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US4848280A Expired / Lapsed US ⏱️ 0.0 years remaining

Intake apparatus for internal combustion engine

Assignee: Mazda Motor Corp
•
Filing: 1988-01-11
•
Granted: 1989-07-18
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Expires: 2008-01-11
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Abstract

Abstract An internal combustion engine of the in-line type having a surge tank located above the engine. Intake tubes connect the surge tank with the in-line engine cylinders. The tubes extend from one side of the engine body in a direction away from the engine body and are then curved upwardly in a U-shaped manner toward the surge tank. Surge tank openings and the ends of the intake tubes connected together are both formed as ellipses having a major axis lying in a direction parallel to the cylinder axes. The cross-sectional shape of the intake tubes gradually changes from an ellipse into a circle at approximately the middle or bend of the intake tube.

Inventors

  • 👤 Takenori Ohtsuka
  • 👤 Yasuo Honda
  • 👤 Tomohiro Sunada
  • 👤 Yasuhiro Kawasako
  • 👤 Tomoyuki Yamamoto

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-27 08:11
CPC Classifications
F; F02; F02B; F02B75/00; F02B75/16; F02B75/18; F02B75/20; F02B27/00; F02B27/005; F02B27/006; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12

Claims Analysis

Total Claims: 14
Claim 1
Independent Claim 282 words
An internal combustion engine for a vehicle comprising: an engine body having a plurality of cylinders arranged in series with their cylinders in a line with the axes of the cylinders lying in a common plane and having on one side thereof an intake port for each of the cylinders; a surge tank located above said engine body and having a pair of opposed sidewalls, one sidewall near the plurality of cylinders and the other sidewall remote from the plurality of cylinders, said other sidewall lying in a plane parallel to the common plane in which the axes of the cylinders lie and defining a plurality of in-line elliptical openings; and a plurality of discrete intake tubes connecting, for independent air flow, the elliptical openings of said surge tank to the intake ports for said cylinders; each of said discrete intake tubes shaped to extend from said one side of said engine body in a direction substantially normal to the common plane in which the axes of the cylinders lie outwardly away from said engine body to beyond the surge tank and then being curved upwardly in a U-shaped manner to substantially the level of the other sidewall of the surge tank and then extending back toward said other sidewall of said surge tank; and each of said discrete intake tubes formed with its end connected to said surge tank defining a matching elliptical opening having a major axis lying substantially in the plane of the sidewall and parallel to the common plane in which the axes of the cylinders lie and defining a transition region extending from said end with its cross-sectional shape gradually changing from an ellipse into a circle.
Claim 2
Dependent Claim 282 words
An internal combustion engine for a vehicle comprising: an engine body having a plurality of cylinders arranged in series with their cylinders in a line with the axes of the cylinders lying in a common plane and having on one side thereof an intake port for each of the cylinders; a surge tank located above said engine body and having a pair of opposed sidewalls, one sidewall near the plurality of cylinders and the other sidewall remote from the plurality of cylinders, said other sidewall lying in a plane parallel to the common plane in which the axes of the cylinders lie and defining a plurality of in-line elliptical openings; and a plurality of discrete intake tubes connecting, for independent air flow, the elliptical openings of said surge tank to the intake ports for said cylinders; each of said discrete intake tubes shaped to extend from said one side of said engine body in a direction substantially normal to the common plane in which the axes of the cylinders lie outwardly away from said engine body to beyond the surge tank and then being curved upwardly in a U-shaped manner to substantially the level of the other sidewall of the surge tank and then extending back toward said other sidewall of said surge tank; and each of said discrete intake tubes formed with its end connected to said surge tank defining a matching elliptical opening having a major axis lying substantially in the plane of the sidewall and parallel to the common plane in which the axes of the cylinders lie and defining a transition region extending from said end with its cross-sectional shape gradually changing from an ellipse into a circle.
Claim 3
Dependent Claim 29 words
An internal combustion engine as defined in claim 1 further comprising throttle body means having a throttle valve within connected to the one sidewall side of the surge tank.
Claim 4
Dependent Claim 29 words
An internal combustion engine as defined in claim 1 wherein the transition region of each of the discrete intake tubes terminates in the curved portion of said each tube.
Claim 5
Dependent Claim 84 words
An internal combustion engine as defined in claim 1, wherein a boss, to install a delivery pipe supplying fuel to a fuel injection valve, is formed on an inner side portion of at least one of the discrete intake tubes; and a rib is formed on the inner side portion of said at least one discrete intake tubes that extends from the surge tank to the boss, said rib lying in a plane normal to the common plane of the axes of the cylinders.
Claim 6
Dependent Claim 38 words
An internal combustion engine as defined in claim 1, wherein the minor axis of the elliptical opening of each discrete intake tube is substantially equal to the diameter of the circular cross-sectional portion of the discrete intake tube.
Claim 7
Dependent Claim 67 words
An internal combustion engine as defined in claim 1, in which each of the discrete intake tubes is divided into two parts, an upstream tube part and a downstream tube part; and at least two bolts connect the upstream tube part with the downstream tube part so that a virtual line connecting the at least two bolts passes through the center of the connected discrete intake tube.
Claim 8
Dependent Claim 47 words
An internal combustion engine as defined in claim 4, wherein said engine body has four cylinders, and two bosses are provided, one between the fuel injection valves for the first and second cylinders and the other between the fuel injection valves for the third and fourth cylinders.
Claim 9
Dependent Claim 63 words
An internal combustion engine as defined in claim 1, wherein each of the discrete intake tubes is divided into two parts at the middle position of the curved portion, an upstream tube part and a downstream tube part, said upstream tube part and said downstream tube part being connected together in a plane substantially perpendicular to the common plane of the cylinder axes.
Claim 10
Dependent Claim 57 words
An internal combustion engine as defined in claim 8, further comprising a flange formed integrally with each said upstream tube part at the downstream end thereof and a flange formed integrally with each said downstream tube part at the upstream end thereof, and said upstream and downstream tube parts are connected by said flanges being connected together.
Claim 11
Dependent Claim 38 words
An internal combustion engine as defined in claim 9, wherein at least two bolts connect said flanges so that a virtual line connecting said at least two bolts passes through the center of the connected discrete intake tube.
Claim 12
Dependent Claim 27 words
An internal combustion engine as defined in claim 8, wherein all of said upstream tube parts are formed integrally with said other sidewall of said surge tank.
Claim 13
Dependent Claim 47 words
An internal combustion engine as defined in claim 4, further comprising a second rib formed on the outer side portion of said at least one discrete intake tube, said second rib lying in a plane substantially normal to the common plane in which the cylinder axes lie.
Claim 14
Dependent Claim 40 words
An internal combustion engine as defined in claim 4, further comprising reinforcement means integrally formed with the discrete intake tubes and extending parallel to the common plane in which the cylinder axes lie for reinforcing the plurality of intake tubes.

References Cited (Backward Citations)

FR1136080A Cited
US4228769A Cited
US4409934A Cited
JPS56105626A Cited
US4497287A Cited
JPS59165562A Cited
US4669428A Cited
US4702203A Cited
JPS6136126A Cited
US4719879A Cited
US4708097A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1992-07-17 1993-01-16 1993-07-18 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1996-07-17 1997-01-16 1997-07-18 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2000-07-17 2001-01-16 2001-07-18 $7700.00 Window Closed / Lapsed

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