US4586387A — Flight test aid

Claim 1

Independent Claim 166 words

A flight test aid comprising means to measure force that is applied by a pilot to the control column of an aircraft to adjust the ailerons and elevators while manoeuvering the aircraft in flight, and having a finger force sensor, a palm force sensor, display means to indicate force on the said sensors, and characterised by support means adapted to be positioned on the hand of a pilot to locate the said sensors between the hand of a pilot and the control column, the said means being arranged to locate the said sensors on substantially opposite sides of the said control column when the pilot grasps the control column, and including an electrical signal differencer connected between the said sensors and the said display means, and means in the said signal differencer to subtract signals proportional to the force generated in one of the said sensors from that generated in the other said sensor to cause the said display means to record only the resultant force.

Claim 2

Dependent Claim 166 words

A flight test aid comprising means to measure force that is applied by a pilot to the control column of an aircraft to adjust the ailerons and elevators while manoeuvering the aircraft in flight, and having a finger force sensor, a palm force sensor, display means to indicate force on the said sensors, and characterised by support means adapted to be positioned on the hand of a pilot to locate the said sensors between the hand of a pilot and the control column, the said means being arranged to locate the said sensors on substantially opposite sides of the said control column when the pilot grasps the control column, and including an electrical signal differencer connected between the said sensors and the said display means, and means in the said signal differencer to subtract signals proportional to the force generated in one of the said sensors from that generated in the other said sensor to cause the said display means to record only the resultant force.

Claim 3

Dependent Claim 74 words

A flight test aid according to claim 1 wherein said support means adapted to be supported on the hand of the pilot comprises a thumb with a heel, a palm and at least two middle fingers, characterised in that said finger force sensor is positioned on the two middle fingers of said support means and the said palm force sensor is positioned on the palm and heel of the thumb of said support means.

Claim 4

Dependent Claim 39 words

A flight test aid according to claim 2, including self-adhering sections on the support means, the said finger force sensor, and the said palm force sensor to allow selective positioning of the said sensors on the said support means.

Claim 5

Dependent Claim 69 words

A flight test aid according to claim 2, characterised in that the said finger force sensor and said palm force sensor each include a sensing fluid, a transducer arranged to change force units to electrical signals supported on a band, fluid lines between each said sensor and separate sections of said transducer, and amplifier and gain control means connected to receive the said electrical signals from the said transducer.

Claim 6

Dependent Claim 42 words

A flight test aid according to claim 1 characterised by self-adhering sections on the said support means and the said finger force sensor and the said palm force sensor to allow selective positioning of the said sensors on the said support means.

Claim 7

Dependent Claim 68 words

A flight test aid according to claim 5, characterised in that the said finger force sensor and said palm force sensor each include a sensor fluid, a transducer arranged to change force units to electrical signals supported on a band, fluid lines between each said sensor and separate sections of said transducer, and amplifier and gain control means connected to receive said electrical signals from the said transducer.

Claim 8

Dependent Claim 68 words

A flight test aid according to claim 1, characterised in that said finger force sensor and said palm force sensor each include a sensing fluid, a transducer arranged to change force units to electrical signals supported on a band, fluid lines between each said sensor and separate sections of said transducer, and amplifier and gain control means connected to receive the said electrical signals from the said transducer.

Claim 9

Dependent Claim 20 words

A flight test aid according to claim 7 in which the said display means are mounted on the said band.

Claim 10

Dependent Claim 29 words

A flight test aid according to claim 8 characterised by said band being mounted on a wrist part of said support means, said support means including a power source.

Claim 11

Dependent Claim 21 words

A flight test aid according to claim 7 in which the said display means are mounted remotely of the said band.

Claim 12

Dependent Claim 156 words

A flight test aid for measuring forces applied between the hand of a pilot and a control column characterised by (a) a glove to fit the hand of a pilot and provide an interface between the said glove and the said control column, (b) a finger force sensor attached across the inside of the middle fingers of the said glove at the said interface, (c) a palm force sensor attached across the palm and the heel of the thumb of the said glove, at the said interface, (d) means to transfer force measurements from each said sensor to gain control means, (e) means to display the measurements of the said sensors from the said gain control means, and (f) a signal differencer interposed between the said gain control means and the said display means arranged to cancel by subtraction the signal proportional to the force of the grip of the pilot on the said control column.

Claim 13

Dependent Claim 156 words

A flight test aid for measuring forces applied between the hand of a pilot and a control column characterised by (a) a glove to fit the hand of a pilot and provide an interface between the said glove and the said control column, (b) a finger force sensor attached across the inside of the middle fingers of the said glove at the said interface, (c) a palm force sensor attached across the palm and the heel of the thumb of the said glove, at the said interface, (d) means to transfer force measurements from each said sensor to gain control means, (e) means to display the measurements of the said sensors from the said gain control means, and (f) a signal differencer interposed between the said gain control means and the said display means arranged to cancel by subtraction the signal proportional to the force of the grip of the pilot on the said control column.

Annuity Stage	Window Opens	Payment Deadline	Surcharge Period Until	Estimated Fee	Status
3.5 Years (Year 4)	1989-05-05	1989-11-04	1990-05-06	$2000.00	Window Closed / Lapsed
7.5 Years (Year 8)	1993-05-05	1993-11-04	1994-05-06	$3760.00	Window Closed / Lapsed
11.5 Years (Year 12)	1997-05-05	1997-11-04	1998-05-06	$7700.00	Window Closed / Lapsed

Flight test aid

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