Michael Lam

US Patent:

7086039, Aug 1, 2006

Filed:

Nov 13, 2002

Appl. No.:

10/293457

Inventors:

Michael Shungkai Lam - Milpitas CA, US

Assignee:

Sun Microsystems, Inc. - Santa Clara CA

International Classification:

G06F 9/44

US Classification:

717136

Abstract:

A method of translating computer source code into optimized object code. The computer source code contains a first label statement defining a first label, a second label statement defining a second label, a third label statement defining a third label, and a computed goto statement for instructing a computer to branch to the first label or to the second label, but not to the third label. The method includes generating a list of labels contained within at least a portion of the computer source code. The list of labels includes the first label and the second label, but not the third label. The method also includes translating the computer source code into an intermediate language. The translation of the computer source code includes translating the computed goto statement into an indirect goto statement within the intermediate language. The method also includes generating object code that includes the first label and the second label but does not include the third label.

US Patent:

8539393, Sep 17, 2013

Filed:

Sep 23, 2011

Appl. No.:

13/244070

Inventors:

James C Word - Portland OR, US
Konstantinos G Adam - Belmont CA, US
Michael Lam - Sunnyvale CA, US
Sergiy Komirenko - Cupertino CA, US

Assignee:

Mentor Graphics Corporation - Wilsonville OR

International Classification:

G06F 17/50

US Classification:

716 54, 716 51, 716 52, 716 53, 716 55

Abstract:

Disclosed are techniques for simulating and correcting the mask shadowing effect using the domain decomposition method (DDM). According to various implementations of the invention, DDM signals for an extreme ultraviolet (EUV) lithography mask are determined for a plurality of azimuthal angles of illumination. Base on the DDM signals, one or more layout designs for making the mask may be analyzed and/or modified.

US Patent:

20130334363, Dec 19, 2013

Filed:

Jun 7, 2011

Appl. No.:

13/702521

Inventors:

Michael Lam - Los Altos Hills CA, US

International Classification:

B64C 13/28
B64C 9/14

US Classification:

244 993

Abstract:

An aircraft control system is presented. The system includes a wing including a flap track, and a shuttle connected to the flap track and configured to slide along a length of the flap track. The system includes a flap panel pivotally attached to the shuttle at a flap pivot. The flap panel is configured to rotate about the flap pivot. When the shuttle is deployed along a length of the flap track, the shuttle is configured to prevent rotation of the flap panel about the flap pivot, and when the shuttle is withdrawn into a stowed position, the shuttle is configured to allow the flap panel to rotate about the flap pivot.

US Patent:

20140001313, Jan 2, 2014

Filed:

Nov 15, 2011

Appl. No.:

13/885630

Inventors:

Michael Lam - Los Altos Hills CA, US

International Classification:

B64C 13/04
B64C 13/28

US Classification:

244221

Abstract:

A mechanical control mixer configured to couple to an aircraft is provided. An axle is mounted to a frame of the mechanical control mixer, and a barrel is configured to rotate about the axle. A central rod is disposed within the barrel. The central rod is configured to rotate with respect to the barrel. A roll control input is connected to the central rod. The roll control input is configured to cause the central rod to rotate within the barrel. Output control rods are connected to the central rod. The output control rods are connected to at least one control surface of the aircraft. An air brake input is connected to the barrel. The air brake input is configured to cause the barrel to rotate about the axle to move at least one of the output control rods

US Patent:

59145013, Jun 22, 1999

Filed:

Aug 27, 1998

Appl. No.:

9/141389

Inventors:

William K. Antle - Sunnyvale CA
Michael K. Lam - San Jose CA
James W. Stewart - San Jose CA

Assignee:

Hewlett-Packard Company - Palo Alto CA

International Classification:

H01L 3300
H01L 2715
H01L 3112

US Classification:

257 99

Abstract:

A light-emitting diode assembly incorporates a power shunting element that provides electrical over-stress protection to a light-emitting diode (LED) and prevents damage to the LED from electrostatic discharge (ESD). The power shunting element is coupled in parallel to the LED within the LED assembly and protects the LED by diverting electrical current from the LED and limiting the voltage across the LED to a clamp voltage when a threshold voltage across the LED is exceeded.

US Patent:

20170285490, Oct 5, 2017

Filed:

Mar 29, 2017

Appl. No.:

15/472364

Inventors:

- Wilsonville OR, US
Michael Lam - Sunnyvale CA, US

International Classification:

G03F 7/20

Abstract:

Disclosed are techniques for correcting the EUV crosstalk effects. Isolated mask feature component diffraction signals associated with individual layout feature components are determined based on a component-based mask diffraction modeling method such as a domain decomposition method. Mask feature component diffraction signals are then determined based on the isolated mask feature component diffraction signals, layout data and predetermined crosstalk signals. Here, the predetermined crosstalk signals are derived based on mask feature component diffraction signals computed using an electromagnetic field solver and the component-based mask diffraction modeling method, respectively. The mask feature component diffraction signals are then used to process layout designs.

US Patent:

20160161949, Jun 9, 2016

Filed:

Jul 25, 2014

Appl. No.:

14/907067

Inventors:

Michael LAM - Los Altos Hills CA, US
Greg COLE - Bend OR, US
- Los Altos Hills CA, US

International Classification:

G05D 1/00
B64C 9/20
G05D 1/08
B64C 13/38
B64C 9/04

Abstract:

An aircraft includes a wing. The wing includes an aileron pivotally connected to a trailing edge of the wing, and a Lam aileron pivotally connected to the trailing edge of the wing. The aircraft includes a motor connected to the Lam aileron and configured to rotate the Lam aileron. The aircraft includes a controller configured to detect a deflection of the aileron from a neutral position, calculate a target deflection for the Lam aileron using the deflection of the aileron, and cause the motor to rotate the Lam aileron to the target deflection.

US Patent:

20150176005, Jun 25, 2015

Filed:

May 22, 2013

Appl. No.:

14/403103

Inventors:

Christopher K. GLASS - San Diego CA, US
Michael G. ROSENFELD - San Diego CA, US
Wenbo LI - San Diego CA, US
Michael t. LAM - La Jolla CA, US
- Carlsbad CA, US
- Oakland CA, US

Assignee:

The Regents of the University of California - Oakland CA
Isis Pharmaceuticals, Inc. - Carlsbad CA

International Classification:

C12N 15/113

Abstract:

Disclosed herein are methods and compounds for inhibiting gene expression by inhibiting enhancer RNAs (eRNAs). Such methods and compounds are useful for reducing expression of certain genes, many of which are associated with a variety of diseases and disorders.

Address:

5411 Cranston Ct, Sugar Land, TX 77479

VIN:

4T1BE46K29U416000

Make:

TOYOTA

Model:

CAMRY

Year:

2009

Address:

2000 Smith St, Houston, TX 77002

VIN:

1D8GU28KX7W640312

Make:

DODGE

Model:

NITRO

Year:

2007

Author:

Michael Lam

ISBN #:

0471582867