US2379299A - Air relay assembly for automatic pilots - Google Patents
Air relay assembly for automatic pilots Download PDFInfo
- Publication number
- US2379299A US2379299A US462033A US46203342A US2379299A US 2379299 A US2379299 A US 2379299A US 462033 A US462033 A US 462033A US 46203342 A US46203342 A US 46203342A US 2379299 A US2379299 A US 2379299A
- Authority
- US
- United States
- Prior art keywords
- air
- diaphragm
- relay assembly
- air relay
- automatic pilots
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
Definitions
- This invention relates to air relays for automatic pilots and has for its primary object to provide an improved housingy that will be leakproof in operation and simple in construction and which may be formed in one simple die casting operation of each of its two complementary parts and still provide for the necessary inlet and outlet ports in the two chambers in the housing that are separated by the conventional two-way pressure responsive flexible diaphragm.
- Figure 1 is an end view of the housing for the air relay
- Figure 2 is a View in section taken through air relay assembly along line 2-2 of Figure 1;
- Figure 3 is a view in section through one of the air outlet passages and nozzles taken along line 3--3 of Figure 1;
- Figure 4 is an enlarged detail view in section taken through one of the outlet nozzles.
- the air relay assembly includes a housing made up of two single separate castings I and 2 releasably joined together by a series of screws 3 near their outer edges passing therethrough and also through a two-way pressure responsive flexible diaphragm 4 held by two stiffening plates I9 and 20 and two retaining members 'I and I0.
- plates I9 and 20 are of lesser diameter than the diaphragm to stiifen the latter against sagging but permit suflicient flexing of the diaphragm for operating purposes.
- the diaphragm divides the space between the inner concave faces of the two complementary castings into two separate air chambers and 6.
- the diaphragm is not actuated in either direction by any springs, or the like, and is strictly a two-way pressure responsive diaphragm that 4is operated in one direction or the other away from central neutralposition by a differential of pressure in air chambers 5 and 6 as the differential is created by a conventional nor- The ⁇ mally equalized pressure differential creating
- the diaphragm. is apertured to receive- Casting I is die cast to include an air outlet passage I2 and a passage screw-threaded to receive a removable inlet nozzle I3 with a restricted bore I6. Both inlet nozzle I3 and outlet I2 are in communication with a channel I'I in the side wall of casing I leading to air chamber 5 on the left side of the diaphragm.
- Casting 2 is die cast to include an air outlet I 4 and a passage screw- ⁇ threaded to receive a removable inlet nozzle I5,
- a housing comprising two separate anged complementary single die castings with opposed concaveV inner surfaces, a two-way pressure responsive flexible diaphragm mounted between and suspended and supported solely by said castings to form two separate air chambers normally of equal size but variable in size by the movements of said diaphragm in either direction away from neutral central position caused solely in response to 'the differences in pressure acting on the opposite sides of said diaphragm, each of said castings having cast integrally within the side wall thereof a single air channel communicating with its separate air chamber and an air inlet and an air outlet in each of said castings communicating with its separate air channel each of said channels constituting the sole means for admission of air to and the exhaust of air from its associated chamber, and a shaft connected to and movable by said diaphragm.
Description
Jupe 26, 1945.
R. M. HEINTZ AIR RELAY ASSEMBLY FOR AUTOMATIC PILOTS Filed Ociu 14, 1942 'lli-5....
INVENTOR. HL PH M. HEM/rz Patented June 26, 1945 AIR RELAY ASSEMBLY FOR AUTOMATIC PILOTS Ralph M. Heintz, Cleveland, Ohio, assignor to Jack & Heintz, Inc., Bedford, Ohio, a corporation of Ohio Application October 14, 1942, Serial No. 462,033
1 Claim.
This invention relates to air relays for automatic pilots and has for its primary object to provide an improved housingy that will be leakproof in operation and simple in construction and which may be formed in one simple die casting operation of each of its two complementary parts and still provide for the necessary inlet and outlet ports in the two chambers in the housing that are separated by the conventional two-way pressure responsive flexible diaphragm.
With the foregoing and other objects in view, the invention resides in the combination of parts and in the details of construction hereinafter set forth in the following specification and appended claim, certain embodiments thereof being illustrated in the accompanying drawing, in which:
Figure 1 is an end view of the housing for the air relay;
Figure 2 is a View in section taken through air relay assembly along line 2-2 of Figure 1;
Figure 3 is a view in section through one of the air outlet passages and nozzles taken along line 3--3 of Figure 1; and
Figure 4 is an enlarged detail view in section taken through one of the outlet nozzles.
Referring more particularly to the drawing the air relay assembly .includes a housing made up of two single separate castings I and 2 releasably joined together by a series of screws 3 near their outer edges passing therethrough and also through a two-way pressure responsive flexible diaphragm 4 held by two stiffening plates I9 and 20 and two retaining members 'I and I0. plates I9 and 20 are of lesser diameter than the diaphragm to stiifen the latter against sagging but permit suflicient flexing of the diaphragm for operating purposes. The diaphragm divides the space between the inner concave faces of the two complementary castings into two separate air chambers and 6. The diaphragm is not actuated in either direction by any springs, or the like, and is strictly a two-way pressure responsive diaphragm that 4is operated in one direction or the other away from central neutralposition by a differential of pressure in air chambers 5 and 6 as the differential is created by a conventional nor- The` mally equalized pressure differential creating The diaphragm. is apertured to receive- Casting I is die cast to include an air outlet passage I2 and a passage screw-threaded to receive a removable inlet nozzle I3 with a restricted bore I6. Both inlet nozzle I3 and outlet I2 are in communication with a channel I'I in the side wall of casing I leading to air chamber 5 on the left side of the diaphragm. Casting 2 is die cast to include an air outlet I 4 and a passage screw-` threaded to receive a removable inlet nozzle I5,
provided with a restricted bore, such as shown at.
I6. Both inlet and outlet are in communication with a channel I8 in the side wall of the casting 2 leading to air chamber 6.
Under the control of the conventional gyro air pick-off and suction pump, not shown, when the air in chamber 6 alone is exhausted under the control of restricted inlet-I nozzle I5 and through passage I4 the diaphragm is drawn to the right so as to force shaft 8 to the right which, in the usual manner, operates the balanced oil valve, not shown, to the right. Likewise, when air chamber 5 alone is exhausted under the control of restricted inlet nozzle I3 and through passage I2 the diaphragm is drawn to the left so as to force shaft 8 to the left which operates the oil valve accordingly.
It will readily be seen from the foregoing that there has been provided an automatic pilot air relay that in addition to the diaphragm and shaft,
includes only two simple complementary removable and replaceable castings which provide the necessary air passages and which inlet passages are adapted to removably receive air intake nozzles.
. I claim:
In combination in an air pressure actuated relay, a housing comprising two separate anged complementary single die castings with opposed concaveV inner surfaces, a two-way pressure responsive flexible diaphragm mounted between and suspended and supported solely by said castings to form two separate air chambers normally of equal size but variable in size by the movements of said diaphragm in either direction away from neutral central position caused solely in response to 'the differences in pressure acting on the opposite sides of said diaphragm, each of said castings having cast integrally within the side wall thereof a single air channel communicating with its separate air chamber and an air inlet and an air outlet in each of said castings communicating with its separate air channel each of said channels constituting the sole means for admission of air to and the exhaust of air from its associated chamber, and a shaft connected to and movable by said diaphragm.
RALPH M. HEINTZ.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US462033A US2379299A (en) | 1942-10-14 | 1942-10-14 | Air relay assembly for automatic pilots |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US462033A US2379299A (en) | 1942-10-14 | 1942-10-14 | Air relay assembly for automatic pilots |
Publications (1)
Publication Number | Publication Date |
---|---|
US2379299A true US2379299A (en) | 1945-06-26 |
Family
ID=23834935
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US462033A Expired - Lifetime US2379299A (en) | 1942-10-14 | 1942-10-14 | Air relay assembly for automatic pilots |
Country Status (1)
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US (1) | US2379299A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2467517A (en) * | 1946-01-04 | 1949-04-19 | Midland Steel Prod Co | Power unit for hydraulic brakes |
US2685304A (en) * | 1951-04-19 | 1954-08-03 | Tokheim Corp | Self-sustaining arched diaphragm structure |
US3435797A (en) * | 1967-05-03 | 1969-04-01 | Continental Oil Co | Compressed air,pressure-sensing actuator |
-
1942
- 1942-10-14 US US462033A patent/US2379299A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2467517A (en) * | 1946-01-04 | 1949-04-19 | Midland Steel Prod Co | Power unit for hydraulic brakes |
US2685304A (en) * | 1951-04-19 | 1954-08-03 | Tokheim Corp | Self-sustaining arched diaphragm structure |
US3435797A (en) * | 1967-05-03 | 1969-04-01 | Continental Oil Co | Compressed air,pressure-sensing actuator |
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