USA flag logo/image

An Official Website of the United States Government

Company Information:

Company Name:
Techniweave, Inc.
Address:
P.O. Box 6314
Rochester, NH 03868
Phone:
N/A
URL:
N/A
EIN:
N/A
DUNS:
N/A
Number of Employees:
42
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 $366,005.00 6
SBIR Phase II $1,193,285.00 2

Award List:

MATERIAL AND PROCESS DEVELOPMENT FOR THE AYPEX BRAIDING METHOD

Award Year / Program / Phase:
1985 / SBIR / Phase I
Award Amount:
$45,750.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
James A Crawford Jr
Abstract:
N/a

MATERIAL AND PROCESS DEVELOPMENT FOR THE AYPEX BRAIDING METHOD

Award Year / Program / Phase:
1986 / SBIR / Phase II
Award Amount:
$445,000.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
James A Crawford Jr
Abstract:
This proposal describes an effort to implement the aypex braiding process. work to be conducted includes weave design, fabrication demonstration, impregnation and test and evaluation.

A NOVEL APPROACH FOR FILTRATION OF DIESEL ENGINE EXHAUST

Award Year / Program / Phase:
1992 / SBIR / Phase I
Award Amount:
$50,000.00
Agency:
EPA
Principal Investigator:
James A Crawford Jr , Principal Ivestigator
Abstract:
The clean air act requires that certain exhaust emissions standards be met by heavy duty trucks and busses (class 8 vehicles) powered by diesel engines. the limits set for 1998 can only be met thru the use of exhaust treatment devices. a novel woven ceramic yarn filter capable of high temperature… More

Integrally Woven Lightweight High Temperature Structures

Award Year / Program / Phase:
1993 / SBIR / Phase I
Award Amount:
$51,891.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Jean Francois Lecostaouec
Abstract:
A new textile process has been developed by Techniweave that employs multidirectional weaving in the fabrication of integrally woven, net shaped, complex components. The process has been demostrated manually and has been shown through design of equipment to be feasible for an automated system. The… More

Affordable High Performance Airframe Concepts

Award Year / Program / Phase:
1994 / SBIR / Phase I
Award Amount:
$79,075.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Keith Burgess
Abstract:
N/a

Affordable High Performance Airframe Concepts

Award Year / Program / Phase:
1995 / SBIR / Phase II
Award Amount:
$748,285.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Keith Burgess
Abstract:
A unique textile process has been developed by Techniweave that employs multi-directional weaving. The process has been adapted to the fabrication of complex confirgurations that are potentially applicable as composite fittings in several areas within future aircraft designs. Lockheed Aircraft… More

Lightweight Composite Sandwich Structure for Navy Aircraft

Award Year / Program / Phase:
1996 / SBIR / Phase I
Award Amount:
$69,977.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Keith E. Burgess
Abstract:
Today, the majority of sandwich structures on aircraft involve a honeycomb and/or foam core with adhesive bonded face sheets. But, there are problems associated with conventionally cored composites. Honeycomb cored composites are expensive and vulnerable to a variety of environmental threats and… More

Woven Hybrid Inserts for Lightweigt Affordable Aircraft Structures

Award Year / Program / Phase:
1997 / SBIR / Phase I
Award Amount:
$69,312.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Keith E. Burgess
Abstract:
The latest generation of three dimensionally reinforced carbon/epoxy composites have demonstrated the ability to carry significantly higher ultimate loads than conventional laminated composites in structural configurations such as T-sections. The failure modes of these composites are complex… More