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Company Information:

Company Name:
Spytek Aerospace Corporation
Address:
450 Frontier Way, Unit D
Bensenville, IL 60106-1170
Phone:
(630) 595-9133
URL:
N/A
EIN:
363723591
DUNS:
615345329
Number of Employees:
5
Woman-Owned?:
No
Minority-Owned?:
No
HUBZone-Owned?:
No

Commercialization:

Has been acquired/merged with?:
N/A
Has had Spin-off?:
N/A
Has Had IPO?:
N/A
Year of IPO:
N/A
Has Patents?:
N/A
Number of Patents:
N/A
Total Sales to Date $:
$ 0.00
Total Investment to Date $
$ 0.00
POC Title:
N/A
POC Name:
N/A
POC Phone:
N/A
POC Email:
N/A
Narrative:
N/A

Award Totals:

Program/Phase Award Amount ($) Number of Awards
SBIR Phase I $598,998.00 6
SBIR Phase II $2,174,598.00 3

Award List:

Advanced Combustor Designs Utilizing Inlet Swirl for High Acceleration of Gravity (G) Combustion

Award Year / Program / Phase:
2007 / SBIR / Phase I
Award Amount:
$99,169.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Abstract:
The recent incorporation of high g combustor designs in gas turbine engines at Spytek Aerospace has presented the need for the further optimization of the compressor/combustor interface (i.e. diffuser). Legacy combustor designs remove the inherent swirl out of the gas stream at the compressor exit,… More

Demonstration of Inter-Turbine Burners for Part-Power Fuel Efficiency Improvements

Award Year / Program / Phase:
2007 / SBIR / Phase I
Award Amount:
$99,907.00
Agency / Branch:
DOD / OSD
Principal Investigator:
Abstract:
Gas turbine engines using multistage turbine sections have the inherent disadvantage of temperature loss through the turbine section. This occurs when each successive turbine stage extracts energy from the superheated mass airflow. The result is limited energy potential due to the first stage… More

Demonstration of Inter-Turbine Burners for Part-Power Fuel Efficiency Improvements

Award Year / Program / Phase:
2008 / SBIR / Phase II
Award Amount:
$749,907.00
Agency / Branch:
DOD / OSD
Principal Investigator:
Abstract:
Advanced turbojet and turboshaft engines will be required to support future Unmanned Air Vehicle (UAV) missions which require a significant amount of time at cruise conditions to achieve a primary objective of increased range and time-on-station. Inter Turbine Burner (ITB) technology is the most… More

Integrated Power Generation for Small Unmanned Vehicles

Award Year / Program / Phase:
2008 / SBIR / Phase I
Award Amount:
$99,969.00
Agency / Branch:
DOD / OSD
Principal Investigator:
Abstract:
The ever increasing utilization of unmanned air, ground and maritime vehicles has dictated the need for the DoD to more effectively integrate the generation of electrical power with the propulsion engine associated with unmanned vehicles. This issue applies equally to turbine and IC engines. The… More

Advanced Combustor Designs Utilizing Inlet Swirl for High Acceleration of Gravity (G) Combustion

Award Year / Program / Phase:
2008 / SBIR / Phase II
Award Amount:
$749,699.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Abstract:
Spytek Aerospace will soon become a low cost supplier of small high performance gas turbines for expendable UAV military operations, university research centers and hobbyists. During Phase I Spytek Aerospace analytically examined and experimentally assessed two 'swirl-maintained' diffuserless high… More

Marine Inter Turbine Burner Equiped Turboshaft Engine for Combatant Craft Increased Payload

Award Year / Program / Phase:
2010 / SBIR / Phase I
Award Amount:
$69,962.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Abstract:
Our twin spool Inter Turbine Burner (ITB) equipped turbine engine is throttleable between 50 Hp to 700 Hp with a weight-to-power ratio (including gearbox) approaching .50 and possesses multi-fuel capability. A demonstration of this unique turbine technology, hybrid capable, marine applications is… More

On Demand Oil Supply

Award Year / Program / Phase:
2012 / SBIR / Phase I
Award Amount:
$80,000.00
Agency:
DOD
Principal Investigator:
Christopher Spytek, President – (630) 595-9133
Abstract:
The need to optimize gas turbine engine performance, coupled with"electrification"of aircraft systems, as on the Lockheed F35 and Boeing 787 , in order to maximize efficiency and flexibility, created an opportunity to develop a"smart"electrically driven lubrication system for gas… More

Multi-ITB-Turbo Fan for Advanced Propulsion and Power Concepts for Large Size Class Unmanned Aerial Systems (UAS), Equipped with Variable Turbine

Award Year / Program / Phase:
2013 / SBIR / Phase I
Award Amount:
$149,991.00
Agency:
DOD
Principal Investigator:
Christopher J. Spytek, President – (630) 595-9133
Abstract:
ABSTRACT: There is an urgent Air Force need for an advanced cycle turbo-fan for UAV applications. Spytek Aerospace proposes a 2-ITB, 500 LBT turbo-fan engine equipped with ITB driven fan capable of running a generator, thru a second ITB in variable modes for additional power on demand and at high… More

Multi-ITB-Turbo Fan for Advanced Propulsion and Power Concepts for Large Size Class Unmanned Aerial Systems (UAS), Equipped with Variable Turbine

Award Year / Program / Phase:
2014 / SBIR / Phase II
Award Amount:
$674,992.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Christopher Spytek, President – (630) 595-9133
Abstract:
ABSTRACT: With the roll of UAV"s becoming more complex, and their use more widespread, tactical requirements for performance, reliability, maintainability, supportability, and most recently low cost, have created the need for an advanced cycle propulsion system. Such an engine, must address… More