shape, vsize and materials may be resorted to without departing from the spirit and scope of the invention as claimed hereinafter.
Having described the invention, what is claimed as new is A propeller comprising a casing open at its front side, a barrel extending through the casing a closureplate at the front of the casing rotatably mounted on the barrel, a drive shaft extending into the barrel and being keyed thereto, tubes radiating from the barrel in the casing and being provided at their outer ends with adjusting nuts, said tubes being provided with spiral grooveways, propeller blades having shanks disposed into the casing and into the said tubes, each of the said shanks being provided with a pintle disposed into the corresponding tube grooveway, a coiled compressible springon each of the tubes interposed between the corresponding adjusting nut and the corresponding propeller shank pin, and pivotal tie rods between the propeller and the rotatable closure plate whereby the blades will adjust themselves in unison.
FRED HAIDLE.
BALTHASER 'HAIDLE.
pintles 11 project laterally from the shank 13 of each of the propellers 14.
Each of the propellers 14 has a stub 15 projecting laterally and forwardly thereof and provided with a ball 16 at its end for disposition into the socket end 17 of an arm 18. Each of these arms 18 is pivotally connected to the removable front.
wall 5 of the casing 5, as at 19 (see Figure 1).
It can now be seen that under ordinary working
US722983A 1934-04-28 1934-04-28 Propeller control Expired - Lifetime US1979616A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US722983A US1979616A (en) 1934-04-28 1934-04-28 Propeller control

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Application Number Priority Date Filing Date Title
US722983A US1979616A (en) 1934-04-28 1934-04-28 Propeller control

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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2416541A (en) * 1943-08-30 1947-02-25 Olman Peter Michael Variable pitch propeller
US2492653A (en) * 1946-04-11 1949-12-27 Bendix Aviat Corp Air propeller
US2495523A (en) * 1945-01-20 1950-01-24 Russell R Hays Sustaining rotor for aircraft
US2818124A (en) * 1955-06-06 1957-12-31 John G Johnston Helicopter blade mounting mechanism
WO1984004362A1 (en) * 1983-04-27 1984-11-08 Gyula Vari Wind driven power source
US4909703A (en) * 1988-12-02 1990-03-20 Jacobs Paul R Motion damping apparatus for wind driven propellers
NL9001636A (en) * 1990-07-18 1992-02-17 Aerpac Holding B V Aerodynamic speed control for wind turbine - has automatic adjustment of pitch of blade tips
WO2004088131A1 (en) * 2003-04-01 2004-10-14 Energie Pge Inc. Self-regulating wind turbine
US20050285406A1 (en) * 2002-06-04 2005-12-29 Dawson Mark H Telescoping wind turbine blade
US20180065730A1 (en) * 2015-05-12 2018-03-08 Safran Aircraft Engines A radial shaft device for controlling the pitch of fan blades of a turbine engine having an un-ducted fan

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2416541A (en) * 1943-08-30 1947-02-25 Olman Peter Michael Variable pitch propeller
US2495523A (en) * 1945-01-20 1950-01-24 Russell R Hays Sustaining rotor for aircraft
US2492653A (en) * 1946-04-11 1949-12-27 Bendix Aviat Corp Air propeller
US2818124A (en) * 1955-06-06 1957-12-31 John G Johnston Helicopter blade mounting mechanism
WO1984004362A1 (en) * 1983-04-27 1984-11-08 Gyula Vari Wind driven power source
US4909703A (en) * 1988-12-02 1990-03-20 Jacobs Paul R Motion damping apparatus for wind driven propellers
NL9001636A (en) * 1990-07-18 1992-02-17 Aerpac Holding B V Aerodynamic speed control for wind turbine - has automatic adjustment of pitch of blade tips
US20050285406A1 (en) * 2002-06-04 2005-12-29 Dawson Mark H Telescoping wind turbine blade
US7632070B2 (en) 2002-06-04 2009-12-15 Dawson Mark H Telescoping wind turbine blade
WO2004088131A1 (en) * 2003-04-01 2004-10-14 Energie Pge Inc. Self-regulating wind turbine
US20180065730A1 (en) * 2015-05-12 2018-03-08 Safran Aircraft Engines A radial shaft device for controlling the pitch of fan blades of a turbine engine having an un-ducted fan
US11225317B2 (en) * 2015-05-12 2022-01-18 Safran Aircraft Engines Radial shaft device for controlling the pitch of fan blades of a turbine engine having an un-ducted fan

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