Terence F Hall

US Patent:

20040046967, Mar 11, 2004

Filed:

Sep 11, 2002

Appl. No.:

10/241334

Inventors:

Terence Hall - Santa Monica CA, US

International Classification:

G01B011/14

US Classification:

356/614000

Abstract:

A Z-form position detector useful for ascertaining the position of Z-forms with respect to underlying composite structure. The device comprises an oscillating laser that generates a line projected onto the Z-form and composite structure at an angle. The line appears discontinuous due to the topography of the Z-form and composite structure. For example, the line is discontinuous at the edges of the Z-form. The device further comprises a sensor sensitive to the frequency of the laser. The sensor scans along the line until a discontinuity (i.e., a break in the line) is detected. Since the discontinuity corresponds to the edge of the Z-form, detection of the discontinuity allows the device to ascertain precise coordinates of a point on the edge of the Z-form. The device thus allows Z-pins to be driven into composite structure automatically for savings on time and cost.

US Patent:

20050270546, Dec 8, 2005

Filed:

Aug 11, 2005

Appl. No.:

11/201619

Inventors:

Terence Hall - Santa Monica CA, US

International Classification:

G01B011/14

US Classification:

356614000

Abstract:

A Z-form position detector useful for ascertaining the position of Z-forms with respect to underlying composite structure. The device comprises an oscillating laser that generates a line projected onto the Z-form and composite structure at an angle. The line appears discontinuous due to the topography of the Z-form and composite structure. For example, the line is discontinuous at the edges of the Z-form. The device further comprises a sensor sensitive to the frequency of the laser. The sensor scans along the line until a discontinuity (i.e., a break in the line) is detected. Since the discontinuity corresponds to the edge of the Z-form, detection of the discontinuity allows the device to ascertain precise coordinates of a point on the edge of the Z-form. The device thus allows Z-pins to be driven into composite structure automatically for savings on time and cost.

US Patent:

20060288553, Dec 28, 2006

Filed:

Jun 22, 2005

Appl. No.:

11/158400

Inventors:

Terence Hall - Santa Monica CA, US
Brian Hill - Torrance CA, US
William DeLeon - Buena Park CA, US
Bettie Marino - Hawthorne CA, US

International Classification:

B23Q 17/00

US Classification:

029407100, 029407050, 029432000

Abstract:

In accordance with the present invention, there is provided a method of inserting at least one Z-pin into a composite laminate for providing Z direction reinforcement thereto. The method comprises the initial step of positioning at least one Z-pin upon the composite laminate. Thereafter, an insertion force is applied to the Z-pin at a first level which is sufficient to commence an insertion process wherein the Z-pin is driven into the composite laminate at a first insertion speed. The insertion force applied to the Z-pin is continuously monitored, with the first insertion speed being reduced to a second insertion speed in response to a monitored increase in the insertion force from a first level to a second level.

US Patent:

20060288554, Dec 28, 2006

Filed:

Nov 22, 2005

Appl. No.:

11/284605

Inventors:

Terence Hall - Santa Monica CA, US

International Classification:

B23Q 17/00
B23P 11/00

US Classification:

029407100, 029432000, 029407010

Abstract:

In accordance with the present invention, there is provided a method of automatically verifying the acceptable insertion of at least one Z-pin into a composite laminate. The method comprises the initial step of positioning at least one Z-pin upon the composite laminate. Thereafter, an insertion force is applied to the Z-pin at a first level which is sufficient to commence an insertion process wherein the Z-pin is driven into the composite laminate at a first insertion speed. The insertion force applied to the Z-pin is continuously monitored, with the first insertion speed being reduced to a second insertion speed in response to a monitored increase in the insertion force from a first level to a second level. The application of the insertion force to the Z-pin is discontinued and the insertion process terminated in response to a monitored increase in the insertion force from the second level to a third level. To confirm an acceptable insertion, the reduction from the first insertion speed to the second insertion speed is verified, as is the increase of the insertion force to the third level.

US Patent:

20060288555, Dec 28, 2006

Filed:

Nov 29, 2005

Appl. No.:

11/288832

Inventors:

Terence Hall - Santa Monica CA, US
Jonathan Bartley-Cho - Arcadia CA, US

International Classification:

B23Q 17/00

US Classification:

029407100, 029432000, 029407010

Abstract:

In accordance with the present invention, there is provided a technique which may be used in conjunction with an automated Z-pin insertion process to automatically monitor the insertion energy applied to the Z-pins during the initial insertion phase of the automated insertion process, and compare it to an empirically derived value for good insertions, thereafter allowing the insertion process to continue to a predetermined additional insertion depth before terminating the process. The insertion energy is calculated by cumulatively summing the insertion force and multiplying it by the insertion time, thus yielding the cumulative energy. At a specified, predetermined insertion depth, the energy accumulation is stopped and the value at the initial insertion depth is stored and compared to an empirically derived value. If the value is less than the empirical value, the insertion energy is too low, thus indicating that either a partial grid insertion is being encountered or defective Z-pins are being inserted. Insertion is allowed to continue until another empirically derived second insertion depth is reached whereat the insertion is terminated. The second depth is necessary for the continued insertion of partial grids to ensure that the Z-pins are fully inserted. The second depth is a function of the laminate thickness to ensure full depth insertions.

US Patent:

60922729, Jul 25, 2000

Filed:

Oct 1, 1999

Appl. No.:

9/410816

Inventors:

Michael D. Durham - Ventura CA
Stewart G. Cramer - Northridge CA
Terence Hall - Santa Monica CA

Assignee:

North Grumman Corporation - Los Angeles CA

International Classification:

B23P 1700

US Classification:

294211

Abstract:

In accordance with the present invention, in an aircraft storage container which is used for the transport of cargo items, defines an enclosed interior compartment and includes a hatch for selectively accessing the interior compartment, there is provided an improvement of the aircraft storage container. The improvement is provided with a high strength flexible bag member disposed about a substantial portion of the interior compartment for distributing force in response to explosive forces emanating from cargo items within the bag member. The bag member includes an opening and is positionable within the interior compartment such that the opening is adjacent the hatch for allowing cargo items to be placed into and removed from within the bag member via the hatch and the opening. The improvement is further provided with a bag opening frame which is attachable to the opening of the bag member and formed to receive cargo items for storage within the bag member therethrough. The bag member includes multiple overlapping door frame folds which are disposed adjacent the bag opening frame for distributing force away from the bag opening frame in response to explosive forces emanating from cargo items within the bag member.

US Patent:

60192372, Feb 1, 2000

Filed:

Apr 6, 1998

Appl. No.:

9/055604

Inventors:

Michael D. Durham - Ventura CA
Stewart G. Cramer - Northridge CA
Terence Hall - Santa Monica CA

Assignee:

Northrop Grumman Corporation - Los Angeles CA

International Classification:

B65D 2514
B65D 8854
B65D 9032

US Classification:

220 16

Abstract:

In accordance with the present invention, in an aircraft storage container which is used for the transport of cargo items, defines an enclosed interior compartment and includes a hatch for selectively accessing the interior compartment, there is provided an improvement of the aircraft storage container. The improvement is provided with a high strength flexible bag member disposed about a substantial portion of the interior compartment for distributing force in response to explosive forces emanating from cargo items within the bag member. The bag member includes an opening and is positionable within the interior compartment such that the opening is adjacent the hatch for allowing cargo items to be placed into and removed from within the bag member via the hatch and the opening. The improvement is further provided with a bag opening frame which is attachable to the opening of the bag member and formed to receive cargo items for storage within the bag member therethrough. The bag member includes multiple overlapping door frame folds which are disposed adjacent the bag opening frame for distributing force away from the bag opening frame in response to explosive forces emanating from cargo items within the bag member.