Abstract: A paint brush having an adhesive attachment that includes an engagement of a mass of adhesive within one or more pockets in a lower portion of the handle and an engagement of the mass of adhesive with an internal surface of the ferrule to form a permanent assembly. At least one flow passage fluidly connects with the pocket(s) to facilitate and/or permit flow of the adhesive into the pocket(s) during manufacturing of the paint brush. In addition, the paint brush may include an elongated upper portion having a rigid internal spine that is overlayed and surrounded with a more flexible grip.

Abstract: An electric power apparatus includes a main planar body having a circular opening that supports a brushless direct-current (BLDC) motor. The motor includes a stator, a rotor, a motor spindle extending through the circular opening, a first end cap formed on a first side of the stator and mounted on the main planar body; and a second end cap formed on a second side of the stator and secured to the first end cap to form a substantially watertight seal around the stator and the rotor. A ratio of a maximum power output of the motor when powered by at least one battery pack to a height of the motor as measured from an upper surface of the main planar body to a top surface of the motor is greater than or equal to approximately 34 watts/mm.

Abstract: An electric motor is provided including a stator, a rotor, a motor spindle coupled to the rotor and extending along a center axis, a first end cap formed on a first side of the stator, a second end cap formed on a second side of the stator and secured to the first end cap to form a first compartment around the stator and the rotor, an electro-magnetic brake module disposed on a side of the second end cap opposite the stator and engaged with the motor spindle, and a motor cover mounted on the second end cap to form a second compartment around the electro-magnetic brake module. The first end cap, the second end cap, and the motor cover form a substantially watertight seal around the stator, the rotor, and the position sensor assembly.

Abstract: ABSGAM is a computer model developed to predict the maximum sortie generation capability of aircraft operating from a typical USAF air base. The model allows the user to easily change input parameters to evaluate their effect on: (1) aircraft sortie rates, (2) cumulative sorties generated, (3) payload launched, and (4) material personnel required to support the air base operation. ABSGAM simulates (1) an air-base-attack and recovery, (2) reduced payload operations, (3) reduced maintenance capability, (4) extended turn-around time, and (5) aircraft attrition (both air and ground). Program input has been minimized for ease of use. Program output is available in tabular and graphical form. This model was developed as part of a technology assessment.