Space condition responsive instrument
US D201914 S
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Description (OCR text may contain errors)
United States Patent 0 "me 201,914
Patented Aug. 10, 1965 SPACE CONDITION RESPONSIVE INSTRUMENT Wallace A. Monson, Golden Valley, and Norbert Thomas Wolfe, Minneapolis, Minn., assignors to Honeywell Inc., a corporation of Delaware Filed Sept. 25, 1963, Ser. No. 76,720
Term of patent 14 years (Cl. D527) .nlllllllllllllllllllllllllllllllll I FIGURE 1 is a front perspective view of the space con- We claim: dition responsive instrument as seen from the right, em- The ornamental design for a space condition responsive bodying our new design; instrument, substantially as shown and described.
FIGURE 2 is a front view; FIGURE 3 is a side view as seen from the left side References Cited by the Examiner of FIGURE 2.
The bottom of the instrument is substantially the same UNITED STATES PATENTS as the top. The rear of the instrument is flat in appear- 177314 4/56 Davis 1352-7 ance except for a conventional controller element illus- 11186997 1/60 Claus D527 trated in broken i D. 1 7, 9 3/60 Becker D522 The essential features of our disclosed design reside in 192100 1/62 Richards et a1 D522 the portions shown in full lines in the drawing. WALLACE R. BURKE, Acting Primary Examiner.
ADELINE B. HANNAH, Examiner.