US2321024A - Propeller control system - Google Patents
Propeller control system Download PDFInfo
- Publication number
- US2321024A US2321024A US407892A US40789241A US2321024A US 2321024 A US2321024 A US 2321024A US 407892 A US407892 A US 407892A US 40789241 A US40789241 A US 40789241A US 2321024 A US2321024 A US 2321024A
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- United States
- Prior art keywords
- pitch
- propeller
- steam
- speed
- blades
- Prior art date
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- Expired - Lifetime
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- 230000008859 change Effects 0.000 description 13
- 239000004020 conductor Substances 0.000 description 9
- 230000007246 mechanism Effects 0.000 description 9
- 230000005494 condensation Effects 0.000 description 6
- 238000009833 condensation Methods 0.000 description 6
- 239000012530 fluid Substances 0.000 description 6
- 230000009471 action Effects 0.000 description 4
- 238000010276 construction Methods 0.000 description 4
- 238000009413 insulation Methods 0.000 description 4
- 230000001276 controlling effect Effects 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 238000004804 winding Methods 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000009699 differential effect Effects 0.000 description 1
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 1
- 229910052753 mercury Inorganic materials 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H3/00—Propeller-blade pitch changing
- B63H3/10—Propeller-blade pitch changing characterised by having pitch control conjoint with propulsion plant control
Definitions
- PROPELLER CONTROL SYSTEM Filed Aug. 22, 1941 3 Sheets-Sheet 3 96 T 1-... T l/I/l/AIY/I/Il. 4 4
- This invention relates to variable pitch propeller systems and more specifically to a system for automatically Varying the pitch of a propeller in accordance with a characteristic of the prime mover.
- the invention further relates to means for controlling or measuring the stem consumption of the prime mover which directly controls means-for varying the pitch of the propeller blades in'such a way that the steam consumed by the prime mover is maintained at a constant value.
- the invention also provides means for varying the rate of change of pitch of the propeller blades in accordance with the rate of change of steam consumption, thus preventing rapidchanges of pitch of the propeller blades which might cause unnecessary strain and vibration on the driving machinery.
- the invention also consists in certain new-and original features of construction" and combinations of parts hereinafter set forth and claimed.
- Figure 2 illustrates diagrammatically the system as applied to the condensation meter of the prime mover.
- FIG. 3 is a top plan view'of the control apparatus, partly in section'taken on line 3-3 of Figure 4, and
- Figure 4 is a vertical section taken on line 4-4 of Figure 3.
- the hull of a marine vessel is indicated at II.
- This vessel is shown as driven by means of a propeller I 2 which is provided with adjustable blades l3.
- the propeller i2 is attached to the end of a hollow shaft I5 which passes through an outboard bearmglfi.
- the shaft is driven by a prime mover which maybe of any desired type but is preferably of a steam engine type and is provided with a governor l1, formaintaining a constant speed of rota- 'ti0n..- Y
- Theblades l3 are connectedtoa variable pitch mechanism l8 which-may be of any well known and standard construction. such as that manufactured by the Escher-Wyss-:.C'ompany of Zurich, Switzerland, the detail ofwhich form no part of .the present invention and are accordingly not specifically set forth herein.
- This mechanism in general comprises a'rod l9 slidable longitudinally within the shaft l5 and connected to control the pitch of the blades l3.
- the rod I9 is actuated by a piston 21 in a.v fluid pressure cylinder 21a.
- Fluid for actuating the'piston 21 is supplied by a pump 26 through a control valve 25 and a. distribution valve 25a which communicates with the cylinder. 21a through ducts, not shown, in the .shaft 15.
- rotatesaworm 2-2 which operates to move the upperend of a floating lever 23, which, in turn,.is pivoted to the end of a valve rod 24 which controls the valve 25'.
- the piston 21 is connected by a rod 28 to a collar 29 which is slidably mounted on the shaft I5- and engages the lower end of the lever 23 so that the position of .this end of the lever corresponds to the pitch of the blades l3.
- the upper end of the lever 23 is connected by a wire 30 to an indicator 3
- the fluid pump 26 is driven either by a motor 33 or a belt 35 from the shaft [5.
- a reservoir 36 and a supply tank 31 are provided for the necessary fluid.
- pitch control devices may be employed in place of that referred to above, for varying the pitch of the propeller blades 13- in responseto actuation of the motor 2
- a particular type is shown for purposes of illustration only.
- a fluid meter HI which may be of any well known and standard construction such as that manufactured by the Bailey Meter Co. of Cleveland, Ohio, and described on pages 911 of their bulletin 301, is shown for measuring the volume of steam supplied toengine 20.
- the meter 10 consists essentially of a box H in which is mounted a bell casing 12. Positioned inside of this casing is a mercury sealed Ledoux bell 73, which is free to move up and down inside the Casing 12. A cap 15 rests on top of the bell 73 and is attached' by a forked lever 16 to a spindle Tl.
- the engine 20 is supplied with steam thru a pipe 18 in which-is located an orifice plate 19.
- the interior of the casing 12 is connected by a tube 8
- the spindle 11 which passes thru the wall of the casing 12, is connected to an arm 85.
- a contact 46 which selectively engages six segments 41-52 mounted on but insulated from an are shaped member which is slidably mounted in brackets 55 and 56, which are attached to a plate 86 secured to the box 1
- the bracket 56 is provided witha clamping screw 54 for holding the member 53 and contacts 41-52 in any desired position.
- the segments 41 and 52 are connected by flexible conductors to two conductors 58 and 59 which in turn are connected to the reversing L windings of the motor 2
- the segments 48 and 49 are connected by flexible conductors to two resistors 68 and 6
- the member 53 is then moved until the insulation between the segments 49 and 50 is under the contact 46 and is held in thisposition by tightening the screw 45.
- the blade of the switch 65 is then moved into engagement with the center contact.
- the pitch of the propeller blades I3 is varied to cause the propeller to operate so as to maintain the steam consumption, and therefore the power supplied from the engine 20, constant under varied conditions.
- the rate of change of pitch will vary in accordance with the change of steam consumption "so that with a gradual change of steam consumption there will be a slow change of propeller pitch, thus preventing violent changes of pitch which would cause undue strain onthe driving mechanism, disagreeable vibrations and inefliciency of the propeller, but a more abrupt change in steam consumption will be promptly and quickly corrected by amore rapid, actuation of the pitch control means.
- metering device 93 which may contain a rotary condensation meter 94 ( Figure 4) such as that made by the American District Steam Co. of North Tonawanda, New York, and described in their bulletin No. 35-80.
- a drain pipe 95 is connected to the device 93.
- lhe meter 94 is provided with a shaft 99 to which is attached a bevel gear 9'. ( Figure 3) which meshes with a bevel pinion 98.
- the pinion 98 is rotatably mounted on a member 99 which in turn is rotatably mounted on the shaft 56.
- Meshing with the bevel pinion 98 is a second bevel gear I98 which is secured to the shaft ID! of a variable speed mechanism such as a clockwork mechanism I92.
- the speed of rotation of the gear N10 is controlled by the position of a pointer, I93 (Fig. 2) which registers with a scale I94.
- Attached to the member 99 is the contact 46 which selectively engages the segments 41 to 52 which are mounted on but insulated from the device 93.
- the segments 41-52 are connected to the motor 2
- the clockwise mechanism I02 is then started in motion and its speed is regulated by the pointer I63 until the gear its rotates in a counterclockwise direction at the same speed as the gear 97 rotates in a clockwise direction. Under these conditions the member 99 on which the pinion 98 is mounted will not rotate on the shaft 96, but will remain stationary with the contact 46 on the insulation between the segments 49 and 50. The switch 56 is now closed on the center contact.
- a propeller having blades, means controlling the pitch of said blades, a steam actuated motor driving said propeller, a steam consumption meter, means connecting said meter to be actuated in accordance with the rate of steam consumption of said motor, and means actuated by said meter to cause said pitch control means to decrease the pitch of said blades in response to an increased rate of steam consumption and vice'versa so as to maintain a substantially constant rate steam consumption.
- a governor connected to cause the propeller to operate at constant speed.
- a system as set forth in claim 1 in which the meter comprises a pressure actuated device, means to produce a pressure differential proportional to the rate of steam flow to said motor and means connecting said device to be responsive to said pressure differential.
- a condenser to condense the exhaust steam from said motor means supplying condensate from said condenser to said meter, said meter being responsive to the rate of condensate flow and being connected to control the pitch of said blades inversely of the rate of condensate flow.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Description
440-50 59 e RPjGTGnCE June 0, no. J. H. HAMMOND, JR 2,321,024
I PROPELLER CONTROL SYSTEM Filed Aug. 22, 1941 I 3 Sheets-Sheet l mvamca JOHN HAYS HAMMOND, JR,
2.3211 2% QR Ia 415/35 uccuul WJUIT.
4 2 1 2 2 t Bu C n 6 w .I a ml N e m H m S m T lu J a 4 9 1 w 8 v e n H J fir PROPELLER CONTROL SYSTEM Filed Aug. 22, 1941 3 Sheets-Sheet 2 Pom NBNASAUQEQ \JIUSS HUIUI UHbU UUCHUH Hoom June 8, 1943. J. H. HAMMOND, JR 2,321,024
PROPELLER CONTROL SYSTEM Filed Aug. 22, 1941 3 Sheets-Sheet 3 96 T 1-... T l/I/l/AIY/I/Il. 4 4
INVENTOR I l g L. JOHN HAYS HAMMOND, JR.
ORNEY Patented June 8, 1943 UNITED STATES PATENT OFFICE This invention relates to variable pitch propeller systems and more specifically to a system for automatically Varying the pitch of a propeller in accordance with a characteristic of the prime mover.
The invention further relates to means for controlling or measuring the stem consumption of the prime mover which directly controls means-for varying the pitch of the propeller blades in'such a way that the steam consumed by the prime mover is maintained at a constant value.
The invention also provides means for varying the rate of change of pitch of the propeller blades in accordance with the rate of change of steam consumption, thus preventing rapidchanges of pitch of the propeller blades which might cause unnecessary strain and vibration on the driving machinery.
The invention also consists in certain new-and original features of construction" and combinations of parts hereinafter set forth and claimed.
Although the novel features. which'are believed to be characteristic of this invention will be particularly pointed out in the claims appended here to, the invention itself, as to its objects and advantages, the mode of its operation and the manner of its organization may be better understood by referring to the following description taken in connection with the accompanying drawings forming a part thereof, in which Figure 1 illustrates diagrammatically the system as applied to the steam consumption meter of the prime mover.
Figure 2 illustrates diagrammatically the system as applied to the condensation meter of the prime mover.
Figure 3 is a top plan view'of the control apparatus, partly in section'taken on line 3-3 of Figure 4, and
Figure 4 is a vertical section taken on line 4-4 of Figure 3. p v
Like reference charactersdenote like parts in the several figures of the drawings.
In the following description and'in the claims parts will be identified by specific names for convenience, but they are intended to be as generic in their application to similar parts as the'art will permit.
Referring to the accompanying drawing, and more particularly to Figure 1, the hull of a marine vessel is indicated at II. This vessel is shown as driven by means of a propeller I 2 which is provided with adjustable blades l3. The propeller i2 is attached to the end of a hollow shaft I5 which passes through an outboard bearmglfi. The shaft is driven by a prime mover which maybe of any desired type but is preferably of a steam engine type and is provided with a governor l1, formaintaining a constant speed of rota- 'ti0n..- Y
Theblades l3 are connectedtoa variable pitch mechanism l8 which-may be of any well known and standard construction. such as that manufactured by the Escher-Wyss-:.C'ompany of Zurich, Switzerland, the detail ofwhich form no part of .the present invention and are accordingly not specifically set forth herein. This mechanism, in general comprises a'rod l9 slidable longitudinally within the shaft l5 and connected to control the pitch of the blades l3. The rod I9 is actuated by a piston 21 in a.v fluid pressure cylinder 21a. Fluid for actuating the'piston 21 is supplied by a pump 26 through a control valve 25 and a. distribution valve 25a which communicates with the cylinder. 21a through ducts, not shown, in the .shaft 15.
The upper end of the lever 23 is connected by a wire 30 to an indicator 3| which shows the pitch at which the blades I3 are set. tops 32 are provided for limiting the maximum and minimum pitch of the blades l3. The fluid pump 26 is driven either by a motor 33 or a belt 35 from the shaft [5. A reservoir 36 and a supply tank 31 are provided for the necessary fluid.
It is to be understood that other pitch control devices may be employed in place of that referred to above, for varying the pitch of the propeller blades 13- in responseto actuation of the motor 2|. A particular type is shown for purposes of illustration only.
A fluid meter HI, which may be of any well known and standard construction such as that manufactured by the Bailey Meter Co. of Cleveland, Ohio, and described on pages 911 of their bulletin 301, is shown for measuring the volume of steam supplied toengine 20. The meter 10 consists essentially of a box H in which is mounted a bell casing 12. Positioned inside of this casing is a mercury sealed Ledoux bell 73, which is free to move up and down inside the Casing 12. A cap 15 rests on top of the bell 73 and is attached' by a forked lever 16 to a spindle Tl.
a o e The engine 20 is supplied with steam thru a pipe 18 in which-is located an orifice plate 19. The interior of the casing 12 is connected by a tube 8| to a point in the pipe I8 below the orifice plate 19 and the interior of the bell 13 is connected by a tube 82 to a point in the pipe 18 above the orifice plate '19.
The spindle 11, which passes thru the wall of the casing 12, is connected to an arm 85. Mounted on but insulated from the arm 85 is a contact 46, which selectively engages six segments 41-52 mounted on but insulated from an are shaped member which is slidably mounted in brackets 55 and 56, which are attached to a plate 86 secured to the box 1|. The bracket 56 is provided witha clamping screw 54 for holding the member 53 and contacts 41-52 in any desired position.
The segments 41 and 52 are connected by flexible conductors to two conductors 58 and 59 which in turn are connected to the reversing L windings of the motor 2|. The segments 48 and 49 are connected by flexible conductors to two resistors 68 and 6| which in turn are connected would cause a greater difference in pressure between the inside and outside of the bell 13 thus causing it to move up, which in turn would cause the contact 46 to engage the segment 49. This will close a circuit from the. battery 65 thru the resistor 6| to the motor 2| causing it to rotate slowly in a direction to move the upper end of the lever 23 to the right which will allow fluid under pressure to pass from the pump 26 to the cylinder 21a by means of the ducts in the shaft |5. This will actuate the piston 21, which, by means of the rod l9 and link mechanism will cause the propeller blades l3 to slowly decrease their pitch. This will allow the engine to increase the speed of rotation of the propeller, which in turn will increase the speed of the governor H, thus decreasing the supply of steam to the conductor 58. The segments and 5| are connected by flexible conductors to two resistors 62 and 63 which in turn are connected to the conductor 59. The common lead of the reversing windings of the motor 2| is connected thru a battery 65 to the blade of a three position switch The center contact of this switch is connected to the contact 46, the upper contact to the conductor 58 and the lower contact to. the conductor 59.
Operation of Figure 1 to the left or right to increase or decrease the pitch in a well known manner, the angle-of pitch being indicated by the pointer of the indicator 3|. The vessel is brought up to the desired speed in the usual manner. The steam necessary to supply the engine 20 under these conditions passes thru the orifice in the plate 19 which causes an increase of pressure in the pipe 82 and a decrease of pressure in the pipe 8|. The reduced pressure established in the pipe 8| is applied to the interior of the casing 12 and the increased pressure established inthe pipe 82' is applied to the interior of the bell 13. This causes the bell 13 to rise an amount proportional to the difference in pressures in the pipes 8| and 82.
The motion of the bell 13 i's transmitted, by.
means of the cap 15 and lever 16, to the arm 85 and contact 46 which takes up-a position depending upon the difierence in pressure inside and outside the bell I3 which is proportional to the volume of steam consumed by the engine 20.
The member 53 is then moved until the insulation between the segments 49 and 50 is under the contact 46 and is held in thisposition by tightening the screw 45. The blade of the switch 65 is then moved into engagement with the center contact.
If the forces against which the vessel is moving should increase, the speed of the propeller |2 would decrease and the throttle valvewould be opened by the governor to supply more steam to;
the engine 20. This increased volume of steam to the pipe 18. This action will continue until the contact 46 is again on the insulation between the segments 49 and 50- at which time the motor 2| will stop.
If under favorable conditions the speed of the propeller should increase, the opposite action would take place and the contact 46 would engage the segment 50 which would cause the blades I3 to slowly increase their pitch until the steam consumption hadbeenincreased to the desired value.
' If the changed conditions cause a rapid change of engine speed so that the contact 46 engages either of the segments 48 or 5|, then the resistor 60 or the resistor 63 will be thrown in circuit with the motor 2|. As resistors 66 and 63 have less resistance than resistors 6| and 62, the motor 2|will be caused to rotate faster, thus changing the propeller pitch more'rapidly to take care of the more rapidly changing conditions.
If conditions change so quickly that the contact 46' engages either segment 41 or segment 52, then no resistance. will be thrown in the circuit of the motor 2| and it will rotate at its maximum speed, thus changing the propeller pitch at a maximum rate. The stops 32 are provided so that the propeller pitch is prevented from exceeding certain limits beyond which it could not operate efficiently under any conditlons.
By the system above described the pitch of the propeller blades I3 is varied to cause the propeller to operate so as to maintain the steam consumption, and therefore the power supplied from the engine 20, constant under varied conditions. The rate of change of pitch will vary in accordance with the change of steam consumption "so that with a gradual change of steam consumption there will be a slow change of propeller pitch, thus preventing violent changes of pitch which would cause undue strain onthe driving mechanism, disagreeable vibrations and inefliciency of the propeller, but a more abrupt change in steam consumption will be promptly and quickly corrected by amore rapid, actuation of the pitch control means.
Referringto the modified form of the invention shown in Figures 2, 3 and 4, the mechanism up to and including the tank 31 is identical to that already described and corresponding parts have been. given the samenumerals. In this form of the invention the governor and throttle valve are not shown but, it is to be understood that such devices may be used to maintain thespeed of the shaft |5 constant. r V
In Figure 2 the engine 20 is. shown as exhausting thru= an exhaustpipe to a'condn'serfSl, the condensate from which passes thru a pipe 92 to a.
Attached to the member 99 is the contact 46 which selectively engages the segments 41 to 52 which are mounted on but insulated from the device 93. The segments 41-52 are connected to the motor 2| by conductors 58 and 59, resistors 6fl63, battery 65 and switch 65 as described in connection with Figure 1.
Operation of Figures 2, 3 and 4 In the operation of the modified form of the invention shown in Figures 2, 3 and 4, the vessel is brought up to the desired speed in the usual manner. The exhaust steam from the engine under these conditions passes thru the pipe 90 to the condenser 9| where it is condensed to water. The condensate from the condenser 9| then passes thru the pipe 92 to the rotary condensation member 94 which is caused to rotate in a clockwise direction at an approximately uniform rate of speed which is determined by the amount of condensate and therefore by the amount of steam supplied to the engine 20.
The clockwise mechanism I02 is then started in motion and its speed is regulated by the pointer I63 until the gear its rotates in a counterclockwise direction at the same speed as the gear 97 rotates in a clockwise direction. Under these conditions the member 99 on which the pinion 98 is mounted will not rotate on the shaft 96, but will remain stationary with the contact 46 on the insulation between the segments 49 and 50. The switch 56 is now closed on the center contact.
If the forces against which the vessel is moving should increase, the speed of the propeller l2 would decrease and the throttle valve would be opened by the governor to supply more steam to the engine 28. This increase of steam used by the engine 29 would cause a greater volume of condensate to leave the condenser 91 by the pipe 92 and enter the rotary meter 94. This would cause an increase of speed of rotation of the shaft 96 which would then rotate the gear 9'! faster in a counterclockwise direction then. the gear. I99 is rotated in a clockwise direction. Due to the differential action of the mechanism the member 99 would then start rotating slowly in a clockwise direction.
This action would cause the contact 46 to engage the segment 49 which as already described in connection with Figure 1 would cause a gradual decrease in pitch of the blades l3, thus causing the engine 20 to speed up which, by means of the governor, would decrease the supply of steam and therefore reduce the volume of the condensate. This would cause the gear 91 to reduce its speed of rotation until the contact 46 was again on the insulation between the segments 49 and 50 at which time the motor 2| would stop.
If under favorable conditions the speed of the propeller should increase the opposite action would take place and the contact 46 would engage the segment 59 which would cause the blades l3 to slowly increase their pitch until the steam consumption and therefore the volume of condensation had been increased to the fixed value. If conditions changed more rapidly the change of propeller pitch would be more rapid as described in connection with Figure 1.
It is thu seen that a system has been developed which will maintain the steam consumption of a prime mover constant under various conditions of wind and weather and that the vessel will be propelled in the most economical. mannerwith a fixed steam consumption.
Although only a few of the various forms in which this invention may be embodied have been shown herein, it is to be understood that the invention is not limited to any specific construction but might be embodied in various forms without departing from the spirit of the invention or the scope of the appended claims.
What is claimed is:
1. In system for driving a vessel, a propeller having blades, means controlling the pitch of said blades, a steam actuated motor driving said propeller, a steam consumption meter, means connecting said meter to be actuated in accordance with the rate of steam consumption of said motor, and means actuated by said meter to cause said pitch control means to decrease the pitch of said blades in response to an increased rate of steam consumption and vice'versa so as to maintain a substantially constant rate steam consumption.
2. In a system as set forth in claim 1, a governor connected to cause the propeller to operate at constant speed.
3. A system as set forth in claim 1 in which the meter comprises a pressure actuated device, means to produce a pressure differential proportional to the rate of steam flow to said motor and means connecting said device to be responsive to said pressure differential.
l. In a system as set forth in claim 1, a condenser to condense the exhaust steam from said motor, means supplying condensate from said condenser to said meter, said meter being responsive to the rate of condensate flow and being connected to control the pitch of said blades inversely of the rate of condensate flow.
5. In a system as set forth in claim 1. means responsive to the amplitude of change in steam consumption, said last means being connected to increase the speed of operation of said pitch control means when the amplitude of change in steam consumption is greater and vice versa, regardless of the direction of such change.
6. The invention set forth in claim 1 in which the meter is responsive to the rate of steam condensation and means causing condensation of the exhaust steam at a rate proportional to the rate of flow of the steam supplied to said motor.
JOHN HAYS HAMfMOND, JR.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US407892A US2321024A (en) | 1941-08-22 | 1941-08-22 | Propeller control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US407892A US2321024A (en) | 1941-08-22 | 1941-08-22 | Propeller control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2321024A true US2321024A (en) | 1943-06-08 |
Family
ID=23613970
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US407892A Expired - Lifetime US2321024A (en) | 1941-08-22 | 1941-08-22 | Propeller control system |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2321024A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2606420A (en) * | 1947-03-12 | 1952-08-12 | Fairchild Camera Instr Co | Elastic fluid engine control system responsive to a temperature factor of the motive fluid |
| US2612956A (en) * | 1942-09-22 | 1952-10-07 | Jr Thomas A Banning | Synchronizing means for multimotored airplanes |
| US2778436A (en) * | 1945-01-18 | 1957-01-22 | Jr Thomas A Banning | Controls for variable pitch propellers and the like |
-
1941
- 1941-08-22 US US407892A patent/US2321024A/en not_active Expired - Lifetime
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2612956A (en) * | 1942-09-22 | 1952-10-07 | Jr Thomas A Banning | Synchronizing means for multimotored airplanes |
| US2778436A (en) * | 1945-01-18 | 1957-01-22 | Jr Thomas A Banning | Controls for variable pitch propellers and the like |
| US2606420A (en) * | 1947-03-12 | 1952-08-12 | Fairchild Camera Instr Co | Elastic fluid engine control system responsive to a temperature factor of the motive fluid |
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