METHOD FOR DETERMINATION OF FLOW-RATE CHARACTERISTICS OF DRAINAGE DEVICES OF FLIGHT VEHICLE COMPARTMENT AND SYSTEM FOR ITS REALIZATION Russian patent published in 2005 - IPC

Abstract RU 2253095 C2

FIELD: aerodynamic tests, applicable in rocket manufacturing and aviation for determination and control of flight aerodynamic loads on the compartments of flight vehicles and their components.

SUBSTANCE: the claimed method includes injection of thermostating medium in the compartment, used as working medium. The flow rate of this medium is so selected that the pressure differentials outside and inside the compartment in the ground conditions would correspond the pressure differentials acting on the compartment in the flight trajectory. The characteristics of interest of the drainage devices are determined according to the measured flow rates at the run over of the thermostating medium through each drainage device, pressure differentials and the medium temperature in the compartment. The non-tightness of the compartment is taken into account. According to the test results, a decision on finishing of the compartment, or a change of the quantity of the drainage devices operating in flight, may be taken.

EFFECT: enhanced accuracy of determination of the flow-rate characteristics of the drainage device, reliability of operation of the compartment, and reduced operating expenditures connected with the work.

2 cl, 5 dwg

Similar patents RU2253095C2

Title Year Author Number
METHOD OF DETERMINATION OF FLOW RATE CHARACTERISTICS OF DRAINAGE FACILITIES OF FLYING VEHICLE CASE AND SYSTEM FOR REALIZATION OF THIS METHOD 2003
  • Legostaev V.P.
  • Aliev V.G.
  • Shorin A.N.
  • Djad'Kin A.A.
  • Lebedev V.I.
  • Bolotin V.A.
  • Kazakov M.I.
RU2267108C2
METHOD OF ESTIMATION OF UNTIGHTNESS OF FLYING VEHICLE COMPARTMENT PROVIDED WITH DRAINAGE DEVICES 2003
  • Bolotin V.A.
  • Djad'Kin A.A.
  • Kazakov M.I.
  • Lebedev V.I.
RU2246708C1
METHOD OF THERMOSTATTING OF ITEMS LOCATED IN SUCCESSION IN COMPARTMENTS OF LAUNCH VEHICLE NOSE CONE 2005
  • Legostaev Viktor Pavlovich
  • Aliev Valerij Gejdarovich
  • Shorin Aleksandr Nikolaevich
  • Djad'Kin Anatolij Aleksandrovich
  • Beloshitskij Aleksandr Vasil'Evich
  • Stavritskij Aleksandr Konstantinovich
  • Bolotin Viktor Aleksandrovich
  • Shuvalov Mikhail Petrovich
RU2294864C2
METHOD OF THERMOSTATTING OF INSTRUMENT BAY OF CRYOGENIC STAGE OF SPACE NOSE CONE OF LAUNCH VEHICLE AND ONBOARD SYSTEM FOR REALIZATION OF THIS METHOD 2004
  • Bolotin Viktor Aleksandrovich
RU2290353C2
METHOD OF THERMOSTATTING OF INSTRUMENT MODULE OF SPACE LAUNCH VEHICLE NOSE CONE AND ONBOARD SYSTEM FOR REALIZATION OF THIS METHOD (VERSIONS) 2004
  • Legostaev Viktor Pavlovich
  • Aliev Valerij Gejdarovich
  • Shorin Aleksandr Nikolaevich
  • Djad'Kin Anatolij Aleksandrovich
  • Beloshitskij Aleksandr Vasil'Evich
  • Bolotin Viktor Aleksandrovich
  • Kazakov Mikhail Ivanovich
  • Jur'Ev Dmitrij Aleksandrovich
RU2279377C2
METHOD FOR THERMOSTATTING PAY LOAD AND INSTRUMENTS OF CONTROL SYSTEM OF SPACE HEAD OF CARRIER ROCKET, AND AIRBORNE SYSTEM USED FOR METHOD REALISATION 2007
  • Bolotin Viktor Aleksandrovich
  • Djad'Kin Anatolij Aleksandrovich
  • Simakova Tat'Jana Vladimirovna
RU2353556C2
MODE OF TEMPERATURE CONTROL OF THE OBJECTS OF A ROCKET BLOCK 2005
  • Beloshitskij Aleksandr Vasil'Evich
  • Bolotin Viktor Aleksandrovich
  • Djad'Kin Anatolij Aleksandrovich
  • Shuvalov Mikhail Petrovich
RU2292291C2
DIFFUSER USED FOR THERMAL CONDITIONING OF CARRIER ROCKET OBJECTS (VERSIONS) 2007
  • Bolotin Viktor Aleksandrovich
  • Djad'Kin Anatolij Aleksandrovich
  • Simakova Tat'Jana Vladimirovna
RU2353557C2
METHOD OF CONTROL OF AERODYNAMIC LOADS ACTING OF FLYING VEHICLE CASE AND DEVICE FOR REALIZATION OF THIS METHOD (VERSIONS) 1999
  • Bolotin V.A.
  • Djad'Kin A.A.
  • Kazakov M.I.
  • Lebedev V.I.
RU2145564C1
ROCKET-CARRIER ASCENT UNIT 2007
  • Bolotin Viktor Aleksandrovich
  • Djad'Kin Anatolij Aleksandrovich
  • Kazakov Mikhail Ivanovich
  • Lebedev Vladimir Ivanovich
RU2355607C1

RU 2 253 095 C2

Authors

Bolotin V.A.

Djad'Kin A.A.

Kazakov M.I.

Lebedev V.I.

Dates

2005-05-27Published

2003-08-06Filed