version of the mk motora Welfare AM-34:
Associated M-34
Project juego spriahnutých motorboat M-34, the town of mali poháňať spoločnú vrtuľu, were designed pre project lietadla Kalinin K-7, nakoniec sa nevyrábal.
M-34F
Malokusová séria built in 1933 with výkonom 620 kW (830 HP).
M-34R
Version of R (Reducer) bola equipped redukčnou prevodovkou. Engine mal power 600 kW (800 HP) and hmotnosť 670 kg. Štátnymi skúškami prešiel in the death of 1933 and the vo manufacture zostal into the konca roka 1939.
M-34RD
It was a verziu M-34R (D ako Daľnyj) určenú pre lietadlá with veľkým doletom - ANT-25 and the Tupolev TB-3 the town were designated to transport VIP osôb. Bolo produced around 50 motorboat (10 pcs pre ANT-25 and 50 pre TB-3), pri ktorých sa dohliadalo on the quality of production and on the menšie tolerancie. Were equipped with karburátormi TO-the 34RD. The rotational speed of motora were increased so that the engine supplied the power of 830 hp.
M-34N
(N ako Nagnetateľ "or preplňovaný) His development of the sa began in 1931, but konštrukcia his dvojstupňového kompresora sa showed nespoľahlivou. How to refund bol developed in kancelárii CIAM jednorýchlostný odstredivý compressor, which sa began to testovať in novembri 1933. Its production started in septembri 1934. Bol designed ako vymeniteľný module and a bolo, it is possible to install anything, etc on the iných verziách motora M-34. Engine mal menovitý power 610 kW (820 HP). In rokoch 1938-1940 bol pre engine developed and tested compressor PTK, nakoniec, however, nebol adopted into production.
M-34NA
Compared to verzii N occurred to predĺženiu life niektorých komponentov motora and slight corrections. Engine mal rovnaký the performance of the ako pôvodná touch.
M-34RN
The engine version of the mk R bol zamontovaný compressor from the version of the mk N. The engine gave rovnaký the performance of the android version of N. Evolution štátnych skúšok motora in septembri 1934 occurred to prepáleniu piestov motora.
M-34RA
It was a verziu M-34R with the rovnakými few modifications and výkonom ako pri motore M-34NA.
M-34RNA
Version of the M-34RN so všetkými few modifications established by the modelov na and RA. Engine mal rovnaký the performance of the ako front of the team, but his hmotnosť sa increased to 748 kg. The first years with týmto motorom graduated from the TB-3 in death in 1935. Its production started koncom roka 1935.
M-34NB
It was a vylepšenú verziu M-34NA, where there has been a zosilneniu kľukovej skrine, odľahčeniu kľukovej hriadele, modified, nosom, and improved kompresorom. Performance motora zostal rovnaký, but its hmotnosť fell to 638 kg. The prototype lietadla Polikarpov R-Z bolo in 1936, the tested turbodúchadlo TK-1.
M-34RNB
Reduktorová version of the model NB with odľahčenou reduktorovou prevodovkou. Engine mal rovnaký performance, but its hmotnosť dropped to 725 kg. Vyrábal sa from októbra 1935 to konca roka 1939).
M-34P
(P ako Pušečnyj). It was a verziu RN upravenú pre uloženie especially kanóna between radmi valcov and strieľajúci hollow hriadeľom prevodovky motora. Špecifikácie on the engine were issued in August 1934, ďalšie details but nie soo know it.
M-34NV
(N ako Neprosredsvennyj vprysk) Version with priamym vstrekovaním fuel. Testovaním on pozemnej stool prešiel engine in 1935 and the first years he graduated in 1937. Pre production but nebol adopted. His performance amounted to 735 kW (985 HP).
M-34RNV
Reduktorová version of the M-34NV.
AM-34RNV-TK
The prototype bol built in 1938 vo verzii RNV with pridaním turbodúchadla TK-1. Menovitý power motora amounted to 630 kW (850 HP) and its estimated hmotnosť bola 810 kg
AM-34RS
The prototype bol built in 1938 so zmiešaným chladením - vzduchom chladené sleeves(??) (sleeves) and ethylene glykolom chladené head valcov. Menovitý power motora amounted to 890 kW (1200 HP).
AM-34NF
The prototype with the poháňaným odstredivým kompresorom and turbodúchadlom TK-1. For the flight of bol tested in TB-3. Kompresný pomer bol a 6.6:1 and power 735 kW (895 HP).
M-34N2B
The prototype with the turbokompresorom, withdrew it two turbodúchadlami and štyroma karburátormi K-4. Performance motora 770 kW (1030 HP).
AM-34FRN
(F ako Forsirovannyj - zosilnený). Its development began in 1934, but its development nebol completed even in the year 1938. There has been posilneniu kľukového hriadeľa, kľukovej skrine, súkolí and bočných spojov ojníc. There has been vylepšeniu kompresora and ku vybaveniu new rozvodmi exhaust plynov. Carburetors sa presunuli for the compressor. The engine was the performance of 890 kW (1200 HP). The Bol issued on the Parížskej leteckej exhibition in 1937.
AM-34FRNA
It was a verziu M-34FRN vybavenú štyroma karburátormi.
AM-34FRNB
Version of the M-34FRN equipped šiestimi karburátormi. Small séria bola equipped rozvodmi pressure of the air supplied prostredníctvom externého kompresora. The system ACN-2 (ACN - Aggregat centraľnogo nadduva) sa tested on the machine Pe-8 in rokoch 1938-1939.
AM-34FRNV
The hlavná variant motora AM-34. Bola built in priebehu rokov 1938-1939. Occurred to change konštrukcie kľukovej skrine, there has been použitiu bronze púzdier pre hlavné podpery. Nose kľukového hriadeľa bol dlhší, occurred to modify the marriage mazacieho system. Engine bol featured štyroma karburátormi. Odliatky ventilov were made up of horčíkovej zliatiny. Performance motora zostal rovnaký, but there has been zvýšeniu of his weight on the 763,5 kg. Were tested etc its variants with priamym vstrekovaním fuel and withdrew it two turbodúchadlami TK-1, or, however, adopted into the production.
AM-34RB
It was about veriu r'n'b, in which we have been committed to odstráneniu kompresorov (in the year 1938-1939).
Námorné variants motora M-34:
GM-34
The engine of the bol to the designated pre powered torpedo člnov. Mal performance of the 600 kW and hmotnosť 864 kg.
GAM-34F
Zosilnená version of the GM-34 with bronze hlavnými púzdrami. Kľukový hriadeľ, block hláv and niektoré ďalšie components were used from the aviation motora AM-34FRNV. The engine supplied menovitý power of 750 kW (1000 HP) and mal hmotnosť 1080 kg. Mal kompresný pomer of 7.3:1.
GAM-34FN
Version of GAM-34F with with poháňaným kompresorom FN-25 and karburátorom K-4 karburátorom. Used the oil system of the motora GAM-34BS and vo manufacture bol since 1939.
GAM-34BP
Version slúžila to drive obrnených riečnych člnov.
GAM-34BS
An enhanced version of GAM-34BP. Menovitý power bol 630 kW (850 HP) with hmotnosťou 1045 kg.
Námorné version of the mk motora poháňali torpedo člny G-5, G-6, G-8 and SM-4 and riečne obrnené člny Project 1124 and Project 1125.
Engine poháňal etc tanks T-100 and SMK and self-propelled delo the SU-100Y.
Zroj:
http://en.wikipedia.org/wiki/Mikulin_AM-34.
Associated M-34
Project juego spriahnutých motorboat M-34, the town of mali poháňať spoločnú vrtuľu, were designed pre project lietadla Kalinin K-7, nakoniec sa nevyrábal.
M-34F
Malokusová séria built in 1933 with výkonom 620 kW (830 HP).
M-34R
Version of R (Reducer) bola equipped redukčnou prevodovkou. Engine mal power 600 kW (800 HP) and hmotnosť 670 kg. Štátnymi skúškami prešiel in the death of 1933 and the vo manufacture zostal into the konca roka 1939.
M-34RD
It was a verziu M-34R (D ako Daľnyj) určenú pre lietadlá with veľkým doletom - ANT-25 and the Tupolev TB-3 the town were designated to transport VIP osôb. Bolo produced around 50 motorboat (10 pcs pre ANT-25 and 50 pre TB-3), pri ktorých sa dohliadalo on the quality of production and on the menšie tolerancie. Were equipped with karburátormi TO-the 34RD. The rotational speed of motora were increased so that the engine supplied the power of 830 hp.
M-34N
(N ako Nagnetateľ "or preplňovaný) His development of the sa began in 1931, but konštrukcia his dvojstupňového kompresora sa showed nespoľahlivou. How to refund bol developed in kancelárii CIAM jednorýchlostný odstredivý compressor, which sa began to testovať in novembri 1933. Its production started in septembri 1934. Bol designed ako vymeniteľný module and a bolo, it is possible to install anything, etc on the iných verziách motora M-34. Engine mal menovitý power 610 kW (820 HP). In rokoch 1938-1940 bol pre engine developed and tested compressor PTK, nakoniec, however, nebol adopted into production.
M-34NA
Compared to verzii N occurred to predĺženiu life niektorých komponentov motora and slight corrections. Engine mal rovnaký the performance of the ako pôvodná touch.
M-34RN
The engine version of the mk R bol zamontovaný compressor from the version of the mk N. The engine gave rovnaký the performance of the android version of N. Evolution štátnych skúšok motora in septembri 1934 occurred to prepáleniu piestov motora.
M-34RA
It was a verziu M-34R with the rovnakými few modifications and výkonom ako pri motore M-34NA.
M-34RNA
Version of the M-34RN so všetkými few modifications established by the modelov na and RA. Engine mal rovnaký the performance of the ako front of the team, but his hmotnosť sa increased to 748 kg. The first years with týmto motorom graduated from the TB-3 in death in 1935. Its production started koncom roka 1935.
M-34NB
It was a vylepšenú verziu M-34NA, where there has been a zosilneniu kľukovej skrine, odľahčeniu kľukovej hriadele, modified, nosom, and improved kompresorom. Performance motora zostal rovnaký, but its hmotnosť fell to 638 kg. The prototype lietadla Polikarpov R-Z bolo in 1936, the tested turbodúchadlo TK-1.
M-34RNB
Reduktorová version of the model NB with odľahčenou reduktorovou prevodovkou. Engine mal rovnaký performance, but its hmotnosť dropped to 725 kg. Vyrábal sa from októbra 1935 to konca roka 1939).
M-34P
(P ako Pušečnyj). It was a verziu RN upravenú pre uloženie especially kanóna between radmi valcov and strieľajúci hollow hriadeľom prevodovky motora. Špecifikácie on the engine were issued in August 1934, ďalšie details but nie soo know it.
M-34NV
(N ako Neprosredsvennyj vprysk) Version with priamym vstrekovaním fuel. Testovaním on pozemnej stool prešiel engine in 1935 and the first years he graduated in 1937. Pre production but nebol adopted. His performance amounted to 735 kW (985 HP).
M-34RNV
Reduktorová version of the M-34NV.
AM-34RNV-TK
The prototype bol built in 1938 vo verzii RNV with pridaním turbodúchadla TK-1. Menovitý power motora amounted to 630 kW (850 HP) and its estimated hmotnosť bola 810 kg
AM-34RS
The prototype bol built in 1938 so zmiešaným chladením - vzduchom chladené sleeves(??) (sleeves) and ethylene glykolom chladené head valcov. Menovitý power motora amounted to 890 kW (1200 HP).
AM-34NF
The prototype with the poháňaným odstredivým kompresorom and turbodúchadlom TK-1. For the flight of bol tested in TB-3. Kompresný pomer bol a 6.6:1 and power 735 kW (895 HP).
M-34N2B
The prototype with the turbokompresorom, withdrew it two turbodúchadlami and štyroma karburátormi K-4. Performance motora 770 kW (1030 HP).
AM-34FRN
(F ako Forsirovannyj - zosilnený). Its development began in 1934, but its development nebol completed even in the year 1938. There has been posilneniu kľukového hriadeľa, kľukovej skrine, súkolí and bočných spojov ojníc. There has been vylepšeniu kompresora and ku vybaveniu new rozvodmi exhaust plynov. Carburetors sa presunuli for the compressor. The engine was the performance of 890 kW (1200 HP). The Bol issued on the Parížskej leteckej exhibition in 1937.
AM-34FRNA
It was a verziu M-34FRN vybavenú štyroma karburátormi.
AM-34FRNB
Version of the M-34FRN equipped šiestimi karburátormi. Small séria bola equipped rozvodmi pressure of the air supplied prostredníctvom externého kompresora. The system ACN-2 (ACN - Aggregat centraľnogo nadduva) sa tested on the machine Pe-8 in rokoch 1938-1939.
AM-34FRNV
The hlavná variant motora AM-34. Bola built in priebehu rokov 1938-1939. Occurred to change konštrukcie kľukovej skrine, there has been použitiu bronze púzdier pre hlavné podpery. Nose kľukového hriadeľa bol dlhší, occurred to modify the marriage mazacieho system. Engine bol featured štyroma karburátormi. Odliatky ventilov were made up of horčíkovej zliatiny. Performance motora zostal rovnaký, but there has been zvýšeniu of his weight on the 763,5 kg. Were tested etc its variants with priamym vstrekovaním fuel and withdrew it two turbodúchadlami TK-1, or, however, adopted into the production.
AM-34RB
It was about veriu r'n'b, in which we have been committed to odstráneniu kompresorov (in the year 1938-1939).
Námorné variants motora M-34:
GM-34
The engine of the bol to the designated pre powered torpedo člnov. Mal performance of the 600 kW and hmotnosť 864 kg.
GAM-34F
Zosilnená version of the GM-34 with bronze hlavnými púzdrami. Kľukový hriadeľ, block hláv and niektoré ďalšie components were used from the aviation motora AM-34FRNV. The engine supplied menovitý power of 750 kW (1000 HP) and mal hmotnosť 1080 kg. Mal kompresný pomer of 7.3:1.
GAM-34FN
Version of GAM-34F with with poháňaným kompresorom FN-25 and karburátorom K-4 karburátorom. Used the oil system of the motora GAM-34BS and vo manufacture bol since 1939.
GAM-34BP
Version slúžila to drive obrnených riečnych člnov.
GAM-34BS
An enhanced version of GAM-34BP. Menovitý power bol 630 kW (850 HP) with hmotnosťou 1045 kg.
Námorné version of the mk motora poháňali torpedo člny G-5, G-6, G-8 and SM-4 and riečne obrnené člny Project 1124 and Project 1125.
Engine poháňal etc tanks T-100 and SMK and self-propelled delo the SU-100Y.
Zroj:
http://en.wikipedia.org/wiki/Mikulin_AM-34.