[go: up one dir, main page]

US2613547A - Dual throttle control - Google Patents

Dual throttle control Download PDF

Info

Publication number
US2613547A
US2613547A US63988A US6398848A US2613547A US 2613547 A US2613547 A US 2613547A US 63988 A US63988 A US 63988A US 6398848 A US6398848 A US 6398848A US 2613547 A US2613547 A US 2613547A
Authority
US
United States
Prior art keywords
lever
levers
slave
master
throttle
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
Application number
US63988A
Inventor
Charles D Stewart
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Lockheed Martin Corp
Original Assignee
Lockheed Aircraft Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Lockheed Aircraft Corp filed Critical Lockheed Aircraft Corp
Priority to US63988A priority Critical patent/US2613547A/en
Application granted granted Critical
Publication of US2613547A publication Critical patent/US2613547A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D25/00Controlling two or more co-operating engines
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/20Control lever and linkage systems
    • Y10T74/20012Multiple controlled elements
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/20Control lever and linkage systems
    • Y10T74/20207Multiple controlling elements for single controlled element
    • Y10T74/20213Interconnected
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/20Control lever and linkage systems
    • Y10T74/20576Elements
    • Y10T74/20582Levers
    • Y10T74/2063Stops

Definitions

  • This invention relates to an improved throttle control providing for the normal operation of two powerplants as a unit from a single master control lever, with provisions for close adjustment of synchronism, and overriding individual controls operable at the will of the pilot.
  • the control lever for conventional type piston engines is commonly called the throttle as it operates a valve in the intake duct thereof.
  • throttle operates a valve in the intake duct thereof.
  • throttle also refer to the control lever of jet or propeller drive turbine powerplants where such levers control the fuel supply and when moved past the idle position cut off the fuel supply to stop such engines.
  • the embodiment hereinafter disclosed is primarily designed for the control of such turbine powerplants, it is equally suitable for use in controlling piston type engines.
  • Such a master throttle control permits the addition of auxiliary controls to the hand grip thereof, which grip may carry switches and may be longitudinally and/or rotatably movable to control still other functions interrelated to the throttle control of the powerplant.
  • a further refinement of this object is to provide a differential control for 3 Claims. (Cl. 74-471) adjusting the position of the slave throttle levers relative to'the master control lever whereby to enable close synchronization of the separate powerplants at an point in their range of operation.
  • a master and slave throttle control lever arrangement of the type described wherein the individual levers are subjected to an adjustable braking force adequate to maintain any relative adjustment of an individual lever unaffected by movements of the other levers.
  • Figure 1 is a perspective View, partly broken away for clearness, of a master and slave throttle lever arrangement embodying a specific form of my invention
  • Figure 2 is a side elevation of the device of Figure l, with parts omitted for clearness;
  • Figure 3 is a central vertical section on the line 3-3 of Figure 4, showing details of the synchronizing adjustment
  • Figure 4 is a fragmentary view from the left of Figure 2 showing thesynchmnizing adjustment mechanism to an enlarged scale
  • Figure 5 is a section on the line 5-5 of Figure 3. 1
  • the throttle control of this invention is intended to be built into a side shelf ill in the cockpit ll of an airplane (not shown), and is intended to operate individual powerplant control rods l2 and I3 which extend to the powerplants themselves.
  • these rods would operate throttle valves for fuel injection controls, and in the case of turbine powerplants would operate fuel injection controls.
  • I will hereinafter refer to these controls as throttle controls. 7
  • Interposed between the slave lever l6 and the flange
  • has a pin 23 which holds stationary a pair of discs 24 on either side of the lever IS.
  • similarly holds stationary a second pair of the discs 24, located on either side of the other slave lever ll.
  • Adjustable braking pressure is put on this assemblage by a hub 25 of a hand wheel 28 which hub is threaded on the shaft M and may be tightened as desired by the pilot to give sufficient friction for smooth operation of the levers and/or to hold them in their adjusted position if it is desired to take the hand off the master lever.
  • the provision of stationary discs 24 between each of the movable parts assures that if either slave lever H5 or I1 is disconnected from the master lever it will remain in its set position, unaffected by subsequent movements of the master lever.
  • the normal operation of the master lever carries both slave levers with it and the pilot merely has to grasp and push or pull on a knob 21 carried by the upper end of the master lever l8, which knob also may be rotatable and/or slidable on the lever
  • its slave lever I6 or I! is pulled sideways to disconnect it from the pin IE] on the master lever, and the slave lever would then be moved counterclockwise.
  • the slave lever H has been moved clockwise to open its throttle, a less likely but possible procedure, so shown for convenience in the drawing layout. Thereafter, control of the other powerplant would continue to be through the master lever.
  • the lever l8 carries an angularly disposed arm 28 at its lower end which forms an idling stop against the lower end of an adjustable screw 29 mounted in a pivoted nut bracket 30 and having a head 3
  • a spring 32 normally holds the screw 29 vertical in a position to intercept the end of the arm 28, thus defining the idling position.
  • a light spring 33, on top of the arm 28 facilitates the release of the idling stop when it is desired to move the master lever
  • the member 35 is conveniently split on its center line and serves to support the discs 34 and a central worm gear 36 therebetween, the worm gear being adjustable by means of a worm 31 operated by an external knob 38.
  • 9 on one side disc 34 will be at its top position and the pin IS on the other disc will be at its bottom position.
  • a stop 39 carried by the member 35, is adapted to cooperate with a cut-away part of one disc 34 to limit the range of movement thereof as best shown in Figure 2.
  • a throttle control arranged to permit both simultaneous and separate control of separate power plants
  • a pivoted master control lever pivoted slave control levers disposed on either side of said master lever, and operable independently thereof a shaft on which said master and slave levers pivot, said shaft having a flange on one end stationary friction members disposed on both sides of each slave lever, and adjustable handwheel threaded on the free end of said shaft and arranged to compress said friction members and levers together to vary the frictional resistance of said levers to pivotal movement, and means releasably engaging each of said slave levers to said master lever for the operation of either or both of said slave levers by said master lever.
  • a throttle control arranged to permit both simultaneous and separate control of separate power plants comprising a pivoted master control lever, pivoted slave control levers disposed on either side of said master lever, a shaft onwhich said master and slave levers pivot, stationary friction members disposed on both sides of each slave lever, adjustable means carried on said shaft and arranged to compress said friction members and levers together to vary the frictional resistance of said levers to pivotal movement, means releasably engaging each of said slave levers to said master lever for the operation of either or both of said slave levers by said master lever, and means to differentially adjust the position of said slave levers relative to the master lever when said slave levers are engaged to said master lever.
  • a throttle control arranged to permit both simultaneous and separate control of separate power plants comprising a pivoted master control lever, pivoted slave control levers disposed on either side of said master lever, a shaft on which said master and slave levers pivot, stationary friction members disposed on both sides of each slave lever, adjustable means carried on said shaft and arranged to compress said friction members and levers together to vary the frictional resistance of said levers to pivotal movement, means carried by the master lever and located between said slave levers comprising a transverse shaft having eccentric pins oppositely disposed and each engageable with one of said slave levers, and means to rotate said shaft to differentially adjust said slave levers relative to the master lever.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)

Description

1952 c. 0. STEWART DUAL THROTTLE CONTROL 2 SHEETSSHEET 1 Filed Dec. 7, 1948 INVENTOR.
. CHARLES D. STEWART Agent C. D. STEWART DUAL THROTTLE CONTROL Oct. 14, 1952 2 SHEETS-SHEET 2 Filed Dec. 7, 1948 IN VEN'I'OR. CHAR LES D. STEWART Age nt Patented Oct. 14, 1952 DUAL THROTTLE CONTROL Charles D. Stewart, Glendale, Calif., assignor to Lockheed Aircraft Corporation, Burbank, Calif.
Application December 7, 1948, Serial No. 63,988
This invention relates to an improved throttle control providing for the normal operation of two powerplants as a unit from a single master control lever, with provisions for close adjustment of synchronism, and overriding individual controls operable at the will of the pilot.
In multi-engined aircraft it has heretofore been the practice to provide individual throttle levers positioned side by side for simultaneous or individual operation by one hand of the pilot, the powerplants being substantially synchronized by minor independent movements thereof and/or thereafter accurately synchronized by speed responsive devices driven by the separate powerplants. Any of the powerplants could be separately shut down or operated, as in the case it was desired to assist in ground maneuvering. In twin engined single pilot aircraft, on the other hand, it is desirable to add other controls to the throttle lever, which would not be practical with separate levers, so that it has been necessary for the pilot to shift his hand from the throttles to adjacent separate controls for such auxiliary functions which ideally should be operable simultaneously with the throttle.
It is accordingly an object of this invention to provide a single master throttle lever or handle control having provisions for simultaneous and overriding individual adjustments or operation of the throttle or control levers for separate powerplants. The control lever for conventional type piston engines is commonly called the throttle as it operates a valve in the intake duct thereof. For convenience in what follows I am using the term throttle to also refer to the control lever of jet or propeller drive turbine powerplants where such levers control the fuel supply and when moved past the idle position cut off the fuel supply to stop such engines. While the embodiment hereinafter disclosed is primarily designed for the control of such turbine powerplants, it is equally suitable for use in controlling piston type engines. Such a master throttle control permits the addition of auxiliary controls to the hand grip thereof, which grip may carry switches and may be longitudinally and/or rotatably movable to control still other functions interrelated to the throttle control of the powerplant.
It is a further object of this invention to provide a master throttle control lever normally used to simultaneously operate individual slave throttle levers, which levers are disengageable from the master control for individual operation at the will of the pilot. A further refinement of this object is to provide a differential control for 3 Claims. (Cl. 74-471) adjusting the position of the slave throttle levers relative to'the master control lever whereby to enable close synchronization of the separate powerplants at an point in their range of operation.
It is also an object of this invention to provide a master throttle control of the type described incorporating an adjustable and releasable idling position stop, the release of which stop can be accomplished by a predetermined movement of the pilots throttle hand without necessitating a release of the flying controls by the pilots other hand. I It is also an object of this invention to provide a master and slave throttle control lever arrangement of the type described wherein the individual levers are subjected to an adjustable braking force adequate to maintain any relative adjustment of an individual lever unaffected by movements of the other levers.
Other and further objects and advantages of my invention will appear as the description of a selected embodiment thereof proceeds, and my invention is not limited to the specific device to be now described.
In the drawings:
Figure 1 is a perspective View, partly broken away for clearness, of a master and slave throttle lever arrangement embodying a specific form of my invention;
Figure 2 is a side elevation of the device of Figure l, with parts omitted for clearness;
Figure 3. is a central vertical section on the line 3-3 of Figure 4, showing details of the synchronizing adjustment;
Figure 4 is a fragmentary view from the left of Figure 2 showing thesynchmnizing adjustment mechanism to an enlarged scale; and
Figure 5 is a section on the line 5-5 of Figure 3. 1
As shown on the drawings, the throttle control of this invention is intended to be built into a side shelf ill in the cockpit ll of an airplane (not shown), and is intended to operate individual powerplant control rods l2 and I3 which extend to the powerplants themselves. In the case of piston type engines these rods would operate throttle valves for fuel injection controls, and in the case of turbine powerplants would operate fuel injection controls. For convenience, I will hereinafter refer to these controls as throttle controls. 7
In Figure 1 the throttle levers to be later described are pivoted on a stationary shaft l4 mounted by means of a flange I5 on the wall of ried by the upper ends of the slave levers. These I levers I6 and H are connected at their lower ends to the rods l2 and I3. As shown in Figure l, clockwise movements of the levers I6, I! and I8 tend to open the throttles of the powerplants, and counterclockwise motion of these levers closes the throttles.
Interposed between the slave lever l6 and the flange |5 is a stationary brakeelement 2| anchored to fixed structure at 22. This element 2| has a pin 23 which holds stationary a pair of discs 24 on either side of the lever IS. A second identical element 2| similarly holds stationary a second pair of the discs 24, located on either side of the other slave lever ll. Adjustable braking pressure is put on this assemblage by a hub 25 of a hand wheel 28 which hub is threaded on the shaft M and may be tightened as desired by the pilot to give sufficient friction for smooth operation of the levers and/or to hold them in their adjusted position if it is desired to take the hand off the master lever. The provision of stationary discs 24 between each of the movable parts assures that if either slave lever H5 or I1 is disconnected from the master lever it will remain in its set position, unaffected by subsequent movements of the master lever.
As described so far, the normal operation of the master lever carries both slave levers with it and the pilot merely has to grasp and push or pull on a knob 21 carried by the upper end of the master lever l8, which knob also may be rotatable and/or slidable on the lever |8 to actuate other accessory controls unrelated to the present disclosure. If it is desired to idle or shut down one powerplant, its slave lever I6 or I! is pulled sideways to disconnect it from the pin IE] on the master lever, and the slave lever would then be moved counterclockwise. As shown in Figure 2, the slave lever H has been moved clockwise to open its throttle, a less likely but possible procedure, so shown for convenience in the drawing layout. Thereafter, control of the other powerplant would continue to be through the master lever.
The lever l8 carries an angularly disposed arm 28 at its lower end which forms an idling stop against the lower end of an adjustable screw 29 mounted in a pivoted nut bracket 30 and having a head 3| projecting through a slot in the shelf ID. A spring 32 normally holds the screw 29 vertical in a position to intercept the end of the arm 28, thus defining the idling position. A light spring 33, on top of the arm 28 facilitates the release of the idling stop when it is desired to move the master lever |8 beyond that stop to shut down the powerplant. This spring 33 is adapted to be depressed upon pressure of the arm 28 towards the idle stop 29 and the brake knob 26 can be set tight enough to hold the lever =|8 in such position, so that the pilot can momentarily shift his throttle hand from the grip 21 to pull the knob 3| shifting the idle stop 29 off the spring 33 and clear of the end of the arm 28, in
4 which position the spring 33 will move up to hold the idle stop in its released position to permit a return of the pilots hand to the grip 21 to continue the counterclockwise movement of the throttle lever past its idle position to shut down the powerplants.
The pins [9, which normally look the slave levers l6 and I! for movement with the master lever I8, form, in effect, diametrically opposed crank pins projecting from crank discs 34 flush with the sides of a member 35 carried by the master lever l8. The member 35 is conveniently split on its center line and serves to support the discs 34 and a central worm gear 36 therebetween, the worm gear being adjustable by means of a worm 31 operated by an external knob 38. In the neutral position the pin |9 on one side disc 34 will be at its top position and the pin IS on the other disc will be at its bottom position. Rotation of the knob 33 in either direction will move one pin and its associated slave lever in a direction to slightly open its throttle and simultaneously moves the other pin and its associated slave lever in a direction to slightly close its throttle. Thus the two powerplants can be closely synchronized in any position of the master lever, yet either slave lever can be pulled sidewise off its pin l9 and moved independently of the master lever to either open or close the throttle controlled thereby, leaving the master lever free to continue to operate the other slave lever if so desired. A stop 39, carried by the member 35, is adapted to cooperate with a cut-away part of one disc 34 to limit the range of movement thereof as best shown in Figure 2.
It will thus be seen that I have invented an improved and simplified throttle control for dual powerplants wherein either powerplant can be separately operated at will and wherein close synchronization of the separate throttles can be attained without the use of complicated power driven synchronizing apparatus.
I claim:.
1. A throttle control arranged to permit both simultaneous and separate control of separate power plants comprising a pivoted master control lever, pivoted slave control levers disposed on either side of said master lever, and operable independently thereof a shaft on which said master and slave levers pivot, said shaft having a flange on one end stationary friction members disposed on both sides of each slave lever, and adjustable handwheel threaded on the free end of said shaft and arranged to compress said friction members and levers together to vary the frictional resistance of said levers to pivotal movement, and means releasably engaging each of said slave levers to said master lever for the operation of either or both of said slave levers by said master lever.
2. A throttle control arranged to permit both simultaneous and separate control of separate power plants comprising a pivoted master control lever, pivoted slave control levers disposed on either side of said master lever, a shaft onwhich said master and slave levers pivot, stationary friction members disposed on both sides of each slave lever, adjustable means carried on said shaft and arranged to compress said friction members and levers together to vary the frictional resistance of said levers to pivotal movement, means releasably engaging each of said slave levers to said master lever for the operation of either or both of said slave levers by said master lever, and means to differentially adjust the position of said slave levers relative to the master lever when said slave levers are engaged to said master lever.
3. A throttle control arranged to permit both simultaneous and separate control of separate power plants comprising a pivoted master control lever, pivoted slave control levers disposed on either side of said master lever, a shaft on which said master and slave levers pivot, stationary friction members disposed on both sides of each slave lever, adjustable means carried on said shaft and arranged to compress said friction members and levers together to vary the frictional resistance of said levers to pivotal movement, means carried by the master lever and located between said slave levers comprising a transverse shaft having eccentric pins oppositely disposed and each engageable with one of said slave levers, and means to rotate said shaft to differentially adjust said slave levers relative to the master lever.
CHARLES D. STEWART.
6 REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number
US63988A 1948-12-07 1948-12-07 Dual throttle control Expired - Lifetime US2613547A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US63988A US2613547A (en) 1948-12-07 1948-12-07 Dual throttle control

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US63988A US2613547A (en) 1948-12-07 1948-12-07 Dual throttle control

Publications (1)

Publication Number Publication Date
US2613547A true US2613547A (en) 1952-10-14

Family

ID=22052799

Family Applications (1)

Application Number Title Priority Date Filing Date
US63988A Expired - Lifetime US2613547A (en) 1948-12-07 1948-12-07 Dual throttle control

Country Status (1)

Country Link
US (1) US2613547A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2747426A (en) * 1952-10-16 1956-05-29 Caterpillar Tractor Co Engine speed control mechanism
US2947191A (en) * 1959-02-05 1960-08-02 Morse Instr Co Single lever marine engine control
US3049939A (en) * 1961-04-03 1962-08-21 Deere & Co Control mechanism
US3101821A (en) * 1958-04-09 1963-08-27 Mcculloch Corp Motor control
US4012015A (en) * 1975-12-29 1977-03-15 Northrop Corporation Control and synchronization of twin engines with a master throttle lever
US4524632A (en) * 1984-03-29 1985-06-25 Mtd Products Inc. Selecting mechanism
US20060230871A1 (en) * 2005-04-18 2006-10-19 Shuji Iekura Control device for marine propulsion system

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1269581A (en) * 1916-02-08 1918-06-18 Daimler Motoren Mechanism for controlling driving means.
US1454505A (en) * 1919-03-31 1923-05-08 Curtiss Aeroplane & Motor Co Multiple control system for multimotored aircraft
US1641567A (en) * 1924-09-27 1927-09-06 Walter H Barling Aircraft-motor-control system
US1889295A (en) * 1930-10-09 1932-11-29 Fiat Spa Differential and simultaneous control for the engines of multiple engine machines
US1994651A (en) * 1933-01-30 1935-03-19 North American Aviation Inc Vernier adjusting control unit
US2071177A (en) * 1934-07-25 1937-02-16 Gen Electric Engine throttle control
US2185160A (en) * 1938-02-05 1939-12-26 Tampier Rene Device for actuating the controls on aircraft
US2235013A (en) * 1936-11-03 1941-03-18 Wright Aeronautical Corp Multiple control
US2265260A (en) * 1938-11-21 1941-12-09 Kay Brunner Steel Products Inc Mechanism for selectively operating valves
US2313768A (en) * 1941-05-24 1943-03-16 Donald L Putt Control lever
US2319908A (en) * 1940-12-06 1943-05-25 Ind Patents Corp Container filling and weighing apparatus
US2439393A (en) * 1945-08-03 1948-04-13 Ralph W Kerr Synchronized control unit

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1269581A (en) * 1916-02-08 1918-06-18 Daimler Motoren Mechanism for controlling driving means.
US1454505A (en) * 1919-03-31 1923-05-08 Curtiss Aeroplane & Motor Co Multiple control system for multimotored aircraft
US1641567A (en) * 1924-09-27 1927-09-06 Walter H Barling Aircraft-motor-control system
US1889295A (en) * 1930-10-09 1932-11-29 Fiat Spa Differential and simultaneous control for the engines of multiple engine machines
US1994651A (en) * 1933-01-30 1935-03-19 North American Aviation Inc Vernier adjusting control unit
US2071177A (en) * 1934-07-25 1937-02-16 Gen Electric Engine throttle control
US2235013A (en) * 1936-11-03 1941-03-18 Wright Aeronautical Corp Multiple control
US2185160A (en) * 1938-02-05 1939-12-26 Tampier Rene Device for actuating the controls on aircraft
US2265260A (en) * 1938-11-21 1941-12-09 Kay Brunner Steel Products Inc Mechanism for selectively operating valves
US2319908A (en) * 1940-12-06 1943-05-25 Ind Patents Corp Container filling and weighing apparatus
US2313768A (en) * 1941-05-24 1943-03-16 Donald L Putt Control lever
US2439393A (en) * 1945-08-03 1948-04-13 Ralph W Kerr Synchronized control unit

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2747426A (en) * 1952-10-16 1956-05-29 Caterpillar Tractor Co Engine speed control mechanism
US3101821A (en) * 1958-04-09 1963-08-27 Mcculloch Corp Motor control
US2947191A (en) * 1959-02-05 1960-08-02 Morse Instr Co Single lever marine engine control
US3049939A (en) * 1961-04-03 1962-08-21 Deere & Co Control mechanism
US4012015A (en) * 1975-12-29 1977-03-15 Northrop Corporation Control and synchronization of twin engines with a master throttle lever
US4524632A (en) * 1984-03-29 1985-06-25 Mtd Products Inc. Selecting mechanism
US20060230871A1 (en) * 2005-04-18 2006-10-19 Shuji Iekura Control device for marine propulsion system
US7665381B2 (en) * 2005-04-18 2010-02-23 Yamaha Hatsudoki Kabushiki Kaisha Control device for marine propulsion system

Similar Documents

Publication Publication Date Title
CA2718080C (en) Rotational aircraft throttle interface
CA2804801C (en) Pilot control system with adjustable pedals
EP2626297B1 (en) Integrated aircraft flight control units
US2665085A (en) Selective dual aileron control for aircraft
EP2626300B1 (en) Pilot control system with hand rest
US2613547A (en) Dual throttle control
EP0120011A4 (en) Modular multi-engine thrust control assembly.
US11634236B2 (en) Pilot interface for aircraft autothrottle control
US2057877A (en) Automatic torque control for aircraft
US2442289A (en) Airplane control system
US2639108A (en) Airplane trim control
US2407322A (en) Differential control device
US3375605A (en) Model plane flight control device
US3107881A (en) Control system for interconnected propellers
US2242314A (en) Control device for aircraft
US2959374A (en) Jet-powered rotorless convertible aircraft
US3168265A (en) Control system for aircraft with slow flight or hovering characteristics, in particular for vertically starting and landing aircraft
US2940696A (en) Differential mixer
US2608104A (en) Throttle system for jet engines
US3056455A (en) Turboprop control
US2450261A (en) Training equipment for aviators
US2334504A (en) Aircraft structure
US3045957A (en) Auxiliary feel system
US3041018A (en) Aircraft adapted for vertical take-off and landing
US2240259A (en) Aircraft