BAROSTATIC DOUBLE ACTING CONTROL VALVE Russian patent published in 2016 - IPC F02C7/00 F16K11/10 F16K17/04 

Abstract RU 2578766 C1

FIELD: motors and pumps.

SUBSTANCE: invention relates to a gas turbine engine system elements (CCD), and can be used in the lubrication system of heat-air turbine engines to control the pressure of the compressed air and the hot gases in the venting system. Barostatic double-acting valve for venting system aircraft gas turbine engine includes a housing with formed therein seats interacting with two poppet valves connected in parallel in the pipe venting, one of which - barostatic - is connected to the sensor, perceiving the change in pressure surrounding the engine atmosphere and the other valve - limiting the pressure in the venting system. Saddles are rotated in the same direction toward the sensing element, a pressure limiting valve is located between the sensing element and barostatic valve and mechanically coupled to the latter with the possibility of free running of both valves. Progress barostatic valve is greater than the valve travel limiting pressure.

EFFECT: present invention reduces the hydraulic resistance barostatic valve by increasing the flow section in the output path of the device that, according to the applicant, will increase the reliability of its work.

1 cl

Similar patents RU2578766C1

Title Year Author Number
DOUBLE-ACTION BAROSTATIC VALVE 2014
  • Golubov Aleksandr Nikolaevich
  • Semenov Vadim Georgievich
  • Marchukov Evgenij Juvenal'Evich
RU2558725C1
TESTING MACHINE FOR TESTING OF OIL PUMPS OF AIR TURBINE JET LUBRICATION SYSTEM 2013
  • Golubov Aleksandr Nikolaevich
  • Semenov Vadim Georgievich
  • Fomin Vjacheslav Nikolaevich
  • Marchukov Evgenij Juvenal'Evich
RU2535802C1
DOUBLE-ACTING SAFETY VALVE FOR THE BREATHING SYSTEM OF OIL CAVITIES OF AIRCRAFT GAS TURBINE ENGINE 2015
  • Golubov Aleksandr Nikolaevich
  • Marchukov Evgenij Yuvenalevich
  • Semenov Vadim Georgievich
RU2596893C2
METHOD OF VENTING ROTOR SUPPORT OIL SPACES OF AIRCRAFT GAS TURBINE ENGINE 1999
  • Andreev A.V.
  • Golubov A.N.
  • Lebedev V.A.
  • Marchukov E.Ju.
  • Semenov V.G.
  • Chepkin V.M.
RU2148177C1
OIL SYSTEM OF AIR GAS TURBINE ENGINE 2013
  • Golubov Aleksandr Nikolaevich
  • Semenov Vadim Georgievich
  • Fomin Vjacheslav Nikolaevich
RU2535796C1
AIR BREATHING SYSTEM IN AIRCRAFT GAS TURBINE ENGINE 2019
  • Golubov Aleksandr Nikolaevich
  • Marchukov Evgenij Yuvenalevich
  • Fomin Vyacheslav Nikolaevich
RU2709751C1
DEVICE FOR LUBRICATING BEARING SUPPORT OF TURBOMACHINE ROTOR 2017
  • Golubov Aleksandr Nikolaevich
  • Fomin Vyacheslav Nikolaevich
  • Marchukov Evgenij Yuvenalevich
RU2639262C1
OIL SYSTEM OF GAS-TURBINE ENGINE 2014
  • Golubov Aleksandr Nikolaevich
  • Semenov Vadim Georgievich
RU2539928C1
DEVICE FOR LUBRICATION OF SUPPORT BEARING OF ROTOR OF JET GAS TURBINE ENGINE 2016
  • Golubov Aleksandr Nikolaevich
  • Fomin Vyacheslav Nikolaevich
RU2623581C1
DOUBLE-FLOW GAS TURBINE ENGINE 2018
  • Kanakhin Yurij Aleksandrovich
  • Kuprik Viktor Viktorovich
  • Marchukov Evgenij Yuvenalevich
  • Nekrasova Elena Sergeevna
  • Starodumova Irina Mikhajlovna
RU2700110C1

RU 2 578 766 C1

Authors

Golubov Aleksandr Nikolaevich

Semenov Vadim Georgievich

Marchukov Evgenij Juvenalevich

Dates

2016-03-27Published

2014-12-30Filed