US1006276A - Combined compound crank and rotary engine. - Google Patents
Combined compound crank and rotary engine. Download PDFInfo
- Publication number
- US1006276A US1006276A US59243310A US1910592433A US1006276A US 1006276 A US1006276 A US 1006276A US 59243310 A US59243310 A US 59243310A US 1910592433 A US1910592433 A US 1910592433A US 1006276 A US1006276 A US 1006276A
- Authority
- US
- United States
- Prior art keywords
- rotor
- engine
- exhaust
- crank
- rotary engine
- 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
Links
- 150000001875 compounds Chemical class 0.000 title description 3
- 239000007789 gas Substances 0.000 description 8
- 238000002485 combustion reaction Methods 0.000 description 4
- 238000010276 construction Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 230000000153 supplemental effect Effects 0.000 description 2
- ZPUCINDJVBIVPJ-LJISPDSOSA-N cocaine Chemical compound O([C@H]1C[C@@H]2CC[C@@H](N2C)[C@H]1C(=O)OC)C(=O)C1=CC=CC=C1 ZPUCINDJVBIVPJ-LJISPDSOSA-N 0.000 description 1
- 230000002301 combined effect Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000000979 retarding effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B41/00—Engines characterised by special means for improving conversion of heat or pressure energy into mechanical power
- F02B41/02—Engines with prolonged expansion
- F02B41/10—Engines with prolonged expansion in exhaust turbines
Definitions
- SHEETS SHEET 2 if Mr 12' g V v j .v a
- My invention relates to engines, either gas or steam, and pertains especially to means for utilizing the exhaust of the engine for propelling iiurposes.
- the invention consists ot the parts and the combination and construction of pub: hereinafter more fully described anu claimed, having reference to the tl(.'tt)lli] ).
- w,hieh- Figure 1 is an elevation and partial section of the. invention as applied to an internal combustion engine.
- Fig. 2 is a side elevation of the rotor ei'nployedin Fig. 1.
- Fig. 3 represents the invention applied to Fig. ,4 is a side elevation of the rotor of Fig. 3.
- A represents one or more reciprocating gas engines operating with a crank shaft 2.
- 3 is'au exhaust pipe leading from each engine and each pipe having a nozzle or inlet 4 delivering into ⁇ teasing 5 in which is the rotor (3.
- the latler is of any suitable description and is preferably disposed between the engines and secured to the crank shaft 2, as shown in Fig. 1.
- the periphery of the rotor is provided with a series of buckets or pockets 7 which run inside of a stationary rim or housing 8; the pockets being adapted to receive the intermittent jets from the exhaust through the nozzles 4, and later to release these gases through suitable exhaust ports 9, into a common exhaust pipe 10'.
- the sides of the rotor running in the stationary rim 8 may be packed on either side by suitable yielding or springressed packing ringsll, for the par ose o? maintaining a tight joint and con ning the gases in the pockets between aninlet 4 and a succeeding -exhaust port 9.
- the rim 8 may be made in sections and bolted together, as shown at 12, Fig. 2, and suitably secured on the engine frame.
- the ex lodcd gases in the cylinder of an engine acts, first, under expansion to drive the piston w-forward to operate the crank shaft like in any ordinary reciprocating engine.
- the exhaust from pipe 3 is delivered through its nozzle 4: against the buckets 7 of the rotor 6, after the fashion of an impulse water wheel.
- the rraetance on the. rotor due to the jet impulses is proportionate to the'foree of two jet and the diameter of the rotor. In many cases these exhaust jets are made with a great. deal of force from the engine. and where there is a plurality-0f e ⁇ -'linder.
- the rotor is in eifcct a supplemental engine operated by the exhaust and acting conjointly with the main engine to drive the crank shaft.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Silencers (AREA)
Description
G. G. RICHARDS.
COMBINED COMPOUND CRANK AND ROTARY ENGINE.
APILHA'I'ION IJLEIJ NOV, 15. 1910.
1,006,276. Patented Oct. 17, 1911 V 2 BHEETB8HEET I 4 T22 E a G. C. RICHARDS. COMBINED COMPOUND CRANK AND ROTARY ENGINE. APPLICATION TILED NOV. 15. 1910.
2 SHEETS SHEET 2 if Mr 12' g V v j .v a
i J I 1 i I I @raggfxizf @JMJ ' Patented Oct. 17, 1911.
twin reciprocating steam engines.
GEORGE C. RICHARDS, OF
BERKELEY, CALIFORNIA.
COMBINED COMPOUND CRANK AIhTD ROTARY ENGINE.
1 ,ooogms.
Specification of Letters Patent.
Patented Oct. 17, 1911.
Application filed November 15. 1910. Serial No, 592,483.
Toot! whom it 1:10.11] concern:
lie it known that l, (ii-:ouou RICHARDS, citizen of the. United States, residing at Berkeley, in the county of Alameda and State of California, have. invented new and useful improvements in onihinerl (onipound. Crank and ltotary Engines, of which the following is a specification;
My invention relates to engines, either gas or steam, and pertains especially to means for utilizing the exhaust of the engine for propelling iiurposes.
The invention consists ot the parts and the combination and construction of pub: hereinafter more fully described anu claimed, having reference to the tl(.'tt)lli] ).'lll ing drawings, in w,hieh- Figure 1 is an elevation and partial section of the. invention as applied to an internal combustion engine. Fig. 2 is a side elevation of the rotor ei'nployedin Fig. 1. Fig. 3 represents the invention applied to Fig. ,4 is a side elevation of the rotor of Fig. 3.
As shown in Fig. 1, A, represents one or more reciprocating gas engines operating with a crank shaft 2. 3 is'au exhaust pipe leading from each engine and each pipe having a nozzle or inlet 4 delivering into {teasing 5 in which is the rotor (3. The latler is of any suitable description and is preferably disposed between the engines and secured to the crank shaft 2, as shown in Fig. 1. The periphery of the rotor is provided with a series of buckets or pockets 7 which run inside of a stationary rim or housing 8; the pockets being adapted to receive the intermittent jets from the exhaust through the nozzles 4, and later to release these gases through suitable exhaust ports 9, into a common exhaust pipe 10'. The sides of the rotor running in the stationary rim 8 may be packed on either side by suitable yielding or springressed packing ringsll, for the par ose o? maintaining a tight joint and con ning the gases in the pockets between aninlet 4 and a succeeding -exhaust port 9.
The rim 8 may be made in sections and bolted together, as shown at 12, Fig. 2, and suitably secured on the engine frame.
In practice, the ex lodcd gases in the cylinder of an engine acts, first, under expansion to drive the piston w-forward to operate the crank shaft like in any ordinary reciprocating engine. On the return stroke pipe 3 and it is the utilization of this exaust by the means herein employed that constitutes the essence of the present invention. The exhaust from pipe 3 is delivered through its nozzle 4: against the buckets 7 of the rotor 6, after the fashion of an impulse water wheel. The rraetance on the. rotor due to the jet impulses is proportionate to the'foree of two jet and the diameter of the rotor. In many cases these exhaust jets are made with a great. deal of force from the engine. and where there is a plurality-0f e \-'linder. operating in unison the combined effect of the exhaust from all of them is practically continuous, and the nozzles may be arranged so as to deliver these. exhaust jets around a considerable aortion of the circumference of the rotor. has, I utilize the otherwise lost power latent in the exhaust gases, positively to drive the engine. The result of this construction is the eombined compound crank and rotary internal combustion engine.
lnFigs. Ii'and 4,. u'hile steam is used'the principle of eompouhding is essentially the same. in this latter case the exhaust steam from the cylinders A is delivered to the exhaust. pipes 23' into an e\iniust chamber 5', which has arseries of utlets or nozzles adapted to discharge at a suitable incline into the. peripheral pockets 7' of the rotor ii. The expanded compounded steam is trapped in the pockets by the inner wall of the chamber 5', until the pockets pass beyond, and exhaustat 9. r
It is manifest that there may be any number of engines working either singly or in pairs, -or according to any other desired group arrangement, and the rotor 6 or (5 may be'sccured at any suitable place on the crank sh aft.
Not only is the exhaust utilized to drive a fluid impulse rotor, but the latter in turn with its buckets and easing operates as a mutiler, andall without materially retarding the speed'of the engine.
.The rotor is in eifcct a supplemental engine operated by the exhaust and acting conjointly with the main engine to drive the crank shaft.
It is manifest that the principle would be the same in regard to the. supplemental engine if a part ofthe'originnl explosive or impelhn charge were directed against the. rotor. lh fact the rotor may he impelled of the piston a, exhaust takes place through i from any source'of fluid pressure generated 'vices interposed between the ring an avin thus described 'my. invention,
what I c aim and desire tosecure'by Letters Patent is- 1. The combination in an engine, of a crank shaft, 3, series of internal combustion engines connected to the shaft, a casing having bearings supporting the shaft, a rotor between the engmes on the shaft :1 ring in the casing circumferentially inciosing. the rotor and ha-Vin jet-openings whereby exhaust gas from t e enlgines maiy against the rotor, an yieldah e packin d: t e faces of the rotor to prevent leakage.
2. The combination in an engine, ofa. crank shaft, a series of internal combustion engines connected tothe shaft, a casing havbe projected 1 devices comprising ing bearings supporting the shaft, a rotor 20 between the engines on the shaft, a ring in .the casing oircumferentially inclosing the rotor and havin jet openings whereby exhaust gas from t e engines ma be projectedagainst the rotor, and yieldab e packin de- 25 vices interposed between the rin an the faces of the rotor to revent lea age, said ands mounted for transverse movement in under cut recesses in the casing ringand adapted to bear upon the side faces of the'ro'tor.
,In testimony whereof I have hereunto set hand in the 'presence of two subscribing witnesses.
, GEORGE C; RICHARDS.
Witnesses: Cmmnns EDELMAN, A. P: LATHROP.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US59243310A US1006276A (en) | 1910-11-15 | 1910-11-15 | Combined compound crank and rotary engine. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US59243310A US1006276A (en) | 1910-11-15 | 1910-11-15 | Combined compound crank and rotary engine. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1006276A true US1006276A (en) | 1911-10-17 |
Family
ID=3074590
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US59243310A Expired - Lifetime US1006276A (en) | 1910-11-15 | 1910-11-15 | Combined compound crank and rotary engine. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1006276A (en) |
-
1910
- 1910-11-15 US US59243310A patent/US1006276A/en not_active Expired - Lifetime
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US1310157A (en) | Planoorapii co | |
| US2544480A (en) | Rotary displacement device | |
| US1705130A (en) | Internal-combustion engine | |
| US1923561A (en) | Rotary combustion engine | |
| US1006276A (en) | Combined compound crank and rotary engine. | |
| US1239694A (en) | Rotary engine. | |
| US1482627A (en) | Rotary internal-combustion engine | |
| US1331749A (en) | Internal-combustion engine | |
| US1503741A (en) | Packing plate for internal-combustion engines or the like | |
| US2248484A (en) | Heat energized apparatus | |
| US1236009A (en) | Rotary engine. | |
| US937653A (en) | Internal-combustion engine. | |
| US938253A (en) | Combined turbine-muffler and fly-wheel. | |
| US1122403A (en) | Rotary engine. | |
| US1717739A (en) | Rotary engine | |
| US892443A (en) | Rotary engine. | |
| US1202828A (en) | Internal-combustion engine. | |
| US1353687A (en) | Turbine-engine | |
| US1246885A (en) | Internal-combustion rotary engine. | |
| US1536245A (en) | Rotary piston engine | |
| US1038295A (en) | Turbine. | |
| US1270546A (en) | Rotary motor. | |
| US426976A (en) | Rotary engine | |
| US1308896A (en) | Znternal-combtjstioit rotary | |
| US1173327A (en) | Rotary engine. |