NI200700288A - ADJUSTMENT DEVICE TO ADJUST PROPULSING ASPES OF A PUMP PUMP, AND A PUMP THAT INCLUDES THE DEVICE. - Google Patents

ADJUSTMENT DEVICE TO ADJUST PROPULSING ASPES OF A PUMP PUMP, AND A PUMP THAT INCLUDES THE DEVICE.

Info

Publication number
NI200700288A
NI200700288A NI200700288A NI200700288A NI200700288A NI 200700288 A NI200700288 A NI 200700288A NI 200700288 A NI200700288 A NI 200700288A NI 200700288 A NI200700288 A NI 200700288A NI 200700288 A NI200700288 A NI 200700288A
Authority
NI
Nicaragua
Prior art keywords
pump
fixing means
adjustment
adjustment device
aspes
Prior art date
Application number
NI200700288A
Other languages
Spanish (es)
Inventor
Roland Svensson
Original Assignee
Itt Mfg Enterprises Inc
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 Itt Mfg Enterprises Inc filed Critical Itt Mfg Enterprises Inc
Publication of NI200700288A publication Critical patent/NI200700288A/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D15/00Control, e.g. regulation, of pumps, pumping installations or systems
    • F04D15/0055Rotors with adjustable blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Details And Applications Of Rotary Liquid Pumps (AREA)
  • Rotary Pumps (AREA)

Abstract

La presente invención se refiere a un dispositivo de ajuste para ajustar el ángulo del grado inclinación de las aspas propulsoras (4) de una bomba impulsora (1), y una bomba impulsora que incorpora este dispositivo. El dispositivo de ajuste comprende medios de ajuste (5;25;35) montados dentro del disco central (2) dispuesto para ser axialmente móvil en una dirección a lo largo del eje impulsor (7), estando los medios de ajuste (5;25;35) provistos con una pluralidad de ranuras de guiado (6;26a;26b;36) dispuestas con separaciones circunferenciales alrededor de la superficie; una pluralidad de medios de fijación (20) montados, a través de la rotación, en el disco central (2), estando cada uno de ellos acoplado de manera fija a una aspa propulsora (4) y soportado por al menos una ranura de guiado (6;26a;26b;36), en el que cada medio de fijación (20) y la correspondiente por lo menos una ranura de guiado (6;26a;26b;36) está dispuesta de manera que interactúa de manera tal que una fuerza aplicada sobre el medio de fijación (20) se distribuye simétricamente alrededor de un eje perpendicular al eje impulsor (7) y paralelo a un eje rotacional del medio de fijación (20); y en la que las ranuras de guiado (6;26a;26b;36) están dispuestas de manera tal que, al tener lugar un movimiento axial de los medios de ajuste (5;25;35), ocasionan que el medio de fijación (5;25;35) rote alrededor de su propio eje rotacional, con lo cual a su vez se hace rotar el aspa propulsora (4).The present invention relates to an adjustment device for adjusting the angle of the inclination degree of the propeller blades (4) of a driving pump (1), and a driving pump incorporating this device. The adjustment device comprises adjustment means (5; 25; 35) mounted within the central disk (2) arranged to be axially movable in a direction along the drive shaft (7), the adjustment means (5; 25 being) ; 35) provided with a plurality of guide grooves (6; 26a; 26b; 36) arranged with circumferential separations around the surface; a plurality of fixing means (20) mounted, through rotation, on the central disk (2), each of them being fixedly coupled to a propeller blade (4) and supported by at least one guide groove (6; 26a; 26b; 36), in which each fixing means (20) and the corresponding at least one guiding groove (6; 26a; 26b; 36) is arranged so that it interacts such that a force applied on the fixing means (20) is distributed symmetrically around an axis perpendicular to the driving shaft (7) and parallel to a rotational axis of the fixing means (20); and in which the guide grooves (6; 26a; 26b; 36) are arranged such that, when an axial movement of the adjustment means (5; 25; 35) takes place, they cause the fixing means ( 5; 25; 35) rotate around its own rotational axis, which in turn rotates the propeller blade (4).

NI200700288A 2005-06-22 2007-11-09 ADJUSTMENT DEVICE TO ADJUST PROPULSING ASPES OF A PUMP PUMP, AND A PUMP THAT INCLUDES THE DEVICE. NI200700288A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US69301805P 2005-06-22 2005-06-22

Publications (1)

Publication Number Publication Date
NI200700288A true NI200700288A (en) 2008-06-25

Family

ID=36809599

Family Applications (1)

Application Number Title Priority Date Filing Date
NI200700288A NI200700288A (en) 2005-06-22 2007-11-09 ADJUSTMENT DEVICE TO ADJUST PROPULSING ASPES OF A PUMP PUMP, AND A PUMP THAT INCLUDES THE DEVICE.

Country Status (9)

Country Link
US (1) US20080199318A1 (en)
EP (1) EP1893873A1 (en)
CN (1) CN101228356B (en)
AR (1) AR054490A1 (en)
BR (1) BRPI0612494A2 (en)
MX (1) MX2007013538A (en)
NI (1) NI200700288A (en)
RU (1) RU2008102237A (en)
WO (1) WO2006137765A1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3005096B1 (en) * 2013-04-29 2018-01-19 Safran Aircraft Engines SYSTEM FOR CONTROLLING THE PITCH OF THE BLADES OF A TURBOMACHINE PROPELLER AND A PROPELLER TURBOMACHINE FOR AN AIRCRAFT WITH SUCH A SYSTEM
CN105508286B (en) * 2015-12-14 2018-02-06 江苏省水利勘测设计研究院有限公司 A kind of blade enters the reflexibie axial flow pump in waterside
CN110127038A (en) * 2019-05-27 2019-08-16 安徽卓尔航空科技有限公司 A kind of propeller hub of adjustable-piston
CN114593067B (en) * 2022-03-23 2023-06-23 扬州弘跃机械有限公司 High-sealing axial flow pump

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1650776A (en) * 1927-11-29 stock
US1008953A (en) * 1905-06-29 1911-11-14 Frank Clennell Ship's propeller.
US1456699A (en) * 1921-09-02 1923-05-29 Kramer Rudolph Air-circulating system
US1891384A (en) * 1930-08-04 1932-12-20 Joseph R Gillis Aircraft propeller
US2357229A (en) * 1941-03-07 1944-08-29 English Electric Co Ltd Operating gear for adjustable propeller blades
US2786539A (en) * 1948-11-26 1957-03-26 Harry J Nichols Controllable-pitch propeller system
US2699221A (en) * 1950-04-19 1955-01-11 Harry J Nichols Controllable reversible pitch marine propeller system
US3092186A (en) * 1962-01-04 1963-06-04 James K Maclean Variable pitch propeller mechanism
US3219121A (en) * 1962-08-03 1965-11-23 John W Barden Controllable pitch propeller hydraulic locking device
US3262502A (en) * 1964-05-28 1966-07-26 Harry J Nichols Manual controllable pitch propeller systems for motorboats
US3295610A (en) * 1965-10-24 1967-01-03 Frias Robert Automatic propeller pitch control and adaptor
NO120011B (en) * 1967-03-22 1970-08-10 Karlstad Mekaniska Ab
US3645644A (en) * 1970-01-22 1972-02-29 Hydro Drive Corp Interlocking variable-pitch propeller assembly
US3676016A (en) * 1970-09-21 1972-07-11 Arne Feroy Controllable pitch propellers
FR2153621A5 (en) * 1971-09-17 1973-05-04 Bretagne Atel Chantiers
JPS57182599A (en) * 1981-04-30 1982-11-10 Kogyo Gijutsuin Variable pitch mechanism of rotor
DE3318163C2 (en) * 1983-05-19 1986-05-07 M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 8500 Nürnberg Adjustment device for blades of a vertically arranged fluid flow machine
US4810166A (en) * 1987-08-03 1989-03-07 Bird-Johnson Company Controllable pitch marine propeller
US5145318A (en) * 1989-11-16 1992-09-08 Bird-Johnson Company Flange-mounted controllable pitch marine propeller
NL9201889A (en) * 1992-10-29 1994-05-16 Klaas Langenberg Adjustable screw.

Also Published As

Publication number Publication date
CN101228356B (en) 2012-01-04
AR054490A1 (en) 2007-06-27
MX2007013538A (en) 2008-01-16
RU2008102237A (en) 2009-07-27
US20080199318A1 (en) 2008-08-21
CN101228356A (en) 2008-07-23
EP1893873A1 (en) 2008-03-05
WO2006137765A1 (en) 2006-12-28
BRPI0612494A2 (en) 2012-01-03

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