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№ п.п. | Наименование | Армировочный чертеж | Агрегат |
---|---|---|---|
Электрощетки генераторов | |||
1 | Щетка | 555198 | ГО-4ПЧ-4 |
2 | Щетка | 555.172 | ГО-16ПЧ-8РС |
3 | Щетка | 555200 | ПТ-7ПЧ-4А |
4 | Щетка | 555265 | СТГ - 3,2с |
5 | Щетка | 555217 | СТГ-12 ТМО-1000 |
6 | Щетка | 995225 | СТГ-18 ТМО-1000 |
7 | Щетка | 555.124 | СГО-12,3с, СГО-8.3с, |
8 | Щетка | 555126 | СГО-30У.4с УРС |
9 | Щетка | 555070 | СГС-90/360, 2с |
10 | Щетка | 555071 | СГС-90/360, 2с |
11 | Щетка | 555127 | СГС-40П, ПУ-2 |
12 | Щетка | 555092 | СГС-30Б |
13 | Щетка | 555.227 | ГС-12 ТО |
14 | Щетка | 8А5593.088 | ГС-18МО (ГС-24Б,2с) |
15 | Щетка | 555046 | ГС-24 А |
16 | Щетка | 555.070 | ГС-24 А, 3с |
17 | Щетка | 555182 | ВГ 7500Я-2с |
18 | Щетка | 555010 | ГСП-3000, Ж, М |
19 | Щетка | 555097 | ГСР-СТ-6000 П |
№п/п | Наименование продукции | Чертежный номер |
---|---|---|
1 | Лампа-фара самолетная | ЛФЛ 27-250 |
2 | Лампа-фара самолетная | ЛФЛ 27-250-1 |
3 | Лампа-фара самолетная | ЛФЛ 27-450-1 |
4 | Лампа-фара самолетная | ЛФЛ 27-450-5 |
5 | Лампа-фара самолетная | ЛФЛ 27-450+250 |
6 | Лампа-фара самолетная | ЛФЛ 27-600+250 |
7 | Лампа-фара самолетная | ЛФЛ 27-1000 |
8 | Лампа-фара самолетная | ЛФЛ 27-1000+450 |
9 | Лампа-фара самолетная | ЛФЛ 26-140-1 |
10 | Лампа-фара самолетная | ЛФЛ 28-60-1 |
11 | Лампа-фара самолетная | ЛФЛ 28-200+130-1 |
12 | Лампа-фара самолетная | ЛФЛ 28-600+180-1 |
- The Priboy battery - 2C is intended for use as an autonomous power source for the R-855 UM and R-855 A1 radios.
- Sensor МУ-615 А heat-resistant potentiometric sensor of angular displacements.
- PTP potentiometer heat-resistant precision.
- PLP linear precision potentiometer.
- PPLM-IM potentiometer precision multi-turn linear.
- PPMF-IM potentiometer precision multi-turn functional.
- Aviation lead-acid battery 12-SAM-28P (TU 16-89 IRFG.563400.001) is designed to operate on aircraft for autonomous starting of aircraft engines and on-board electrical equipment, for power supply during emergency conditions in the aircraft power supply system.
- Aviation battery 20NKBN-25-U3 - designed to operate on aircraft to autonomously launch aircraft engines and on-board electrical equipment, to power the electrical system during emergency conditions in the aircraft’s power supply system.
- Contactors TKD501 DOD, TKD501 KOD, TKD101 D1, TKD201 D1, TKD201 KT with one pair of open contacts are designed to connect one DC circuit in various climatic conditions.
- TKD502 DT contactors with two pairs of open contacts are designed to connect two DC circuits.
- Contactors TKS101DOD, TKS201DOD, TKS401DOD, TKS601DOD, TKS101KOD, TKS201KOD, TKS401KOD, TKS601KOD with one pair of open contacts are designed to connect one DC circuit in different climatic conditions.
- Contactors TKS210DT, TKS410DT with one pair of closed contacts are designed to disconnect one DC circuit.
- TKS 602A contactors with two pairs of open contacts are designed to connect two DC circuits.
- Contactors electromagnetic KM series, designed for remote on and off loads in a DC system. KM100-V, KM200-V, KM400-V, KM600-V, KM100-D-V, KM200-D-V, KM400-D-V, KM400-D-V, KM600-D-V, KM25-V, KM25-D-V, KM50-D-V.
- KP electromagnetic contactors are designed to remotely transfer loads from one DC system to another. KP100-D-V.
- Sockets and connectors (РМ, ШР, etc.):
- Hyperboloid contacts
- Electrical connectors
- Contact devices,
- Sockets connecting
- Rectangular connectors
-Cylindrical connectors
- Miniature connectors
- Subminiature connectors
- ATP system BGO:
The fire alarm system for the baggage and cargo compartments of the aircraft (SPS-BGO) is designed to perform the following functions on the ground and in flight:
- self-monitoring of the health of the components, namely: the alarm unit (BS) and smoke detectors (DD), as well as inter-unit connections;
- smoke alarm in the compartments of the aircraft, the degree of which characterizes the possibility of a fire.
Specifications:
The number of system channels is from 1 to 7.
The range of smoke change is 0 .... thirty %.
The response threshold of each channel of the system is set from 7% to 10% of smoke.
The limit of permissible basic absolute error of the alarm operation of each channel of the system is ± 3% of smoke.
The system is not a source of radio interference.
The system is powered from an on-board DC network with a voltage of 27 ± 15%.
The current consumed by the system is not more than 1.0 A.
Smoke detectors (DD) remain operational when the ambient temperature rises to 200 ° C for at least 2 minutes.
Overall dimensions of system devices, mm: BS - 41x208x125, DD - Æ115 × 50.
Mass of system devices, kg: BS - 0.75; DD - 0.18.
- LED smoke detector:
The smoke detector (DM) is designed to detect fire (smoke) in the compartments of the aircraft and performs the following functions on the ground and in flight:
fire detection;
issuing fire (smoke) and failure signals.
Specifications
A fire signal is generated when:
smoke - level 10% (smoke channel);
temperature - 100˚С (along the temperature channel).
The limits of the permissible basic absolute error of the alarm:
by smoke ± 3%;
temperature ± 5 ° С
LED output signal levels (nominal values) at a load of not more than 200 Ohms:
fire signal - 20 mA;
health signal - 10 mA;
LED failure signal - 5 mA.
The alarm device remains operational when the ambient temperature rises to 200 ° C for 2 minutes.
Signaling device power - on-board DC network with voltage of 27 V.
The design of the signaling device is vibration and shock resistant.
Operating temperature range - from minus 35 ° С to plus 70 ° С;
The alarm device is adapted to dust pollution, noise-resistant and is not a source of interference.
Overall dimensions of SD, mm - Ø115 x 50.
The mass of diabetes, kg - 0.25.
- The receiver of the resistance thermometer P-1 TU 25-7529.001-87:
The receiver is intended for use in a set of electric resistance thermometer for measuring the temperature of liquids and gases (oil, air).
The working range of the measured temperatures, ° C - from -70 to +150
Receiver impedance, Ohm
at a temperature of 0 ° C - 99.1 ± 0.15
at a temperature of 100 ° C - 129.8 ± 0.44
Vibration resistance frequency range, Hz: - 5 ... 500
acceleration amplitude, m / s2, no more - 98
Thermal inertia index, s, not more than -
Material of steel reinforcement 12X18H10T
- Relay:
RES-9 RES-22 RES-34 RES-39 RES-47 RES-49 RES-53
RES-55 RES-60 RES-80 REC-23 REC-30 REC-37 REC-43
REK-48 REN-33 REN-35 REV-14/15 REV-16/17 RPA-14 RPA-16