US2389663A - Marine power unit - Google Patents

Marine power unit Download PDF

Info

Publication number
US2389663A
US2389663A US443230A US44323042A US2389663A US 2389663 A US2389663 A US 2389663A US 443230 A US443230 A US 443230A US 44323042 A US44323042 A US 44323042A US 2389663 A US2389663 A US 2389663A
Authority
US
United States
Prior art keywords
gear
propeller
engine
units
shaft
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
US443230A
Inventor
Forsyth Archibald Graham
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.)
Fairey Aviation Co Ltd
Original Assignee
Fairey Aviation Co Ltd
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 Fairey Aviation Co Ltd filed Critical Fairey Aviation Co Ltd
Priority to US443230A priority Critical patent/US2389663A/en
Application granted granted Critical
Publication of US2389663A publication Critical patent/US2389663A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H5/00Arrangements on vessels of propulsion elements directly acting on water
    • B63H5/07Arrangements on vessels of propulsion elements directly acting on water of propellers
    • B63H5/08Arrangements on vessels of propulsion elements directly acting on water of propellers of more than one propeller
    • B63H5/10Arrangements on vessels of propulsion elements directly acting on water of propellers of more than one propeller of coaxial type, e.g. of counter-rotative type

Description

Nov. 27, 1945. A FORS'YTH 2,389,663
MARINE. POWER UNIT Filed May 16, 19,4; 3 Sheets-Sheet 1 Nov. 2?, 1945. FQRSYTH I 2,389,663
MARINE POWER UNIT Filed May 16. 1942 I 3 Sheets-Sheet 2 W u K I gs mu 067M041 Nov .27,1945. A. G. FORSYTH 6 MARINE POWER UNIT Filed May 16, 1942 3 Sheets-Sheet 3 3 wua/wfom Patented Nov. 27, 1945 MARINE POWER UNIT Archibald Graham Forsyth, Cheam, England, as-
signor to IJhe Fairey Aviation Company Lime ited, Hayes, Middlesex, England Application May 16, 1942, Serial No. 443,230
(Cl. 115-3'l) 8 Claims.
This invention relates to power plants for high speed marine torpedo boats. and the like, and particularly to a power plant suitable for mass production.
Generally speaking, boats of this type have been equipped with airplane engines which have been converted or adapted in an attempt to meet the special requirements of torpedo craft. Such converted or adapted arrangements have presented difliculties and drawbacks and have not been wholly satisfactory.
In a preferred form of the invention, power units are employed, each of which may advantageously consist of a 12-cylinder internal combustion engine, with two of such identical units being disposed in longitudinal alignment with the driving ends of the crankshafts of said units facing, but spaced from each other by a gear housing, the gearing in said gear housing being suitably connected to drive two marine propellers. One object of the invention is to provide such an arrangement.
Another object of the invention is to provide such an arrangement with interchangeable superchargers, each engine being provided with a faced opening adapted detachably to receive a supercharger to be mechanically driven by the crankshaft, the faced openings when no superchargers are attached, being closed by a cover plate or the like. Such an arrangement gives rise to the, advantage of effecting satisfactory balancing of the running times of the engines, as will later appear, so that the craft may remain in operation for longer periods between overhauling than heretofore.
Still another object of the invention resides in the provision of a power plant which may be simply adjusted to obtain, with maximum efliciency, the necessary power and speed for various types of operating conditions.
The invention has for another object the provision of a power plant which with two units provides four engine reliability and which may be used for driving contra-rotating propellers. One feature of the invention resides in the provision of means for changing the pitch of the propeller blades.
Still anotherobject of the invention resides in the provision of a power plant for marine torpedo boats with which all conditions of operation are covered by the combination .of engines employed.
The invention provides a power plant which is easily and simply adjusted or repaired, the parts being readily accessible, thereby assisting production and maintenance, It is an object of the invention to provide such a power plant.
Another important object of the invention resides in providing a power plant having a low weight power ratio.
These and other objects of the invention will become more apparent from the following detailed description and claims when read in conjunction with the accompanying drawings, in which:
Figure 1 is a side elevation of a powerplant assembly according to the invention, the drive shafts for the propellers being broken 01f because of their length.
Figure 1A is a side elevation of the remainder of the propeller drive shaft.
Figure 2 is a view on the line 2-2 of Figure 1.
Figure 3 is a vertical longitudinal section through the gear housing.
Figure 4 is a sectional view of the gearing for changing the pitch of the propellers, illustrated diagrammatically.
Figure 5 is a view on the line 5-.-5 of Figure 3, and
Figure 6 is a fragmentary sectional view showing a part of the pitch changing gearing.
The general layout of the power plant is shown in Figures 1 and 2. The power plant in this instance is preferably constituted of two l2-cylinder internal combustion engines A and B, each consisting of two banks of six cylinders. These engines are of identical design and both have the same direction of rotation. The .engines are placed end to end, the motor casing at the juncture forming a housing for a gear box, a portion of which 2 extends downwardly below the engines.
The gearing within the gear box is adapted to drive the propellers C and D, the propeller C being driven by engine 13, and the propeller D by the engine A, thus providing an arrangement for contra-rotating propellers. The specific gearing arrangements for driving the propellers will be described in detail hereinafter.
The power unit may also include advantageously an electric motor 4 which is connected in such manner as to change the pitch of propeller D when it is operated. Consequently, it is possible with such an arrangement to use the propeller D for reversing.
Each engine is provided with two side facings 6 (one on each motor side), which facings are adapted to-have mechanically driven.
superchargers, such as -B detachably secured thereto. These superchargers should-be large The intakes l2 of the superchargers B are:
Any suitable clutching arprovided with throttles l4 to prevent overboosting and these are operated by boost-controls l6.-
Air may be supplied to' both engines through the manifold I8, and passes to the engines through downdraught carburetors 26, each of which is also provided with a screened intake opening 22 which is controlled by a throttle.
The manifold I6 is also provided with two throttles 26, 28 disposed intermediate the two engines- With the power unit as thus described each engine may be operated separately, or both together. Moreover, it is possible to run eachengine normally aspirated, in which event the throttle 24 is open so that air may reach the carburetor 20 through the screened intake 22 In this event the superchargers 6 of that engine should be declutched, I When it is desired to run an engine supercharged, the superchargers 8 of that engine may be clutched in so as to be driven by the engine crankshaft and the throttle 24 of the carburetor should be closed. If desired, any suitablearrangement (not shown) may be provided so that when the supercharger is clutched in, the throttle 24 will be closed, and when the supercharger is declutched, the throttle24 will be open.
Moreover, both engines can; be operated simultaneously and supercharged for maximum speed.
One important feature of the invention which is effected through the power unit, -described,'
is that it permits the running time of theengines to be balanced. Forexample, in, use it will probably be true that one engine, such as A, will be used for minimum cruising, normally.
aspirated, more than the other, which, being provided with a supercharger, would only ,be used occasionally when maximum cruising and maximum speed is required. Consequently, engine A would be subjected to more wear over a given period of time than engine B. With the usual arrangement it would be necessary to remove the power unit for servicing; However, withthe present invention, a balancing may be effected by using the other engine B for minimum cruising. The superchargers on engine A can be detached from that engine and placed on engine B on the facings 6. The boat can thus be kept in service without engine removal for the maximum time between overhauling. In;
gine from a minimum cruising engine'to a maximum speed engine. Because of the arrangement of the facings, manifold, etc, such a change creates no difficulties.
, The particular gearing arrangements for driving the propellers C and D may be as illustrated in Figures 2, 3, 5 and 6. Figure 2 is a view on the line 2-2 of Figure 1, and shows the splined crankshaft ends 36 and 32 of the two motors of engine B. As shown in Figure 3 a gear box is disposed between engines A and B. The splined crankshaft ends 30 and 32 are adapted to have gears 34 mounted thereon. These gears 34 engage an intermediate gear 36 mounted for rotation in' bearings 38. The intermediate gear 36 in turn engages a gear 40 which is disposed on the inner end of a hollow drive shaft 42. The ther end of shaft 42 is secured to the hub of propeller C so as to rotate the propeller hub and the propeller blades (in this instance three) mounted thereon. The inner end-of shaft 42 is suitably journaled in bearings 44 in the gear housing.
From the above it should be evident that operation of either motor of engine B will, through the'gearing described, drive propeller C.
It will be seen from Figure 3 that the gear housing is divided by a partition 46 and that gearingsimilar to that just described is suitably mounted in the space to the left of the partition to be driven by the splined crankshaft ends of engine A. Specifically, the crankshaft ends of engine A have gears 48 mounted thereon. These engage an intermediate gear 56 which in turn engages a gear 52 disposed on the inner end of hollow drive shaft 54. The shaft 54 is concentric with, and surrounds, shaft 42. The outerend of shaft 54 is connected with the hub'qf propeller D. Operation of either orboth of the motorsof engine A will, through 'the gearing described, rotate the propeller hub of the propellers; D
Manifestly then, the invention provides an arrangement in accordance with which one propeller is driven by one or both of themoto rs of one engine (such as'B) while the other propeller is likewise driven by one or both of the motors of the other engine'iA). Four motor reliability is thus provided. t l I v Under certain conditions it maybe desirable to change the pitch of the blades of oneof the propellers to feather thmor to provide for reversing. Such a change may be effected through mechanism which will now be described. e
With reference to Figure 3, the lower end of the gear housing has an extension 56 to which is secured the electric motor 4. The drive shaft 58 of this motor is provided with a gear wheel 60 which engages a gear wheel 62 carried by the motor housing. Gear wheel 62 in turn engages gear teeth on the inner peripheryof a wheel 64 secured tothe inner end of a hollow shaft 66, so that operation of the electric motor 4, through this gearing will rotate shaft 66. V
Disposed within hollow shaft 66 is another shaft 68, the inner end of which is secured-by bracket 16 to the end of the extension 56. ;-As shown in Figure 3 the bracket may have a flange 12, which when the arrangement is assembled is disposed between'the end of extension 56 and a flange 14 on the housing of electric motor4, As shown in dotted lines the bracket 11] must have a cut-away portion H to provide passage space for thegear 62.
Both the hollow shaft 66 and the shaft 68, dis posed therein, are themselves disposed within the hollow shaft 42 and run to the rear to'the hub of propeller D.
With reference to Figure 4 it willbeseenthat the end of shaft 68 is provided with a gear wheel 16 which engages idle gears 18 mountedio n a shaft 86 carried by'a freely" rotatable spider62. The idle gears 18 engage gear teeth on the inner circumference of the propeller hub 84 of proviously described, the idle gears 18 move around i the gear 16.
The hollow shaft 66, which as described, is adapted to be rotated by the electric motor 4, is provided at its outer end with a gear wheel 86 which engages gear wheels 88 carried by the spider 82. These in turn engage gear teeth on the inner circumference of a sleeve 90. The sleeve 90 is mounted for rotary movement within the hub 84. This sleeve 99 is provided, with an annular flange 92 provided on its outer periphery with gear teeth S-iwhich engage a gear wheel 96 mounted on a shaft 98 carrying a worm gear I00. This worm engages a gear ring H32 mounted ion the root m4 of th propeller blade Int (see Figure 6).
While only one propeller blade is shown in Figures 4 and 6, actually there may be three such blades on the propeller hub and by duplication of the gearing within the hub it is, of course, possible to change the pitch of the blades simultaneously and to the same degree.
In effecting a change in pitch it obviously is only necessary to operate the electric motor as through the gearing, shaft 66 will be rotated thus through gears 86, 88 rotating the sleeve 90, the
gear 96, worm I86 and ring gear Hi2 thus turn tending within said gear housing, said gear housing having a downwardly extending portion, a pair of drive shafts having one end disposed in said downwardly extending portion, the other ends of said shafts being connected each to a propeller hub, gearing connecting the crankshafts of .one of said units with one of said drive shafts and the crankshafts of the other unit with the other of said drive shafts, said drive shafts being hollow, and propeller blade pitch changing means passing through the inner hollow shaft.
2. A marine propulsion system for torpedo boats and the like, comprising two internal combustion engine units joined end to end with a gear housing therebetween, a pair of hollow propeller drive shafts, a pair of propellers, the hubs of which are each mounted on a drive shaft, gearing means connecting said internal combustion engine units to drive said shafts, gear means in one of said propeller hubs for changing the pitch of the blades on said hub when said means is actuated, a pitch control shaft being connectedat one end to said gear means, said pitch control shaft being disposed within the inner hollow drive shaft, and motor means connected to 'the other end of said pitch control shaft.
3. A marine propulsion system for torpedo boats and the like, comprising two internal combustion engine units joined end to end with a gear housing therebetween, a pair of hollow propeller drive shafts, a pair of propellers, the hubs of which are each mounted on a drive shaft,
. gearing means connecting said internal combustion engine units to drive said shafts, gear means .in. one of saidLpropeIIer hubs for changing the pitch of the blades on said hub when said means is actuated,.a pitch control shaft being connected .at oneend to said gear means, said pitch control shaft being disposed within the inner hollow drive shaft, and motor means connected to the other end of said pitch control shaft, said motor means comprising an electric motor disposed on said gear housing, and said gear. means including a ring gear rigid with the propeller blade root, and a worm gear engaging said ring I5 .geary; whereby a propeller blade may be turned 360 or less as determined by the time of operation of the electric motor.
4. A marine propulsion system for torpedo boats and the like, comprising two internal combustion engine units joined end to end with a gear housing therebetween, each of said units having at least one opening on the sides of the crankcases adjacent the rear ends of the crankshafts of said units, whereby superchargers or covers selectively may be detachably securedover said side openings, each of said units comprising two internal combustion engines with the crankshafts of said engines disposed within a common crankcase, the ends of said crankshafts extending within said gear housing, said gear housing having a downwardly extending portion, a pair of drive shafts having one end disposed in said downwardly extending portion, the other ends of said shafts being connected each to a propeller hub, gearing connecting the crankshafts of one of said units with one of said drive shafts and the crankshafts of the other unit with the other of said drive shafts, said drive shafts being hollow, and propeller blade pitch changing means passing through the inner hollow shaft.
5. A marine propulsion system for torpedo boats and the like, comprising two internal combustion engine units joined end to end with a gear housing therebetween, each of said units having at least one opening on the sides of the crankcases adjacent the rear ends of the crankshafts of said units, whereby superchargers or covers selectively may be detachably secured over said side openings, a pair of hollow propeller drive shafts, a pair of propellers, thehubs of which are each mounted on a drive shaft, gearing means connecting said internal combustion engine units to drive said shafts, gear means in one of said propeller hubs for changing the pitch of the blades on said hub when said means is actuated, a pitch control shaft being connected at one end to said gear means, said pitch control shaft being disposed within the inner hollow drive shaft, and motor means connected to the other end of said pitch control shaft.
6. A marine propulsion system for torpedo boats and the like, comprising two internal combustion engine units joined end to end with a gear housing therebetween, each of said units having at least one opening on the sides of the crankcases adjacent the rear ends of the crankshafts of said units, whereby superchargers or covers selectively may be detachably secured over said side openings, a pair of hollow propeller drive shafts, a pair of propellers, the hubs of which are each mounted on a drive shaft, gearing means connecting said internal combustion engine units to drive said shafts, gear means in one of said propeller hubs for changing the pitch of the blades on said hub when said means is actuated, a pitch control shaft being connected at one end to said gear means, said pitch control shaft being disposed within the inner hollow drive shaft, and motor means connected to the other end of said pitch control shaft ,said motor means 5 comprising an electric motor disposed on said gear housing, and said gear means including a ring gear rigid with the propeller blade root, and a worm gear engaging said ring gear, whereby a propeller blade may be turned 360 or less as determined by the time of operation of the electric motor.
'7. A marine propulsion system for torpedo boats and the like, comprising two internal combustion engine units joined end to end with a gear box therebetween, each of said units having openings on the sides near the rear ends, said openings being adjacent the rear ends of the crankshafts of said engine units, superchargers detachably secured over said side openings of one of said units, covers detachably secured over the openings of the other of said units, said superchargers and said covers being interchangeable, a pair of propeller hubs mounted for rotation about a common axis, a drive shaft secured to each propeller hub, and gearing in said gear box connecting one drive shaft with the crankshaft of one of said engine units and the other drive shaft with the crankshaft of the other engine unit.
78. A marine propulsion system for torpedo boats and the like, comprising two internal combustion engine units joined'end to end with a gear housing therebetween, each of said units having at least one opening on the sides of the crankcases adjacent the rear ends of the crankshafts of said units, a supercharger detachably secured over one of said openings on one of said units, a cover detachably secured over the other of said openings on the other of said units, each of said units comprising two internal combustion engines with the crankshafts of said engines disposed within a common crankcase, the ends of said crankshafts extending within said gear housing, a pair of concentrically disposed propeller drive shafts, and gear means within said housing connecting the crankshafts of one unit with one of said shafts and the crankshafts of the other unit with the other of said shafts.
ARCHIBALD GRAHAM FORSYTH.
US443230A 1942-05-16 1942-05-16 Marine power unit Expired - Lifetime US2389663A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US443230A US2389663A (en) 1942-05-16 1942-05-16 Marine power unit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US443230A US2389663A (en) 1942-05-16 1942-05-16 Marine power unit

Publications (1)

Publication Number Publication Date
US2389663A true US2389663A (en) 1945-11-27

Family

ID=23759936

Family Applications (1)

Application Number Title Priority Date Filing Date
US443230A Expired - Lifetime US2389663A (en) 1942-05-16 1942-05-16 Marine power unit

Country Status (1)

Country Link
US (1) US2389663A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3795463A (en) * 1971-07-21 1974-03-05 Herbert William Controllable pitch propeller and drive means therefor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3795463A (en) * 1971-07-21 1974-03-05 Herbert William Controllable pitch propeller and drive means therefor

Similar Documents

Publication Publication Date Title
US2372247A (en) Propeller drive for marine vessels
US2274743A (en) Air impeller device
US1466394A (en) Propulsion of aircraft
US2427846A (en) Power unit
US2470155A (en) Power plant assembly
US1874681A (en) Internal combustion engine
US2389663A (en) Marine power unit
US2350377A (en) Aircraft engine gearing
US1921893A (en) Propelling device
US1838974A (en) Internal combustion engine
US2165453A (en) Multiple engine power plant
US2505853A (en) Output shaft coupling mechanism for multiple power plants
US2127460A (en) Engine accessory drive
US2018794A (en) Mounting for internal combustion engines
US2426008A (en) Power unit for aircraft and the like
US2420764A (en) Directional propeller control
US2359045A (en) Motive plant for watercraft or aircraft
US2933892A (en) Angular free turbine rotor drive
US2027819A (en) Internal combustion engine
US2342672A (en) Aircraft power plant and propeller drive
US2540973A (en) Power transmission mechanism
US1905145A (en) Transmission
US2263449A (en) Airplane
US2426878A (en) Radial aircraft engine
GB764005A (en) Improvements in or relating to ship propelling installations