FIELD: turbo-machines.
SUBSTANCE: turbine machine design with heat exchanger, integrated into of turbine machine hot gases flow (1) outlet gas-air duct (10), characterized by that heat exchange elements (60, 60a-60i; 9), installed in one of components (11, 14, 14a, 14b, 15, 16, 16a, 16b, 18, 18a, 18c) of outlet gas-air duct (10), are made with possibility of directing hot gases (1) flow part, passing through heat exchange components, with further use of residual heat energy of said part of hot gases flow (1) to increase power on turbo-machine (20, 20a, 20b) shaft (30, 31), leaving larger part of hot gases flow (1) undisturbed.
EFFECT: enables to achieve optimum total compromise between technical characteristics, weight and operating costs.
9 cl, 9 dwg
Title | Year | Author | Number |
---|---|---|---|
VEHICLE POWER PLANT | 2018 |
|
RU2693953C1 |
POWER PLANT | 1989 |
|
RU2029880C1 |
HEAT ENGINE; METHOD OF OPERATION AND DESIGN VERSIONS | 1996 |
|
RU2146014C1 |
MULTIFUNCTION SWIRLING JET BLOWER | 1999 |
|
RU2156892C1 |
METHOD AND BENCH FOR TESTING TURBO-SUPERCHARGING COMPRESSOR OF INTERNAL COMBUSTION ENGINE | 1990 |
|
RU2023248C1 |
METHOD AND SYSTEM OF ENERGY RECOVERY IN AIRCRAFT | 2012 |
|
RU2608195C2 |
METHOD OF AND DEVICE FOR INCREASING TEMPERATURE DIFFERENCE IN HEAT ENGINE | 1998 |
|
RU2151310C1 |
INTERNAL COMBUSTION PISTON ENGINE | 1998 |
|
RU2132954C1 |
GAS PUMPING UNIT | 2017 |
|
RU2685802C1 |
METHOD OF CONVERTING HEAT ENERGY TO MECHANICAL WORK IN GAS-TURBINE ENGINE AND GAS-TURBINE ENGINE | 1992 |
|
RU2031226C1 |
Authors
Dates
2017-01-30—Published
2011-07-05—Filed