2016
Aerospace & Defense

My design is of an aircraft named LA-95, which is constructed from an alloy of Lithium and Aluminum and has a double turbo fan system, along with Pratt and Whitney F119 engine network. Below mentioned, in detail are some of the changes designed which are developed differently from other jet engines to enable faster means of travel.

Compression Chamber :-
In most passenger aircraft the turbojet is an air breathing jet engine, usually used in aircraft. It consists of a gas turbine with a propelling nozzle. The gas turbine has an air inlet, a compressor, a combustion chamber, and a turbine (that drives the compressor). The compressed air from the compressor is heated by the fuel in the combustion ...

Problem Statement
Thrust developed by engines of an aircraft is used to propel it in a forward direction. Its size or wing size that produces the required lift force to fulfill the need to hover a plane against the force of gravity is proportional to payload or overall weight. But lift force is not responsible for forward motion of the aircraft or used during liftoff, cruising and landing that are the parts of flight and if an airplane runs on ground without requirement of lift force it will travel same distance in less time.

Solution Statement
A Road In The Air For Aircraft.
In this innovation, lift force has been used to thrust the vehicle and to increase the overall ...

If a school or office needed all rooms or just a room to be locked down and secured. simply press a button in the class or in the office. The automated door falls down (as shown in diagram). The door is made much like a standard bay door, with Kevlar backing behind the slats. This makes the door bullet proof for the active shooter emergency. The door falls and locks into place. Above the door on the outside is a 360 degree camera for the teacher to watch outside the room. Inside the room there is also a camera for the POLICE or admin to look inside and clear rooms without threats. This could also be incorporated into office ...

The project is connected with a new approach for drone range/operating time improvement by using an Ecological LPG powered onboard micro power genset.

The frame is contructed in a way that tubes incorporate LPG tank - shaped in a way not to influence the flight control. A spark ignition engine together with generator is located in the center to ensure a better flight control.

The energy balance is calculated in a way to allow a long distance flights without the necessity of using heavy high capacity batteries.

Project provides 2 possible ways of realizing the energy flow control - use of 2 separate low weight lithium battery packs swiched from charging mode - to supply continuously.

The Problem:
Conventional aircraft make use of elliptical wings to minimize drag. However, achieving
aircraft stability and control in conventional elliptical wings requires a strong adverse
yaw component in roll control (i.e., the aircraft will yaw the opposite direction with
application of roll control). Therefore, a vertical tail or some other method of direct yaw
control is required, such as split elevons for use as drag rudders. The use of elliptical
wings also results in a suboptimal amount of structure to carry the wing root bending
moments. To counteract these problems, engineers at NASA Armstrong Flight Research Center developed an innovative wing design that has proverse yaw to optimize aircraft efficiency.

A Novel Solution and How It Works: ...

There is exiguity and lots of difficulties in alternative methods which represent satellites services and its implements, according to the high cost of sending and operating satellites. Specifically in the fields of Telecommunications, Research, wild life, Geographic surveying, civilian spying and cities security. My innovation idea aims to provide a sustainable solutions for using satellites. I provide a new generation of things that could work as satellites. NIUTS is just the name of my invention; it is simply a self flying object that could fly inside Earth's atmosphere for a long period of time during to Earth gravity and wind forces, other characteristics.

NIUTS is a self flying object. That means it doesn't have any kind of fuel ...

This particular Nuclear Powered Aircraft uses heat generated during Nuclear Fission to generate steam from stored water.

The nuclear fission is performed on a low weight radioactive material like Iodine. The heat so released is used to convert water into steam, which in turn drives the turbine. the water is stored initially in water tank which is at level 1 in the plane, and later is generated by heating air to turn water vapor to water. the fission is controlled according to power demand. the turbine converts steam pressure energy to mechanical energy. this is directed towards the propellers by means of gears and transmission devices. there is an electric generator placed in level 2 which extracts electricity from ...

Introduction

Today space debris traffic is one of the most critical concerns for space researchers. The current population of space debris is divided into small fragmentation debris of about 42 %, satellite and rocket bodies debris of about 17 % and dead spacecraft debris of about 31 %. Most of the debris are concentrated mainly in Low Earth Orbit (LEO) and Geostationary Earth Orbit (GEO), which imposes a major threat for future space missions due to high risk of collisions with the active spacecraft.

According to Kessler’s syndrome, more and more debris will be produced due to continuous collisions among existing debris even if in future all launches into space are stopped. Therefore, removal of space debris ...

The new P.A.W.N. project (Pollutant Automated Wireless Node) is a significant and innovative part of the integrated hardware-software solution which embraces a wide scope of civil aviation environmental impact factors and is being developed to implement a sophisticated approach to environmental analysis on different scales: from local air quality and noise impact to on-cruise pollutant and greenhouse gas emission. The integrated solution is intended to assist in three main objectives of environmental analysis: 1) evaluation and quantification; 2) monitoring and forecasting; 3) mitigation and optimization. The motivation of this work is to improve and create methodologies and tools to meet modern standards and apply cutting-edge technologies for solving aviation related environmental problems and perform corresponding advanced analysis for ICAO/CAEP, ...

Passive method for flying objects detection

This idea for detection flying objects in atmosphere are going from probabilistic and statistical analysis of received cosmic radiation, usually perceived as “cosmic noise.”

Using a spreaded cosmic radiation directional receiver network and a central computer system for data analysis, in conjunction with previously received data, the location of a flying object can be determined with enough precision.

The receiver's antennas will sweep the sky in a coordinated syncronicity and the received data are sent to central computer for analysis and position determination.

The antennas are mobile (mechanical sweep) or fixed (electronic sweep).

The perturbation in a “constant” cosmic noise signal – statistical determined – are produced by ...

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