SU129345A1 - Device for checking the state of a gas turbine during its operation - Google Patents
Device for checking the state of a gas turbine during its operationInfo
- Publication number
- SU129345A1 SU129345A1 SU642103A SU642103A SU129345A1 SU 129345 A1 SU129345 A1 SU 129345A1 SU 642103 A SU642103 A SU 642103A SU 642103 A SU642103 A SU 642103A SU 129345 A1 SU129345 A1 SU 129345A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- state
- checking
- gas turbine
- turbine during
- probe
- Prior art date
Links
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Description
Устройства дл проверки состо ни i-азовон турбины в гтроцессо ее укоплуатЗЦии, к которых применен щуп. вволимьп ;5 между .гопатками ротора it корпусом и си зг.ниый с регнстрируюнщм прибором , известны.Devices for checking the state of i-Azovon turbines in the process with its utilization, to which the probe is applied. In no way; 5 between the rotor’s housings of the it’s body and those that are equipped with a mounting device are known.
Отличительной особенностьн) предлагаемого устройства н.ч етс П)именепие щупа, HA-iciOHiero во/пюобразнл-ю рабочую поверхность дл контакта с торцами двил ущихс .чопаток П св занного соответствующими передачами с пером и поворотным барабаном самоппи1 Н1его механизма . Такое выполнение устройства обеспечивает автоматическую непрерывную регистранию величины относительной выт жки каждой .ггопатки.Distinctive features of the device proposed are: n) n) the name of the probe, the HA-iciOHiero in / pyoobraznly working surface for contact with the ends of the twelve knives n connected with the corresponding gears with a feather and a rotary drum of the self-supporting mechanism. Such an embodiment of the device provides automatic continuous registration of the relative extrusion value of each footer.
На чертеже схематически показано оиисываемое устройство.The drawing shows a schematic of the device.
1)ужин щий / устройства имеет 1юлнообразпую рабочую ;ioве )хность. Он сидит на конце зубчатой рейки 2, св занной с пером посредство.м ншстерни 4, помещенной на ва.тике 5. Ibi этом же ва;1ИК15 сидит секторный кулачок 6, сообщающий Периодическое качате.чьное движение анкеру 7, взаимодействующему с наход щимс под действием пружины 8; анкерным колесом 9. Это колесо на .одном валу с попоротным барабаном 10 самопишуи1его механизма.1) The supporter / device has a one-sided worker; iove). It sits on the end of the toothed rack 2, which is connected to a pen through a shaft 4, placed on model 5. Ibi is the same; 1IK15 is a sector cam 6, which informs Periodic kachat.chnye movement anchor 7, interacting with being under the action of the spring 8; an anchor wheel 9. It is a wheel on a single shaft with a reversible drum 10 self-writing mechanism.
11ри поворачивании рабочего колеса r;i: OBoi; лопатки С1юими TOpua.viK // набегают на волнообразную рабочую поверхность пружин щего щупа / и ирогибают его. Перемещение щупа передаетс через щестерню 4 на перо 3 и через анкер 7 и анкерное колесо 9 на барабан 10 самопищущего механизма, в результате чего последний ро:истрирует ВЫТЯЖКУ отдельных .топаток.11 when turning the impeller r; i: OBoi; blades S1yuimi TOpua.viK // run over the wave-shaped working surface of the spring probe / and irogi it. The movement of the probe is transmitted through the brush 4 to the feather 3 and through the anchor 7 and the anchor wheel 9 to the drum 10 of the self-searching mechanism, as a result of which the last po: it will shrink the EXTRACT of the individual.
t; . fi . 5 Пред мет изобретени t; . fi. 5 Prev Invention
Уаиройсйй дМзгтфбйерКи состо ни газовой турбины в процессе ее эксплуатации..Л. ройприменен щун, вводимый в зазор между лопатками ротора и корпусом и св занный с регистрирующим прибором , о т.тH.fa кЛ.1|&ес , что, с целью автоматическо) непрерывной регистрациивеличины относите;гьной выт жки каждой лопатки, Н1.ун выполнен с волнообразной 1)абочей поверхностью д.г контакта с торцамн движун1,ихс лопаток и св зан соответст Люпдими -нередачами с пером и поворотным барабаноМ caMoin-iniyinero механизма.The state of the gas turbine in the process of its operation. Reymployed shchun, introduced into the gap between the rotor blades and the body and associated with the recording device, about t.H.fa kL.1 | & eu, which, for the purpose of automatic) continuous registration, relate the damping out of each blade, H1. un is made with a wave-shaped 1) abdomen surface dg contact with the end face of the blades, their blades and is associated with Lupdimi-neredachi with a feather and a rotary drum caMoin-iniyinero mechanism.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU642103A SU129345A1 (en) | 1959-10-22 | 1959-10-22 | Device for checking the state of a gas turbine during its operation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU642103A SU129345A1 (en) | 1959-10-22 | 1959-10-22 | Device for checking the state of a gas turbine during its operation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU129345A1 true SU129345A1 (en) | 1959-11-30 |
Family
ID=48400505
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU642103A SU129345A1 (en) | 1959-10-22 | 1959-10-22 | Device for checking the state of a gas turbine during its operation |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU129345A1 (en) |
-
1959
- 1959-10-22 SU SU642103A patent/SU129345A1/en active
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