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Mark D Resendes

from La Mesa, CA
Age ~57
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Also known as:
Mark David Resendes, Mark L Resendes, Mark D Resenders, Mark S
Phone and address:
9450 Alto Dr, La Mesa, CA 91941
Related to:
Paul ResendesYukie OkazakiAudrey Resendes, 27Jared Resendes, 34
Connected to:
Adrianne P Resendez, 41Amy Resendez, 43Andrea M Resende, 35Andreia Resende, 30Angelena Resende, 37Angelina Resendez, 67Angelo Resendez, 51Antonio F Resende, 57Barbara L Resendes, 58Ben R Resendez, 42

Mark Resendes Phones & Addresses

  • 9450 Alto Dr, La Mesa, CA 91941
  • Spring Valley, CA
  • 2175 Mariposa Dr, Dixon, CA 95620
  • 1035 Mason Ct, Dixon, CA 95620 (707) 693-1095
  • Vacaville, CA
  • Fairfield, CA
  • Davis, CA
  • Alamogordo, NM
  • Stockton, CA

Work

Position: Project foreman

Education

Degree: Associate degree or higher

Resumes

Resumes

Mark Resendes Photo 1

Project Foreman

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Work:

Project Foreman

Publications

Us Patents

Parked Aircraft Power Cable Protection System And Method

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US Patent:
7572981, Aug 11, 2009
Filed:
Sep 14, 2005
Appl. No.:
11/227330
Inventors:
Scott Takayuki Koizumi - Fairfield CA, US
Brian Michael Piety - Vacaville CA, US
Folkert Fred Koch - San Ramon CA, US
Wolfgang Ott - Antioch CA, US
Dale Arnold Miller - Vacaville CA, US
Denise Marie Frazier - Pleasant Hill CA, US
Mark David Resendes - Dixon CA, US
Assignee:
Illinois Tool Works Inc. - Glenview IL
International Classification:
H01B 7/00
US Classification:
174111
Abstract:
A power delivery system for parked aircraft includes protective rings on the power cords. These protective rings protect the power cord jackets from wear and facilitate movement of the power cords across the ground. The rings may be configured for securement to the cable so as to compress the insulative jacket of the cable somewhat, thereby firmly maintaining the rings in place on the cable. The rings may be formed of two identical elements that are joined to envelope the cable. The rings may accommodate both round insulated cable, as well as bundled cable.

Preconditioned Air Connector Assembly For Aircraft

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US Patent:
7984930, Jul 26, 2011
Filed:
Nov 3, 2006
Appl. No.:
11/592867
Inventors:
Alan J. Janis - Green Valley CA, US
Folkert Fred Koch - San Ramon CA, US
Wolfgang Ott - Antioch CA, US
Christopher Robin Drake - Fairfield CA, US
Brian Michael Piety - Vacaville CA, US
Mark David Resendes - Dixon CA, US
Assignee:
Illinois Tool Works Inc. - Glenview IL
International Classification:
F16L 37/20
B65B 1/04
US Classification:
285312, 285311, 285358, 141383
Abstract:
In certain embodiments, a PCA connector has a nylon body, wherein the nylon is durable, corrosion resistant, and exhibits excellent strength over a large range of temperature and moisture conditions. The nylon body may be described as a single structure with integral features, such as a bearing portion, a latch housing portion, a latch guide portion, and so forth. Thus, the number of parts is significantly reduced by the one-piece design of the body. In addition, the PCA connector may include a latching mechanism configured to secure the PCA connector to an aircraft. For example, the latching mechanism may include a pair of levers, which engage a pair of latches on opposite sides of the nylon body. In some embodiments, the levers may be rotated in opposite directions relative to one another to impart movement of the latches in the same direction, e. g. , an axial direction.

Self-Positioning Adapting System Between Aircraft And Preconditioned-Air Supply Hose

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US Patent:
8016325, Sep 13, 2011
Filed:
May 24, 2007
Appl. No.:
11/753382
Inventors:
Anatoly Gosis - Palatine IL, US
Scott Takayuki Koizumi - Fairfield CA, US
Folkert Fred Koch - San Ramon CA, US
Brian Michael Piety - Vacaville CA, US
Mark David Resendes - Dixon CA, US
Dale Arnold Miller - Vacaville CA, US
Assignee:
Hobart Brothers Company - Troy OH
International Classification:
F16L 27/00
US Classification:
285236, 285280, 285261, 2851471
Abstract:
A system and method for connecting a traditional air chute to an air hose delivering preconditioned air to an aircraft includes an adapter system. The adapter system includes a flexible stage having an exterior surrounding a hollow interior configured to receive air from the air hose and deliver the air to the air chute. The adapter system also includes a rotational stage coupled to the flexible stage and having an exterior surrounding a hollow interior configured to receive air from the air hose and deliver the air to the air chute. The flexible stage is adjustable relative to the rotational stage to selectively move the hollow interior of the flexible stage between extending along a common axis through the air chute and the rotational stage and not extending along the common axis.

Preconditioned Air Connector Assembly For Aircraft

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US Patent:
8146957, Apr 3, 2012
Filed:
Apr 29, 2010
Appl. No.:
12/770452
Inventors:
Alan J. Janis - Green Valley CA, US
Folkert Fred Koch - San Ramon CA, US
Wolfgang Ott - Antioch CA, US
Christopher Robin Drake - Fairfield CA, US
Brian Michael Piety - Vacaville CA, US
Mark David Resendes - Dixon CA, US
Assignee:
Illinois Tool Works Inc. - Glenview IL
International Classification:
F16L 37/20
B65B 1/04
US Classification:
285312, 285311, 285358, 141383
Abstract:
In certain embodiments, a PCA connector has a polyethylene body, wherein the polyethylene is durable, corrosion resistant, and exhibits excellent strength over a large range of temperature and moisture conditions. The polyethylene body may be described as a single structure with integral features, such as a bearing portion, a latch housing portion, a latch guide portion, and so forth. Thus, the number of parts is significantly reduced by the one-piece design of the body. In addition, the PCA connector may include a latching mechanism configured to secure the PCA connector to an aircraft. For example, the latching mechanism may include a pair of levers, which engage a pair of latches on opposite sides of the polyethylene body. In some embodiments, the levers may be rotated in opposite directions relative to one another to impart movement of the latches in the same direction, e. g. , an axial direction.

Preconditioned Air Connector Assembly For Aircraft

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US Patent:
8146958, Apr 3, 2012
Filed:
Apr 29, 2010
Appl. No.:
12/770456
Inventors:
Alan J. Janis - Green Valley CA, US
Folkert Fred Koch - San Ramon CA, US
Wolfgang Ott - Antioch CA, US
Christopher Robin Drake - Fairfield CA, US
Brian Michael Piety - Vacaville CA, US
Mark David Resendes - Dixon CA, US
Assignee:
Illinois Tool Works Inc. - Glenview IL
International Classification:
F16L 37/20
B65B 1/04
US Classification:
285312, 285311, 285358, 141383
Abstract:
In certain embodiments, a preconditioned air connector has a hollow body configured to route a fluid therethrough and a hook member configured to mate with a cooperating element to draw the hollow body into fluid communication with a mating component. The preconditioned air connector also has a pivotable member actuatable along an arc tangential to the hollow body to direct axial translation of the hook member from a first position to a second position to draw the hollow body into fluid communication with the mating component. The pivotable member has an arcuate camming surface having a locking portion that secures the connector in a fully engaged position with respect to the mating component.

Air Hose Delivery Assembly With Inner Liner

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US Patent:
20100212768, Aug 26, 2010
Filed:
Jan 19, 2010
Appl. No.:
12/689931
Inventors:
Mark David Resendes - Dixon CA, US
Assignee:
Illinois Tool Works Inc. - Glenview IL
International Classification:
F16L 11/00
US Classification:
138116, 138137, 138128, 138DIG011
Abstract:
An air hose delivery assembly includes an external conduit. The air hose delivery assembly also includes a continuous inner liner disposed within the external conduit. The continuous inner liner is secured to the external conduit only at the ends of the continuous inner liner to form a tubular structure that is configured to be collapsed to a flat structure.

Preconditioned Air Connector Assembly For Aircraft

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US Patent:
20120235402, Sep 20, 2012
Filed:
Mar 14, 2012
Appl. No.:
13/420512
Inventors:
Alan J. Janis - Green Valley CA, US
Folkert Fred Koch - San Ramon CA, US
Wolfgang Ott - Antioch CA, US
Christopher Robin Drake - Fairfield CA, US
Brian Michael Piety - Vacaville CA, US
Mark David Resendes - Dixon CA, US
Assignee:
Illinois Tool Works Inc. - Glenview IL
International Classification:
F16L 37/18
US Classification:
285312
Abstract:
A preconditioned air connector (PCA) may be provided with a hollow body configured to pass a fluid flow, and a first mount assembly coupled to the hollow body. The first mount assembly may include a first cam joint with a first arcuate path of motion in a first plane generally tangential to the hollow body, a first mount coupled to the first cam joint, and a first lever coupled to the first cam joint. The first lever may be configured to actuate the first mount via a first transfer of motion through the first cam joint to draw the first mount inwardly toward the hollow body. In addition, the first mount may be configured to draw the hollow body and a mating component inwardly toward one another to pass the fluid flow between the hollow body and the mating component.

Preconditioned Air Connector Assembly For Aircraft

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US Patent:
7152886, Dec 26, 2006
Filed:
Jun 24, 2003
Appl. No.:
10/602310
Inventors:
Alan J. Janis - Green Valley CA, US
Folkert Fred Koch - San Ramon CA, US
Wolfgang Ott - Antioch CA, US
Christopher Robin Drake - Fairfield CA, US
Brian Michael Piety - Vacaville CA, US
Mark David Resendes - Dixon CA, US
Assignee:
Illinois Tool Works Inc. - Glenview IL
International Classification:
F16L 37/20
F16L 39/00
F16L 17/00
US Classification:
285311, 285320, 285358
Abstract:
A connector for coupling a preconditioned air source to an aircraft is provided. The connector comprises actuating members rotatably secured to a body. In one embodiment, the actuating members are supported, at least partially, by an integrated bearing assembly. The connector also comprises securing members that are positionably coupled to the actuating members. Accordingly, rotation of the actuating members displaces the securing members. Moreover, the actuating members comprise respective camming surfaces, wherein the camming surfaces define the axial position of the corresponding securing members.
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Mark D Resendes from La Mesa, CA, age ~57 Get Report