SBIR-STTR Award

Electromagnetic Actuators for Flight Control Systems
Award last edited on: 4/30/02

Sponsored Program
SBIR
Awarding Agency
DOD : AF
Total Award Amount
$829,246
Award Phase
2
Solicitation Topic Code
AF95-228
Principal Investigator
Vatche Artinian

Company Information

AVCON - Advanced Controls Technology

5210 Lewis Road Suite 14
Agoura Hills, CA 91301
   (805) 865-0250
   N/A
   N/A
Location: Single
Congr. District: 33
County: Los Angeles

Phase I

Contract Number: F34601-95-C-0726
Start Date: 8/31/95    Completed: 2/28/96
Phase I year
1995
Phase I Amount
$79,968
AVCON has developed a highly efficient linear motor actuator (LMA) design that has already demonstrated performance that exceeds the power to volume ratio goal of 20 hp/ft3, when operated at high speeds than required for use in moving aircraft flight control surfaces. Additional engineering will be required to demonstrate the feasibility of achieving an equivalent power to volume ration to reduce operating speeds. This proposed Phase I effort would investigate the physical phenomena, equations, materials, and manufacturing techniques for our unique coaxial design to determine the feasibility of building an LMA with a power to volume ration of 20hp/ft3, capable of moving 13.75 inches at a no load rate of 7.3 inches per second, with a frequency response of 3 Hz, a maximum output force of 3,000 pounds, and a back drive force of less than 125 pounds at 1.0 inches per second. After it has been proven feasible to design and build an LMA capable of meeting these requirements, a conceptual design of the actuator and its control system will be developed, based on an input voltage of 270 VDC. The conceptual design will allow for basic parameters, other than the physical limitation of a 13.75 inch stroke, to be varied so that the design can be optimized. Preliminary heat generation calculations will be performed, and a heat rejection scheme will be developed for a maximum ambient temperature of 160 degrees F (71 C). A work plan for Phase II will be developed, wherein a more in-depth analysis and design will be performed, and the LMA (including control system) will be fabricated and tested.

Keywords:
Linear Actuator Linear Motor

Phase II

Contract Number: F34601-97-C-0024
Start Date: 11/14/96    Completed: 11/14/98
Phase II year
1997
Phase II Amount
$749,278
Under Phase I funding, AVCON developed three conceptual designs for candidate linear motor actuators (LMA), analyzed the performance characteristics of each, then compared the designs to select the most efficient LMA. The selected design configuration was shown to meet the following goals: (1) power to volume ratio goal of 20 hp/ft3, (2) capable of moving 13.75 inches at a no load rate of 7.3 inches per second, (3) a frequency response of 3 Hz, (4) a maximum output force of 3,000 pounds, and (5) a back drive force of less than 125 pounds at 1.0 inches per second. The proposed Phase II effort will develop the conceptual design chosen in Phase I into a fully engineered prototype and test the prototype to verify its performance under simulated flight conditions of varying load and speed conditions. A successful demonstration of the LMA under simulated flight conditions of varying load and speed conditions. A successful demonstration of the LMA under simulated flight conditions will contribute significantly to the advancement of the More Electric Aircraft program, in which the elimination of hydraulic systems in future military aircraft is a high priority.

Keywords:
Linear Actuator Linear Motor