This document appears to list 5 names that may be associated with developing a stratified charged engine. It provides a very high-level listing of names without any additional context about the people, project, or engine described.
Definition of Supercharging ,
Effect of Supercharging ,
Need of Supercharging ,
Types of Supercharging
1) Centrifugal Supercharger
2) Rootes Supercharger
3) Vane Supercharger ,
Advantages & Disadvantages of Supercharging
Definition of Supercharging ,
Effect of Supercharging ,
Need of Supercharging ,
Types of Supercharging
1) Centrifugal Supercharger
2) Rootes Supercharger
3) Vane Supercharger ,
Advantages & Disadvantages of Supercharging
Hybrid pneumatic engine with exhaust heat recoveryLiviu Giurca
The invention relates to a four-stoke hybrid pneumatic engine of the type ensuring energy recovery, which can be used for road motor vehicles or other transportation means with a view to reducing the fuel consumption and emissions which are deemed to cause the greenhouse effect. According to the invention, the hybrid pneumatic engine has a number of cylinders which are of the conventional type and at least one modified cylinder operating an active valve actuated by a mechatronic system.
A kinetic energy recovery system (often known simply as KERS, or kers) is an automotive system for recovering a moving vehicle's kinetic energy under braking. The recovered energy is stored in a reservoir (for example a flywheel or high voltage batteries) for later use under acceleration
Blended Wing Body (BWB) - Future Of AviationAsim Ghatak
What Is Blended Wing Body, History of BWB, How Airplanes Fly, Aircraft Control Surfaces, Design and Structure of BWB, Advantages and Disadvantages, Conventional aircraft vs. BWB, Future Scope and Challenges
The Secret To Super-Charging Your Creativitysanglass
This talk explores techniques and practices for enhanced creative thinking using EXTERNAL and INTERNAL resources. Attendees will walk away with tangible creative exercises they can use and practice daily to generate more robust ideas and solutions faster.
Numerical simulation of inlet for turbine assisted ramjeteSAT Journals
Abstract
The ramjet engine performs faster than a Turbojet Engine at higher Mach numbers, but the engine can’t start with the own power
itself. The starting thrust must be attained by additional thrust producing devices like solid rocket boosters. The more reasonable
solution to overcome the starting problem is the integration of ramjet engine with turbojet engine, which leads to the Turboramjet.
This work describes some challenges in the design of an inlet for turbo-ramjet. Since it is a critical component, its design
has important effects on the overall performance of the engine. Here this work deals with a design of a turbo ramjet inlet and an
analysis for its optimization. Our aim is to reduce total pressure loss and entropy rise. A design of turbo-ramjet intake is made
with CATIA as well as a complete engine for better understanding. Gambit is used to mesh the geometry while ANSYS 14 is used
to perform the analysis for design optimization.
Key Words: Ramjet, Inlet, Turbine assisted, Subsonic and Supersonic Diffuser.
THIS PPT CONTAINS WHAT IS MEANT BY THE VIRTUAL MANUFACTURING AND APPLICATION AND DRAWBACKS ,
AND IT CONTAINS ABOUT HOW IT IS REALISED USED IN PRESENTSCENARIO.
Aircraft Design : Business Jet: Design of Wing spar, Power plant System & Eng...Prakul Mittal
This was my degree thesis where I designed an intercontinental transonic business jet which was capable of carrying up-to 15 passenger with range of 6500 Km, with in the supervision of various experienced supervisor.
Hybrid pneumatic engine with exhaust heat recoveryLiviu Giurca
The invention relates to a four-stoke hybrid pneumatic engine of the type ensuring energy recovery, which can be used for road motor vehicles or other transportation means with a view to reducing the fuel consumption and emissions which are deemed to cause the greenhouse effect. According to the invention, the hybrid pneumatic engine has a number of cylinders which are of the conventional type and at least one modified cylinder operating an active valve actuated by a mechatronic system.
A kinetic energy recovery system (often known simply as KERS, or kers) is an automotive system for recovering a moving vehicle's kinetic energy under braking. The recovered energy is stored in a reservoir (for example a flywheel or high voltage batteries) for later use under acceleration
Blended Wing Body (BWB) - Future Of AviationAsim Ghatak
What Is Blended Wing Body, History of BWB, How Airplanes Fly, Aircraft Control Surfaces, Design and Structure of BWB, Advantages and Disadvantages, Conventional aircraft vs. BWB, Future Scope and Challenges
The Secret To Super-Charging Your Creativitysanglass
This talk explores techniques and practices for enhanced creative thinking using EXTERNAL and INTERNAL resources. Attendees will walk away with tangible creative exercises they can use and practice daily to generate more robust ideas and solutions faster.
Numerical simulation of inlet for turbine assisted ramjeteSAT Journals
Abstract
The ramjet engine performs faster than a Turbojet Engine at higher Mach numbers, but the engine can’t start with the own power
itself. The starting thrust must be attained by additional thrust producing devices like solid rocket boosters. The more reasonable
solution to overcome the starting problem is the integration of ramjet engine with turbojet engine, which leads to the Turboramjet.
This work describes some challenges in the design of an inlet for turbo-ramjet. Since it is a critical component, its design
has important effects on the overall performance of the engine. Here this work deals with a design of a turbo ramjet inlet and an
analysis for its optimization. Our aim is to reduce total pressure loss and entropy rise. A design of turbo-ramjet intake is made
with CATIA as well as a complete engine for better understanding. Gambit is used to mesh the geometry while ANSYS 14 is used
to perform the analysis for design optimization.
Key Words: Ramjet, Inlet, Turbine assisted, Subsonic and Supersonic Diffuser.
THIS PPT CONTAINS WHAT IS MEANT BY THE VIRTUAL MANUFACTURING AND APPLICATION AND DRAWBACKS ,
AND IT CONTAINS ABOUT HOW IT IS REALISED USED IN PRESENTSCENARIO.
Aircraft Design : Business Jet: Design of Wing spar, Power plant System & Eng...Prakul Mittal
This was my degree thesis where I designed an intercontinental transonic business jet which was capable of carrying up-to 15 passenger with range of 6500 Km, with in the supervision of various experienced supervisor.