WO2002055887A1 - Entrainement a commande pneumatique, moteur a jet (variantes) et appareil de commande electropneumatique - Google Patents

Entrainement a commande pneumatique, moteur a jet (variantes) et appareil de commande electropneumatique Download PDF

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Publication number
WO2002055887A1
WO2002055887A1 PCT/RU2001/000499 RU0100499W WO02055887A1 WO 2002055887 A1 WO2002055887 A1 WO 2002055887A1 RU 0100499 W RU0100499 W RU 0100499W WO 02055887 A1 WO02055887 A1 WO 02055887A1
Authority
WO
WIPO (PCT)
Prior art keywords
shaft
chτο
pneumatic
gear
πρivοda
Prior art date
Application number
PCT/RU2001/000499
Other languages
English (en)
Russian (ru)
Inventor
Vadim Vasilievich Sayapin
Original Assignee
Vadim Vasilievich Sayapin
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 Vadim Vasilievich Sayapin filed Critical Vadim Vasilievich Sayapin
Priority to EP01273216A priority Critical patent/EP1350959A1/fr
Publication of WO2002055887A1 publication Critical patent/WO2002055887A1/fr

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B9/00—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member
    • F15B9/02—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type
    • F15B9/08—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type controlled by valves affecting the fluid feed or the fluid outlet of the servomotor
    • F15B9/09—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type controlled by valves affecting the fluid feed or the fluid outlet of the servomotor with electrical control means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/30—Non-positive-displacement machines or engines, e.g. steam turbines characterised by having a single rotor operable in either direction of rotation, e.g. by reversing of blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/32—Non-positive-displacement machines or engines, e.g. steam turbines with pressure velocity transformation exclusively in rotor, e.g. the rotor rotating under the influence of jets issuing from the rotor, e.g. Heron turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B9/00—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member
    • F15B9/14—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with rotary servomotors

Definitions

  • E ⁇ a ⁇ e ⁇ niches ⁇ aya task ⁇ eshae ⁇ sya on account ⁇ g ⁇ , ch ⁇ ⁇ us ⁇ v ⁇ n ⁇ g ⁇ me ⁇ anizma vy ⁇ lnen as tsen ⁇ aln ⁇ g ⁇ ⁇ ela two ⁇ ysh ⁇ ami, ⁇ i e ⁇ m in ⁇ use vy ⁇ lnen s ⁇ v ⁇ zn ⁇ y na ⁇ avlyayuschy ⁇ az 0 ⁇ yam ⁇ ug ⁇ ln ⁇ g ⁇ section in ⁇ m ⁇ azmeschen ⁇ v ⁇ d ⁇ with ⁇ d ⁇ v ⁇ y gay ⁇ y, s ⁇ edinenn ⁇ y ⁇ ezb ⁇ y with ⁇ d ⁇ vym vin ⁇ m, s ⁇ edinennym with us ⁇ ys ⁇ v ⁇ m
  • the absorptions of the kinetic energy of the mobile device are equipped with the device for the protection of the consumer.
  • the essence of the invention is included in the case, in that a separate channel is connected to the pneumatic switch, while the gas is disconnected from the source, and the gas is disconnected from the source.
  • the outlet of the outlet is connected to the source of the pressure medium, and the outlet is disconnected from the medium.
  • Improvement of operational performance of the device is achieved 0 due to the exclusion of the secondary working body and facilitation of the process of regulating the end switches.
  • ⁇ a ⁇ ig. 1 pneumatic flow diagram is illustrated. 5 ⁇ a ⁇ ig. 2 is cut off when the engine is turned on. ⁇ a ⁇ ig. 3 shows a side view of a rotational engine with four nozzles and interchangeable squirrel blocks.
  • ⁇ a ⁇ ig. 4 is cut off through a rotary engine, made in the form of a central hub connected to two shoulders and with nozzles pointing to the same side.
  • ⁇ a ⁇ ig. 5 shows a side view of a drive of a jet engine with nozzles pointing to one side.
  • ⁇ a ⁇ ig. 6 shows a view of the top of the rocker-screw mechanism.
  • ⁇ a ⁇ ig. 7 is shown at a glance in FIG. 6 of the new mechanism.
  • ⁇ a ⁇ ig. 8 It is shown after switching on the power transmission of the pneumatic control device in FIG. 9 The view is shown in the graph.
  • Fig. 8. ⁇ a ⁇ ig. 10 Delivered through a pneumatic distributor of an electrical control device.
  • inlet ducts 8, 9 of the motor 10, rotational drive 11 (Fig. 2 - 5) connects the channel channels 13, 14 connected by slanted and radial channels with the ramps of 15, 16, 11, 16 .
  • zubcha ⁇ g ⁇ ring 20 associated with ⁇ edu ⁇ m 21 ⁇ y 5 s ⁇ de ⁇ zhi ⁇ ⁇ uchn ⁇ y duble ⁇ 22 me ⁇ anizm ⁇ m 23 av ⁇ ma ⁇ iches ⁇ g ⁇ ⁇ lyucheniya sh ⁇ u ⁇ vala 24.
  • P ⁇ v ⁇ ny me ⁇ anizm ( ⁇ ig. 6, 7) s ⁇ de ⁇ zhi ⁇ ⁇ a ⁇ zhe ⁇ v ⁇ d ⁇ 31 5 ⁇ d ⁇ v ⁇ y gay ⁇ y 32 s ⁇ de ⁇ zhaschy two tsa ⁇ y 33, 34, ⁇ ye with ⁇ m ⁇ schyu ⁇ lzun ⁇ v 35, 36 ⁇ azmescheny in ⁇ aza ⁇ ⁇ ulisy 37 s ⁇ edinenn ⁇ y zhes ⁇ with vy ⁇ dnym val ⁇ m 38 ⁇ iv ⁇ da and further with ⁇ be ⁇ m Decisions 39.
  • ⁇ y ⁇ dn ⁇ y shaft 38 ⁇ iv ⁇ da s ⁇ edinen with v ⁇ dnym vali ⁇ m 41 ele ⁇ nevma ⁇ iches ⁇ g ⁇ us ⁇ ys ⁇ va 1 ( ⁇ ig. 8, 9), ⁇ dyaschim che ⁇ ez ⁇ ysh ⁇ u 42 vz ⁇ yv ⁇ zaschischenn ⁇ y ⁇ ame ⁇ y 43 in ⁇ y ⁇ azmescheny ge ⁇ ny 44, 45.
  • the rotor 11 of engine 10 (Fig. 2, 3) consists of units 55, 56 with executed units 15, 16, 17, 18 mounted on the shoulders of unit 11. eleven
  • the 11th engine 10 connects the central hub 57 and the shoulders 58, 59 connected to it with the 15 arms pointing to the same side.
  • Pneumatic divider 4, 5 (Fig. 10) consists of 61, 5 servo valves 62, 63 valves, 64 valves, 65 levers 66, 67 output channels, 69 output channels
  • ⁇ a ⁇ ig. 1 and 10 also mean the inlet pressure is higher., The outlet pressure is higher. and the inlet pressure of Hex. 1 in the downstream channel of the valve. 10 Pnevm ⁇ me ⁇ aniches ⁇ e us ⁇ ys ⁇ v ⁇ s ⁇ eniya ⁇ iv ⁇ da s ⁇ de ⁇ zhi ⁇ ⁇ nevm ⁇ nilind ⁇ 71, 72 ⁇ shen s ⁇ sh ⁇ m 73 ⁇ d ⁇ uzhinennym ⁇ uzhin ⁇ y 74 and associated ⁇ u ⁇ ya ⁇ y 75.
  • the pneumatic device, the jet engine and the electric pneumatic control unit operate together with the following device.
  • Drive 11 is driven through gear ring 20 5 and then through gear 21 to gear 26 and through gear slotted to gear screw 27.
  • the loose nut 32 is turned off, and the loose screw 27 is rotated and screwed into the nut 32, while not being moved away from it, even if it is 30 thirteen
  • P ⁇ myshlennaya ⁇ imenim ⁇ s ⁇ ⁇ e ⁇ e ⁇ iches ⁇ ie ⁇ asche ⁇ y and b ⁇ ly ⁇ y ⁇ bem e ⁇ s ⁇ e ⁇ imen ⁇ alny ⁇ issled ⁇ vany and is ⁇ y ⁇ any nes ⁇ l ⁇ i ⁇ ⁇ i ⁇ azme ⁇ v and m ⁇ di ⁇ i ⁇ atsy ⁇ iv ⁇ d ⁇ v, ⁇ vedenny ⁇ on e ⁇ s ⁇ e ⁇ imen ⁇ alny ⁇ ⁇ lig ⁇ na ⁇ and usl ⁇ viya ⁇ ⁇ d ⁇ n ⁇ ln ⁇ y e ⁇ s ⁇ lua ⁇ atsii in ⁇ azlichny ⁇ ⁇ egi ⁇ na ⁇ ⁇ ssii ⁇ echenie in 1987 - 2000 years. CONFIRMED PRODUCTIVITY AND EFFICIENCY OF OFFERED COMPONENTIAL CIRCUIT AND PARAMETER SOLUTIONS.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Crystals, And After-Treatments Of Crystals (AREA)
  • Transmission Devices (AREA)
  • Actuator (AREA)

Abstract

La présente invention peut être utilisée pour commander à distance les vannes de gazoducs, d'oléoducs et de conduites de transport pour produits pétroliers et gaziers. Selon l'invention, l'entraînement à commande pneumatique comprend un dispositif de commande électropneumatique (1) doté d'électro-aimants (2, 3), de distributeurs pneumatiques (4, 5) et de régulateurs du débit de gaz (6, 7) reliés aux tubes d'admission (8, 9) du moteur à jet (10). Le rotor (11) du moteur à jet comporte des canaux axiaux (13, 14) reliés aux buses (15). L'arbre du rotor (19) est relié par une couronne dentée (20) à l'engrenage réducteur (21), qui comprend un dispositif de réserve manuel (22) doté d'un mécanisme (23) de déconnexion mécanique du volant de commande (24). La roue dentée (26) est montée sur l'arbre avec la vis-mère (27) du mécanisme de direction à vis coulissante (28). L'entraînement comprend l'appareil (29) d'absorption de l'énergie cinétique des pièces mobiles de l'engrenage qui est muni d'un ressort à rondelles coniques (30). Le mécanisme de direction (28) comprend un écrou coulissant (32) muni de deux tourillons (33) qui sont disposés dans les encoches de la coulisse (37) raccordée à l'arbre de sortie de l'entraînement (38) puis à l'objet commandé (39). L'arbre (38) est relié au cylindre d'entrée (41) du dispositif (1), et des commutateurs à lames (44, 45) avec aimants constants (52, 53) sont disposés à l'intérieur dudit arbre (38).
PCT/RU2001/000499 2001-01-09 2001-11-22 Entrainement a commande pneumatique, moteur a jet (variantes) et appareil de commande electropneumatique WO2002055887A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP01273216A EP1350959A1 (fr) 2001-01-09 2001-11-22 Entrainement a commande pneumatique, moteur a jet (variantes) et appareil de commande electropneumatique

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU2001100316 2001-01-09
RU2001100316A RU2178842C1 (ru) 2001-01-09 2001-01-09 Пневматический привод, струйный двигатель (варианты) и электропневматическое управляющее устройство

Publications (1)

Publication Number Publication Date
WO2002055887A1 true WO2002055887A1 (fr) 2002-07-18

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU2001/000499 WO2002055887A1 (fr) 2001-01-09 2001-11-22 Entrainement a commande pneumatique, moteur a jet (variantes) et appareil de commande electropneumatique

Country Status (3)

Country Link
EP (1) EP1350959A1 (fr)
RU (1) RU2178842C1 (fr)
WO (1) WO2002055887A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1431587A2 (fr) * 2002-12-19 2004-06-23 Kay Fischer Dispositif d'actionnement pour une soupape

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3907289A1 (de) * 1989-03-07 1990-09-13 Siemens Ag Stellantrieb fuer sicherheitsventile
RU2050478C1 (ru) * 1994-11-29 1995-12-20 Вадим Васильевич Саяпин Пневматический привод
RU2064606C1 (ru) * 1995-03-28 1996-07-27 Вадим Васильевич Саяпин Пневматический следящий привод и струйный двигатель
RU2131065C1 (ru) * 1998-03-17 1999-05-27 Саяпин Вадим Васильевич Пневматический привод саяпина и электропневматическое управляющее устройство
RU2159362C1 (ru) * 1999-05-05 2000-11-20 Саяпин Вадим Васильевич Многооборотный пневматический привод, струйный двигатель, устройство поглощения кинетической энергии подвижных частей (варианты)

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3907289A1 (de) * 1989-03-07 1990-09-13 Siemens Ag Stellantrieb fuer sicherheitsventile
RU2050478C1 (ru) * 1994-11-29 1995-12-20 Вадим Васильевич Саяпин Пневматический привод
RU2064606C1 (ru) * 1995-03-28 1996-07-27 Вадим Васильевич Саяпин Пневматический следящий привод и струйный двигатель
RU2131065C1 (ru) * 1998-03-17 1999-05-27 Саяпин Вадим Васильевич Пневматический привод саяпина и электропневматическое управляющее устройство
RU2159362C1 (ru) * 1999-05-05 2000-11-20 Саяпин Вадим Васильевич Многооборотный пневматический привод, струйный двигатель, устройство поглощения кинетической энергии подвижных частей (варианты)

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
D.F. GUREVICH ET AL.: "Spravochnik po armature dlya gazo- I nefteprovodov", NEDRA, 1988, LENINGRAD, pages 346, 348, 408 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1431587A2 (fr) * 2002-12-19 2004-06-23 Kay Fischer Dispositif d'actionnement pour une soupape
EP1431587A3 (fr) * 2002-12-19 2005-03-30 Kay Fischer Dispositif d'actionnement pour une soupape

Also Published As

Publication number Publication date
RU2178842C1 (ru) 2002-01-27
EP1350959A1 (fr) 2003-10-08

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