USD214202S - Space condition responsive instrument - Google Patents

Description

United Statos Patent 0 F Des.

Patented May 20, 1969 SPACE CONDITION RESPONSIVE INSTRUMENT Alvin J. Stahel, St. Paul, Minn., assignor to Honeywell Inc., Minneapolis, Minn., a corporation of Delaware Filed Feb. 7, 1968, Ser. No. 10,468

Term of patent 14 years Int. Cl. DID-07 U.S. Cl. D52-7 [Pink 3 Des. 214,202

PAGE 2 FIGURE 1 is a top view of a space condition responsive instrument embodying my new design;

FIGURE 2 is a front view of the instrument;

FIGURE 3 is a side view as seen from the right side of FIGURE 2, the other side being substantially a mirror image thereof;

FIGURE 4 is a back view;

FIGURE 5 is a frontal view as seen when looking directly at the face of the instrument.

FIGURE 6 is a fragmentary cross-sectional view taken generally along line 66 in FIGURE 5;

FIGURE 7 is a front view as seen when looking directly at the face of the instrument utilizing another embodiment of my design; and

FIGURE 8 is a fragmentary cross-sectional view taken generally along line 8-8 in FIGURE 7.

In the design embodiment comprising FIGURES 7 and 8 the sides, as well as the top and rear, of the instrument are essentially the same in appearance as the corresponding views of the other design embodiment shown.

The dominant features of the design reside in the portions shown in full lines.

I claim:

The ornamental design for a space condition responsive instrument, substantially as shown and described.

References Cited UNITED STATES PATENTS D. 181,053 9/1957 Hauser D52-7 D. 208,798 10/ 1967 McLeod D427 D. 210,676 4/1968 Miley D427 WALLACE R. BURKE, Primary Examiner.

I. COOPERSMITH, Assistant Examiner.

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