SU430721A1 - STAND FOR RESOURCE TESTS OF ELECTRIC HOSTS OF ANTI-IGNITION SYSTEM OF BLADES OF THE STEERING SCREW OF THE HELICOPTER WITH THE CARDANE SUSPENSION OF THE SCREW OF THE SCREW TO THE SHAFT - Google Patents

STAND FOR RESOURCE TESTS OF ELECTRIC HOSTS OF ANTI-IGNITION SYSTEM OF BLADES OF THE STEERING SCREW OF THE HELICOPTER WITH THE CARDANE SUSPENSION OF THE SCREW OF THE SCREW TO THE SHAFT

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Publication number
SU430721A1
SU430721A1 SU1800133/23A SU1800133A SU430721A1 SU 430721 A1 SU430721 A1 SU 430721A1 SU 1800133/23 A SU1800133/23 A SU 1800133/23A SU 1800133 A SU1800133 A SU 1800133A SU 430721 A1 SU430721 A1 SU 430721A1
Authority
SU
USSR - Soviet Union
Prior art keywords
screw
stand
shaft
helicopter
blades
Prior art date
Application number
SU1800133/23A
Other languages
Russian (ru)
Inventor
И.Н. Бакиев
В.М. Боровский
Н.И. Гончаров
А.Ю. Лисс
В.И. Тюхтиенко
Original Assignee
И.Н. Бакиев
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 И.Н. Бакиев filed Critical И.Н. Бакиев
Priority to SU1800133/23A priority Critical patent/SU430721A1/en
Application granted granted Critical
Publication of SU430721A1 publication Critical patent/SU430721A1/en

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  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)

Abstract

Стенд для ресурсных испытаний электрожгутов системы антиобледенения лопастей рулевого винта вертолета с карданной подвеской втулки винта к валу, содержащий станину, на которой установлен привод, на валу которого закреплена испытываемая втулка, и механизм нагружения, в качестве одного из элементов которого используется проводка управления шагом винта, отличающийся тем, что, с целью приближения условий испытания к условиям летной эксплуатации, стенд снабжен вторым элементом механизма нагружения, выполненным в виде кронштейна, прикрепленного к втулке винта и снабженного установленным соосно с втулкой винта подшипником, прикрепленным к станине таким образом, что ось втулки винта наклонена относительно оси вала привода.Stand for endurance testing of electrical assemblies of the anti-icing system of the blades of the helicopter’s tail rotor with cardan gimbal-hinge suspension bracket containing the frame on which the drive is mounted, on the shaft of which the tested sleeve is fixed, and the loading mechanism, one of the elements of which is used to control the pitch of the screw, characterized in that, in order to approximate the test conditions to the conditions of flight operation, the stand is equipped with a second element of the loading mechanism, made in the form of a bracket, attached nnogo to the sleeve and provided with a screw mounted coaxially with the hub bearing screws attached to the frame so that the axis of the screw sleeve is inclined relative to the axis of the drive shaft.

SU1800133/23A 1972-06-23 1972-06-23 STAND FOR RESOURCE TESTS OF ELECTRIC HOSTS OF ANTI-IGNITION SYSTEM OF BLADES OF THE STEERING SCREW OF THE HELICOPTER WITH THE CARDANE SUSPENSION OF THE SCREW OF THE SCREW TO THE SHAFT SU430721A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1800133/23A SU430721A1 (en) 1972-06-23 1972-06-23 STAND FOR RESOURCE TESTS OF ELECTRIC HOSTS OF ANTI-IGNITION SYSTEM OF BLADES OF THE STEERING SCREW OF THE HELICOPTER WITH THE CARDANE SUSPENSION OF THE SCREW OF THE SCREW TO THE SHAFT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1800133/23A SU430721A1 (en) 1972-06-23 1972-06-23 STAND FOR RESOURCE TESTS OF ELECTRIC HOSTS OF ANTI-IGNITION SYSTEM OF BLADES OF THE STEERING SCREW OF THE HELICOPTER WITH THE CARDANE SUSPENSION OF THE SCREW OF THE SCREW TO THE SHAFT

Publications (1)

Publication Number Publication Date
SU430721A1 true SU430721A1 (en) 2004-07-20

Family

ID=60522100

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1800133/23A SU430721A1 (en) 1972-06-23 1972-06-23 STAND FOR RESOURCE TESTS OF ELECTRIC HOSTS OF ANTI-IGNITION SYSTEM OF BLADES OF THE STEERING SCREW OF THE HELICOPTER WITH THE CARDANE SUSPENSION OF THE SCREW OF THE SCREW TO THE SHAFT

Country Status (1)

Country Link
SU (1) SU430721A1 (en)

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