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Abdul N Sitabkhan

from Arcadia, CA
Age ~85
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Also known as:
Abdul Farida Sitabkhan, Farida A Sitabkhan, Farida A Abdul, Abdul N
Phone and address:
434 Harvard Dr, Arcadia, CA 91007
Related to:
Margaret V Vellani, 37Yasmin A Sitabkhan, 48Amir M Sitabkhan, 43Rayeka M Sitabkhan, 76Manny KahnSaima Siddiqui, 42Sameena A Sitabkhan, 52Arif Sitabkhan, 49Siddiqui Zuhair, 71Farida A Sitabkhan, 78
Connected to:
Shaheen Sitabkhan, 47Krystal Sital, 37Ketsy K Sitanggan, 45Vikrant Sitani, 50Andria M Sitar, 63Kerry L Sitar, 80Melanie K Sitar, 65Sandra J Sitar, 78Steven M Sitar, 71Wendi J Sitara, 45

Abdul Sitabkhan Phones & Addresses

  • 434 Harvard Dr, Arcadia, CA 91007
  • 782 Island View Cir, Port Hueneme, CA 93041
  • 1738 Rutherford St, Anaheim, CA 92806
  • San Dimas, CA
  • Brea, CA
  • Baldwin Park, CA
  • San Jose, CA
  • Baldwin Park, CA
  • Westlake, OH

Work

Company: Ametek/ameron Jan 1990 Position: Business consultant

Education

Degree: Masters, Master of Science In Mechanical Engineering School / High School: University of Michigan 1960 to 1962 Specialities: Engineering

Industries

Airlines/Aviation

Resumes

Resumes

Abdul Sitabkhan Photo 1

Business Consultant

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Location:
434 Harvard Dr, Arcadia, CA 91007
Industry:
Airlines/Aviation
Work:
Ametek/Ameron
Business Consultant
Htl/Pacific Scientific Dec 1968 - Oct 1989
President
Education:
University of Michigan 1960 - 1962
Masters, Master of Science In Mechanical Engineering, Engineering

Business Records

Name / Title
Company / Classification
Phones & Addresses
Abdul N. Sitabkhan
Branch Manager
Ametek Ameron, LLC
Mfg Process Cntrl Instr Mfg Misc Products Mfg Aircraft Parts/Equip Engineering Services · Mfg Process Cntrl Instr Mfg Misc Products Mfg Aircraft Parts/Equip Engineering Services Mfg Surgical Appliances · Mfg& Dist Aviation Products
4750 Littlejohn St, Duarte, CA 91706
(626) 337-4640
Abdul N. Sitabkhan
Manager
Crafty Innovations, Inc
Nonclassifiable Establishments · Whol Flowers/Florist Supplies
4540 Littlejohn St, Duarte, CA 91706
2387 Buena Vis St, Duarte, CA 91010
Abdul N. Sitabkhan
President
SMLA INVESTORS, INC
4601 Littlejohn St, Baldwin Park, CA 91706
4601 Littlejohn St, Duarte, CA 91706

Publications

Us Patents

Self-Activated Fire Extinguisher

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US Patent:
7841420, Nov 30, 2010
Filed:
Sep 24, 2008
Appl. No.:
12/236679
Inventors:
Abdul Sitabkhan - Arcadia CA, US
Assignee:
X-Fire, LLC - Valencia CA
International Classification:
A62C 37/12
A62C 3/00
US Classification:
169 57, 169 51, 169 65
Abstract:
A self-activating fire extinguisher includes a pressure vessel having an outlet and containing a fire suppressant therein. A fusible material caps the outlet such that melting the fusible material allows escape of the fire suppressant from the pressure vessel. A deflector is associated with the pressure vessel for deflecting the fire suppressant escaping the pressure vessel onto a corresponding hazard.

Temperature Compensated Pressure Switch (Tcps)

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US Patent:
8443650, May 21, 2013
Filed:
Nov 30, 2007
Appl. No.:
11/948842
Inventors:
Abdul N. Sitabkhan - Arcadia CA, US
Michael A. Mallari - Alta Loma CA, US
Assignee:
Mass Systems, A Unit of Ameron Global, Inc. - Baldwin Park CA
International Classification:
G01F 25/00
US Classification:
73 173
Abstract:
A temperature compensated pressure switch (“TCPS”) with thermal lag compensation, trend indication, and forecast analysis. The TCPS has a first control unit, a pressure sensor connected to the first control unit outputting a first pressure data, a temperature sensor connected to the first control unit outputting a first temperature data, and a first storage unit connected to the first control unit storing: minimum and maximum pressure data corresponding to temperature data and rate of temperature change values. The first control unit can substitute a second temperature data, for the first temperature data for a period of time. The first control unit also outputs a first signal indicating the amount of material is acceptable when the first pressure data is above the minimum pressure data and outputs a second signal indicating the amount of material is unacceptable when the first pressure data is not above the minimum pressure data.

Self-Activated Fire Extinguisher

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US Patent:
20080087446, Apr 17, 2008
Filed:
Oct 17, 2006
Appl. No.:
11/550064
Inventors:
Abdul Sitabkhan - Arcadia CA, US
Assignee:
AMERON GLOBAL, INC. - Valencia CA
International Classification:
A62C 37/12
A62C 37/50
US Classification:
169 57, 169 74, 169 77, 169 89
Abstract:
An automatic fire extinguisher that is self-activated in the presence of specified temperature. The fire extinguisher includes a sealed pressure vessel having a fitting and a tube permitting access to the contents of the pressure vessel. A valve in the end of the tube includes a fusible alloy temperature sensor designed to melt or soften in the presence of heat and/or flame. Once the temperature sensor softens or melts, the contents of the pressure vessel are released through the valve thereby extinguishing the fire. A capillary tube is provided to charge the pressure vessel with fire suppressant agent and a pressurized gas.

Hermetically Welded Sealed Oxygen Cylinder Assembly And Method Of Charging

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US Patent:
20120111871, May 10, 2012
Filed:
Jul 16, 2010
Appl. No.:
13/383816
Inventors:
Abdul N. Sitabkhan - Arcadia CA, US
Michael A. Mallari - Alta Loma CA, US
Souvanh Bounpraseuth - Ontario CA, US
International Classification:
B60P 3/00
US Classification:
220562
Abstract:
An emergency oxygen system for aircraft passengers includes a hermetically welded sealed oxygen cylinder of stainless steel, a welded metal diaphragm sealing a discharge port and an extended hermetically sealed capillary tube for charging the cylinder with pressurized oxygen. A hollow piston cutter is driven to pierce the metal diaphragm as part of a first passageway delivering oxygen to the passenger. A second passageway delivers any leaking oxygen to a release port when the piston cutter is in position. A method of filling the cylinder includes welding to the cylinder a member having a metal diaphragm of a predetermined rupturable characteristic and using the open capillary tube to fill oxygen in the cylinder and subsequently crimping a portion of the capillary tube to provide a hermetic seal. A pressure gauge can be hermetically sealed to the bottom of the oxygen cylinder.

Temperature Compensated Annunciator

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US Patent:
55789935, Nov 26, 1996
Filed:
Nov 28, 1994
Appl. No.:
8/345929
Inventors:
Abdul N. Sitabkhan - Arcadia CA
James W. Tseng - La Canada CA
Assignee:
Autronics Corporation - Arcadia CA
Mass Systems Inc. - Baldwin Park CA
International Classification:
G08B 2100
US Classification:
340614
Abstract:
A solid state temperature compensated annunciator is disclosed. The solid state temperature compensated annunciator includes a pressure sensor for measuring a pressure of the fillant within a vessel and a temperature sensor for measuring the temperature of the fillant within the vessel. The solid state temperature compensated annunciator determines a pressure that the vessel would have if the vessel were filled with a predetermined amount of fillant, and compares the measured pressure to the determined pressure. If the measured pressure is below the determined pressure, a warning signal is issued.

Magnetic Pressure Indicator For A Container

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US Patent:
39461750, Mar 23, 1976
Filed:
Dec 3, 1973
Appl. No.:
5/421152
Inventors:
Abdul N. Sitabkhan - Monrovia CA
Assignee:
HTL Industries, Inc. - Pasadena CA
International Classification:
H01H 3532
US Classification:
200 83L
Abstract:
A temperature compensated pressure indicator adapted to be mounted within a pressure container includes a reservoir housing and housing member welded together to form a secondary pressure chamber. A bellows member is hermetically mounted within the secondary pressure chamber and communicates with the exterior pressure of the container. Mounted on the bellows member is a movable magnetic member adapted to slide on a hollow guide post as a result of any pressure differentials. A reed switch assembly is held stationary in the guide post by a pair of band springs. The switch assembly is electrically connected to a source of power and an external indicator such as a light. When the bellows member moves the magnetic member close to the switch assembly due to a pressure differential, the magnetic field closes the switch assembly to activate the light. The indicator is substantially non-responsive to wide variations in the ambient temperature.

Pressure Gauge Assembly

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US Patent:
41435451, Mar 13, 1979
Filed:
Jan 3, 1978
Appl. No.:
5/866371
Inventors:
Abdul N. Sitabkhan - Arcadia CA
Assignee:
HTL Industries, Inc. - Pasadena CA
International Classification:
B60C 2304
G01L 704
US Classification:
731468
Abstract:
A pressure gauge assembly for aircraft tires and the like having a helical coil bourdon tube sensor capable of indicating a pressure differential between a monitored source of pressure and a calibrated reference source of pressure. The reference pressure is applied to one surface of the bourdon tube coils while the monitored pressure is applied to the other surface of the coils. The resultant movement is a linear indication of any pressure differential. A valve assembly can be provided with the pressure gauge assembly to permit fluidic access to the monitored pressure. If the volume of the monitored pressure is variable such as an aircraft tire, the secondary source of calibrated pressure can be provided with a predetermined pressure relative to the normal tire pressure to compensate for any volumetric changes in the tire during operation. In an alternative embodiment, the bourdon tube can be used to monitor the pressure in a fire extinguisher for indicating any leaks. Advantageously, dials are provided for a visual inspection to determine a go or no-go situation.

Fire Metering Protection System For Aircraft

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US Patent:
20190151690, May 23, 2019
Filed:
Jun 17, 2016
Appl. No.:
16/310339
Inventors:
- Baldwin Park CA, US
Abdul N. Sitabkhan - Arcadia CA, US
Souvanh Bounpraseuth - Ontario CA, US
Michael A. Mallari - Rancho Cucamonga CA, US
International Classification:
A62C 3/08
A62C 35/13
A62C 99/00
Abstract:
A metering cargo fire inerting assembly is activated to supplement an initial release of fire extinguishing fluid into a cargo hold of an aircraft when a fire is detected during flight. The metering components of the fire inerting assembly control the temperature and pressure of the fire extinguishing fluid within a metering container. A heater element within the metering container controls temperature and pressure. A flow control metering orifice is immersed in a portion of the fire extinguishing fluid sealed by a hermetically sealed disc downstream of the metering orifice. A cutter with an internal fluid flow passageway can pierce the disc to release the fire extinguishing fluid under control of a timer attached to the metering container that can activate a pyrotechnic charge to drive the cutter for releasing the fire extinguishing fluid such as Halon 1301 to a discharge outlet for delivery to the cargo hold.
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Abdul N Sitabkhan from Arcadia, CA, age ~85 Get Report