2016
Aerospace & Defense

*State of the Art, Novel Technology, Featured Project Development / Space, Satellite and Habitat, Power-Plant, Generator, Self-Feed Unit; H2O => HHO => H2O => HHO => Etc... *4 Systems All in One Unit, One By One, Plus Four-4 Projects added One to Other; *·1-Gearturbine, ·2-Imploturbocompressor, ·3-Dynamic Generator, ·4-Electrolysis System:

·1-GEARTURBINE; Rotary-Turbo-InFlow Tech,Have the similar basic system of the Aeolipilie Heron Steam Turbine device from Alexandria 10-70 AD * With Retrodynamic = DextroRPM VS LevoInFlow + Ying Yang Way Power Type - Non Waste Looses *8X/Y Thermodynamic CYCLE Way Steps. 4 Turbos, Higher efficient percent. No blade erosion by sand & very low heat target signature Pat:197187IMPI MX Dic1991 Atypical Motor Engine Type.

·2-IMPLOTURBOCOMPRESSOR; One Moving Part System Excellence Design - ...

Adversaries threaten multiple High Altitude EMP (HEMP) attacks initially sparing human life, crippling power, communications and High Frequency (HF) backup disaster response networks for hours. HEMP is less disruptive between surviving Low Frequency (LF) radio stations. HEMP response networks comprising small two-way low data rate LF relay stations similar to Air Force's retired 1970's Ground Wave Emergency Network are proposed to assure timely damage reports from the field critical to resources management. More, smaller, less expensive stations can also reuse existing HEMP protected HF transceivers.

Size, complexities, costs of LF terminals increase with decreasing frequency and ground wave communications distances decrease with increasing frequency. A sweet spot is currently unoccupied Aeronautical Navigation spectrum between 190 and 198 kHz, ...

The fluid dynamical boundary layer is fluid volume partially carried along by a moving body, due to adhesion to the body – then between molecules in the layer. Dependencies on velocity, body shape, fluid density, viscosity and surface characteristics affect how fluid behaves within this layer and defines Flow Condition, approximately predicted by nondimensional Reynolds Numbers. These associate with Laminar, Transitional, Reattached and Separated flow conditions, which affect Drag Coefficient.

Factors contributing to boundary layer growth involve boundary layer shear, which induces flow-perpendicular pressure differential gradients and flow curvature via Bernoulli Effect, vortical flow patterns, eddies and pressure anomalies.

Most drag reduction is passive – streamlining, boundary layer shedding, vortex mitigation and inducing reattached flow.

Tollmien-Schlichting Waves are inherent in boundary layers, ...

A Novel High Efficiency Variable Inlet Area Propulsor

The aircraft industry continues to search for a single aircraft capable of both high-speed cruise and efficient take-off and landing. Yet nearly all propulsion systems with nacelle inlets that fly today operate in a compromised state with at least one important flight condition existing in a sub-optimal state. In low speed flight, the inlets are often too constricted, in high speed flight, spillage often occurs. Thomas International, Inc., proposes a solution to the problem caused by the conflicting needs of highly efficient low speed lift related to propulsion versus efficient high-speed cruise with minimum spillage drag cruise with advanced technology propulsion units, the adjustable size inlet system, ASIS.

The ASIS propulsion ...

My name is Saugat and I am from Nepal. My project entitled “Modification in aircraft wing to increase lift” is theft from the engineering of nature seeing birds flying around the sky. Like humans, birds are the perfect engineering creation of nature.

While trying to think about the modification in the aircraft wing I thought about the bird's wings and developed a similar structure. I found out that the lift produced by such wings are better than the wings that the recent aircraft use. It’s because the highly pressurized air below the surface of the wings gets less area to give the lift force. As a result the overall lift increases. Using this mechanism we not only ...

The Aerospace Integrated Bearing is a design that can only be fabricated by additive manufacturing and which exploits most of the benefits of this technology.

We have created an optimized and customizable support for space that can rotate in the 3 axes and it can be manufactured ALL in just 1 step. It does not need any assembly and still contains a ball-bearing inside the support.

The application of this design is a mechanism to orientate the solar panels of a satellite.

Current supports in most satellites only deploy the panels to a fixed position with a hinge mechanism. We performed a holistic approach addressing structural integrity, functionality, material, energy consumption and assembly simplicity to ...

Take the sky with you leaving Earth.

Earth's atmosphere is a unique substance that people are looking for on other planets vainly. This light blue veil gently enveloping Earth gives us clouds of dream's star. How to take the sky with itself?

Aerogel will help us. Aerogel is a material that is 98.2% air. Aerogel has a porous solid network that contains air pockets, with the air pockets taking up the majority of space within the material. The lack of solid material allows aerogel to be almost weightless. The piece of the sky "Aerogel" in the form of the cylinder is placed in the aerographite capsule and goes to the stars. Black aerographite visually merges with black space. ...

Application of the Biefeld Brown Effect

In 1923 Professor Paul Biefeld and his student Thomas Townsend Brown discovered this effect during the test of a new type of capacitor. Basically the Biefeld Brown effect is electro gravitation. If you have a flat disk capacitor with a good dielectric like Barium Strontium Titanate (BaSrTiO3) and apply high voltage to the plates a directional force normal to the plates will be generated according to the formula developed by Musha Takaaki from Japan.

Eg=-8.62 x10-11*Z*(er) ^0.5*E

Where Eg is the acceleration obtained, Z is the atomic number of the dielectric, er is the relative permittivity of the dielectric and E is the Electric field through the dielectric given by ...

In our project, we propose an innovative software solution to the problem of electrical arcing risk prediction in high-voltage on-board electronic equipment intended for long-term self-contained use, like spacecraft conditions. As modern on board equipment is not vacuumed the appearance of arcing leads to considerable damages due to high energetic output from arcs. In spacecraft, this problem has been actual since 1995 when Boeing Satellite Systems offered the BSS 702 platform with high-voltage bus connected to 100 V stabilized power source. Possible further increase of operating voltages (e.g. due change in standard) will only escalate the problem.

Arcing simulation is a monumental challenge because it represents an attempt of numerical solution to the multiscale discharge plasma problem. The main ...

The easy to fly Fying Segway is a personal electric octa-copter with computer assisted stabilization. It has many uses. It can be flown manually or pre-programmed to fly autonomously navigating by GPS guidance. It can autonomously fly to any location and then be used to return rescue injured flyers & soldiers behind enemy lines, lost hikers, climbers. and flood victims.

It can go around town, fly across hills, valleys, streams. lakes, and even jump mountains. It can be an observation platform, weapon platform, supply delivery system, personal transportation vehicle, and handicapped mobility system. Two of several configurations, (A) Handlebar Control and (B) Body Tilt Control are illustrated.

In configuration (A), a man sits in a swinging chair ...

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