U.S. patent number D900,899 [Application Number D/690,637] was granted by the patent office on 2020-11-03 for flow passage contours for a hydraulic manifold for actuator control with dual solenoids.
This patent grant is currently assigned to THE BOEING COMPANY. The grantee listed for this patent is The Boeing Company. Invention is credited to Mitchell L. R. Mellor, Jonathan B. Wallace.
United States Patent |
D900,899 |
Mellor , et al. |
November 3, 2020 |
Flow passage contours for a hydraulic manifold for actuator control
with dual solenoids
Claims
CLAIM The ornamental design for flow passage contours for a
hydraulic manifold for actuator control with dual solenoids, as
shown and described.
Inventors: |
Mellor; Mitchell L. R.
(Seattle, WA), Wallace; Jonathan B. (Mount Vernon, WA) |
Applicant: |
Name |
City |
State |
Country |
Type |
The Boeing Company |
Chicago |
IL |
US |
|
|
Assignee: |
THE BOEING COMPANY (Chicago,
IL)
|
Appl.
No.: |
D/690,637 |
Filed: |
May 9, 2019 |
Current U.S.
Class: |
D15/149 |
Current International
Class: |
1509 |
Field of
Search: |
;D15/5,138,148,149
;D23/245 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Palasik; Patricia A
Attorney, Agent or Firm: Parsons Behle & Latimer
Description
FIG. 1 is a perspective view showing the top, front, and right
sides of a supply boss for a hydraulic manifold for actuator
control with dual solenoids showing the new design;
FIG. 2 is a right side elevation view thereof;
FIG. 3 is a left side elevation view thereof;
FIG. 4 is a top side elevation view thereof;
FIG. 5 is a bottom side elevation view thereof;
FIG. 6 is a front side elevation view thereof; and,
FIG. 7 is a back side elevation view thereof.
The evenly spaced broken lines depict portions of the manifold and
environmental subject matter that forms no part of the claim. The
dash-dot broken lines represent boundaries of the claim and form no
part thereof.
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