GB2280710A - Rotating and reciprocating piston i.c. engine. - Google Patents

Rotating and reciprocating piston i.c. engine. Download PDF

Info

Publication number
GB2280710A
GB2280710A GB9316191A GB9316191A GB2280710A GB 2280710 A GB2280710 A GB 2280710A GB 9316191 A GB9316191 A GB 9316191A GB 9316191 A GB9316191 A GB 9316191A GB 2280710 A GB2280710 A GB 2280710A
Authority
GB
United Kingdom
Prior art keywords
piston
internal combustion
combustion engine
engine
ignition
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.)
Withdrawn
Application number
GB9316191A
Inventor
Keith Andrew Maclaughan
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB9316191A priority Critical patent/GB2280710A/en
Publication of GB2280710A publication Critical patent/GB2280710A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01BMACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B3/00Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis
    • F01B3/0079Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis having pistons with rotary and reciprocating motion, i.e. spinning pistons
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/025Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/26Engines with cylinder axes coaxial with, or parallel or inclined to, main-shaft axis; Engines with cylinder axes arranged substantially tangentially to a circle centred on main-shaft axis

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Abstract

The piston 5 is secured to the main shaft 3 and rotates and moves axially between the cylinder heads 2 within a cylinder liner 1. Each piston stroke provides 90 DEG of shaft rotation. Ports 4 are controlled by the piston 5 during its helical motion. <IMAGE>

Description

INTERNAL COMBUSTION ENGINE This invention relates to an internal combustion engine, hereinafter referred to as the engine.
Internal combustion engines are well known and have many uses and applications as a source of power. Internal combustion engines in current applications are predominantly of the piston and crank design ( simple harmonic motion ). Despite continued development of this concept they remain inefficient and detrimental to the enviroment.
According to the present invention a design of engine not employing the piston and crank is provided to build an efficient power source.
The engine design can be summarised as: - the piston and output motion of the main shaft is as near to pure rotary and achieves the required compression cycle ( stroke ).
- on a single cylinder basis, double acting, there are four power strokes per revolution of the main shaft.
- the manufacture and production of the engine is simplified compared to current engines with considerably fewer moving parts and inherent parasitic losses.
- mechanical torque is constant throughout the power stroke.
- the engine does not require valves.
- lubrication and piston sealing is not expected to be a problem like prior rotary designs.
The design concept of the engine will now be described with reference to the accompanying drawings in which: Figure 1, this is a line drawing to illustrate the essential components of the engine. The piston 5 is secured to the main output shaft 3 and free to rotate and move axially within a cylinder liner 1. The cylinder liner 1 has ports 4. The elevation shown is sectioned on X - X and the plan on Y - Y. The piston in turning 900 of rotation moves axially between the cylinder heads 2., the piston always rotates in the same direction of rotation. The exact path of any point on the piston 5, for a full combustion cycle, would move and be constrained to an approximate double helix. The path will hereinafter be described as helical.
There are many devices in use to convert this described motion to single plane rotation. The mechanical advantage of converting helical motion to rotary are obvious.
It should be noted that ports 4 are closed by the action of the piston in motion.
Figure 2, this is a schematic line drawing to support the explanation of the engine combustion cycle. The piston 5, is shown at rest. The piston is turned 90 and moved axially a distance between the heads 2 ( the stroke ) by an external force.
The piston closes ports 4 and compression begins, at a desired point after port closure, fuel is injected into the chamber A. The fuel/air ratio is further compressed and twin ignited between before or after top dead centre. Depending upon fuel used spark ignition may be substituted by compression ignition.
Upon ignition the expansion of the gas will tend to move the piston helically towards the opposite cylinder head.
As the piston moves under expansion of the burning gas, compression begins in opposing chamber.
0 Figure 3, shows the position of the piston after 90 of shaft rotation and axial movement from that shown in Figure 2a. As the piston moves helically as described above the ports in chamber B close and compression begins, fuel is injected and ignited, the piston now returns the the position shown in Figure 2a after a further 900 of piston rotation. The ports in chamber A are now open and air or a gas is blown in through one open port 4 and exhausted out the other, the chamber is therefore purged. This engine cycle like current two stroke diesels relies on an device separate to., but related to the engine for purging exhaust gases. The piston now moves helically from the position shown in Figures 2 to 3, the cycle is now self sustaining.
In summary: Figure 2 engine at rest Figure 3 piston after 90 of shaft rotation Figure 2 piston after 1800 of shaft rotation Figure 3 piston after 2700 of shaft rotation Figure 2 piston after 360 of shaft rotation The above summary demonstrates the four power "strokes" ( two on each end of the piston ), in one revolution of the main shaft/piston.
Figure 4, represents the cylinder head and piston crown profiles.
If a point on the circumference of a cylinder is rotated 900 and at the same time moved axially, the desired stroke. The line X is defined. Line Y is an appropriate radius scribed from the axis of the main shaft 3. The actual shapes and cylinder head/piston crown relationship can only be determined by experiment., but will approximate as drawn. Were upon the burning of the gases the piston tends to move along the "helical path" without reliance and losses on "path" constraints.
Figure 5, is a sketch showing the surfaces bounded by the lines X and Y. The construction of the engine would be such that the surfaces R are closer together than surfaces F. This would maximise the compressed gas volumes over F. Twin ignition over surfaces F will tend to move the piston helically with little or no negative expansion over the R surfaces. The ignited gases will expand and swirl around the main shaft 3.
0 Figure 6, shows the piston in four positions during 90 of shaft rotation. Twin ignition over the surface F will tend to move the piston along the desired path with minimal negative effect of gas burning over surfaces R. As can be seen from the four piston positions. The piston/cylinder heads volumes over F are expanding at a greater rate than the volumes over R. Over R the piston crown and head stay in close proximity.

Claims (6)

1. an internal combustion engine were the gas, fuel/air, is compressed by a piston that rotates at the same time moving axially between cylinder heads.
2. an internal combustion engine whereby the cylinder head profiles and piston crowns are shaped such that upon ignition the expansion of the burning gases acts and tends to move the piston ( output shaft ) in a given rotation/axial movement away from one cylinder head towards the other.
3. an internal combustion engine that embodies all the claims above, but is double acting. The piston moves axially and rotates for each 900 of shaft rotation.
4. an internal combustion engine where to achieve useful rotation will require a flexible coupling.
5. an internal combustion engine that either relies on an external device to purge spent gases or the cycle is modified were the functions of induction, compression, ignition/expansion and exhaust are divided between each chamber.
6. an internal combustion engine that embodies all of the claims above, but can be designed to be either spark or compression ignition.
GB9316191A 1993-08-04 1993-08-04 Rotating and reciprocating piston i.c. engine. Withdrawn GB2280710A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9316191A GB2280710A (en) 1993-08-04 1993-08-04 Rotating and reciprocating piston i.c. engine.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9316191A GB2280710A (en) 1993-08-04 1993-08-04 Rotating and reciprocating piston i.c. engine.

Publications (1)

Publication Number Publication Date
GB2280710A true GB2280710A (en) 1995-02-08

Family

ID=10739978

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9316191A Withdrawn GB2280710A (en) 1993-08-04 1993-08-04 Rotating and reciprocating piston i.c. engine.

Country Status (1)

Country Link
GB (1) GB2280710A (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB294510A (en) * 1927-04-21 1928-07-23 Nicolai Von Gribojedoff Internal combustion engine
GB606981A (en) * 1945-12-27 1948-08-24 John Neville Morris Improvements relating to reciprocatory pump and/or fluid operated motor mechanisms
GB710104A (en) * 1951-05-29 1954-06-09 Francis Emile Myard Improvements in or relating to rotatable-piston machines
GB2030220A (en) * 1978-04-27 1980-04-02 Deacon B I.c. engine with reciprocating and rotating piston
GB2198788A (en) * 1986-04-04 1988-06-22 Iso Wrysch Rotating and alternating piston machine
GB2233386A (en) * 1989-04-10 1991-01-09 Jan Szuler Rotating end reciprocating piston i.c. engine

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB294510A (en) * 1927-04-21 1928-07-23 Nicolai Von Gribojedoff Internal combustion engine
GB606981A (en) * 1945-12-27 1948-08-24 John Neville Morris Improvements relating to reciprocatory pump and/or fluid operated motor mechanisms
GB710104A (en) * 1951-05-29 1954-06-09 Francis Emile Myard Improvements in or relating to rotatable-piston machines
GB2030220A (en) * 1978-04-27 1980-04-02 Deacon B I.c. engine with reciprocating and rotating piston
GB2198788A (en) * 1986-04-04 1988-06-22 Iso Wrysch Rotating and alternating piston machine
GB2233386A (en) * 1989-04-10 1991-01-09 Jan Szuler Rotating end reciprocating piston i.c. engine

Similar Documents

Publication Publication Date Title
US5927236A (en) Variable stroke mechanism for internal combustion engine
US6546908B1 (en) Variable geometry toroidal engine
US4022167A (en) Internal combustion engine and operating cycle
US5676037A (en) Apparatus for mutual conversion between circular motion and reciprocalmotion
USRE30565E (en) Internal combustion engine and operating cycle
EP1819912B1 (en) Reciprocating machine
US4010611A (en) Compression-expansion power device
HU222393B1 (en) Mechanism for transforming rectilinear motion to rotating motion mainly for reciprocating piston internal combustion engines
WO2018171452A1 (en) Power system of cam rotary internal combustion engine
JP3143564B2 (en) Cam type engine
JP5904686B2 (en) Variable stroke mechanism for internal combustion engines
EP0153325A1 (en) Internal combustion engine.
US20020007815A1 (en) O-ring type rotary engine
GB2050509A (en) Internal combustion engine and operating cycle therefor
US20030131807A1 (en) Rotating positive displacement engine
EP0103985A2 (en) Rotary engine or compressor
GB2280710A (en) Rotating and reciprocating piston i.c. engine.
JPH06280603A (en) Fuel injection internal combustion engine whose engine body rotates
US3874346A (en) Internal combustion engine
KR20040074573A (en) Rotary engine
GB2261025A (en) Four-stroke engine inlet and exhaust valving
JPS6282236A (en) Opposed-piston type coaxial engine
KR200206389Y1 (en) O-ring type rotary engine
JPS5996436A (en) Four-stroke-cycle engine to reciprocate piston by rolling ball and guide groove
JPH0626359A (en) Internal combustion engine

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)