Mechanical fuel pump deactivation
10273945 ยท 2019-04-30
Assignee
Inventors
Cpc classification
F02D19/0649
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M59/102
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01B31/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L1/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M43/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B9/042
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L2820/041
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L13/0005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L13/0036
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T10/30
GENERAL 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
F04B27/0437
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D19/0684
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L1/146
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M43/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B27/0428
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B1/0435
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L2305/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M59/38
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M59/027
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F04B1/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B9/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B27/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L13/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01B31/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M59/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M59/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M39/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A mechanical fuel pump is disclosed for delivering fuel to an engine of a vehicle, the mechanical fuel pump having an activated configuration and a deactivated configuration. A dual fuel system and method are also disclosed for use with the mechanical fuel pump.
Claims
1. A fuel pump comprising: a rotatable camshaft including a lobe which protrudes from the camshaft and is immovable relative to the camshaft as the camshaft rotates through a plurality of revolutions; a pump housing defining a pump chamber; a pump piston mounted in the pump chamber for reciprocal movement; and a deactivating element operatively positioned between the lobe and the pump piston, the deactivating element having: a first configuration wherein the deactivating element transfers movement of the lobe to the pump piston to deliver fuel to an engine; and a second configuration wherein the deactivating element absorbs movement of the lobe, thereby causing the pump piston to remain substantially stationary and avoid operating the fuel pump during rotation of the camshaft through the plurality of revolutions.
2. The fuel pump of claim 1, wherein the deactivating element is rigid in the first configuration and collapsible in the second configuration.
3. The fuel pump of claim 1, wherein the deactivating element comprises: an outer body; an inner body; and at least one locking pin being movable between: a locked position corresponding to the first configuration, wherein the inner body moves with the outer body in the locked position; and an unlocked position corresponding to the second configuration, wherein the inner body moves relative to the outer body in the unlocked position.
4. The fuel pump of claim 3, wherein, in the unlocked position of the at least one locking pin, at least one spring forces the at least one locking pin radially inward and away from the outer body.
5. The fuel pump of claim 3, wherein the at least one locking pin is biased in the unlocked position.
6. The fuel pump of claim 3, wherein, in the locked position of the at least one locking pin, a pressurized fluid in the inner body forces the at least one locking pin radially outward and toward the outer body.
7. The fuel pump of claim 3, wherein the pump piston moves along a first axis and the at least one locking pin moves along a second axis transverse to the first axis.
8. The fuel pump of claim 1, further comprising a lobe follower coupled to the deactivating element to interact with the lobe of the rotatable camshaft.
9. A fuel pump comprising: a rotatable camshaft including a lobe which protrudes from the camshaft and is immovable relative to the camshaft as the camshaft rotates through a plurality of revolutions; a pump housing defining a pump chamber; a pump piston reciprocally mounted in the pump chamber; and a deactivating element that uncouples the lobe from the pump piston to cause the pump piston to remain substantially stationary and avoid operating the fuel pump during rotation of the camshaft through the plurality of revolutions.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The above-mentioned and other features and advantages of this disclosure, and the manner of attaining them, will become more apparent and the invention itself will be better understood by reference to the following description of embodiments of the invention taken in conjunction with the accompanying drawings, wherein:
(2)
(3)
(4)
(5)
(6)
(7) Corresponding reference characters indicate corresponding parts throughout the several views. The exemplifications set out herein illustrate exemplary embodiments of the invention and such exemplifications are not to be construed as limiting the scope of the invention in any manner.
DETAILED DESCRIPTION
(8) Referring initially to
(9) The illustrative fuel system 10 of
(10) The first fuel system 30 may differ from the second fuel system 40. For example, the first fuel system 30 may be a low pressure system, whereas the second fuel system 40 may be a high pressure system. As another example, the first fuel source 32 of the first fuel system 30 may supply a low octane fuel to engine 12, whereas the second fuel source 42 of the second fuel system 40 may supply a high octane fuel to engine 12. However, it is also within the scope of the present disclosure that the first fuel source 32 and the second fuel source 42 may be a common fuel source to supply a single fuel type to engine 12. As yet another example, the first fuel pump 34 of the first fuel system 30 may be an electric pump, whereas the second fuel pump 44 of the second fuel system 40 may be a mechanical pump that is driven by camshaft 14 of engine 12. As still yet another example, the first fuel injector 36 of the first fuel system 30 may be a port injection device that injects low pressure fuel into an air intake manifold (not shown) of engine 12, whereas the second fuel injector 46 of the second fuel system 40 may be a direct injection device that injects high pressure fuel directly into a cylinder (not shown) of engine 12.
(11) As discussed further below, a mechanical coupling 18 between the camshaft 14 of engine 12 and the second fuel pump 44 may be controlled using a suitable pressure source. In the illustrated embodiment of
(12) Referring still to
(13) An exemplary embodiment of the second fuel pump 44 is shown in
(14) Between the pump piston 54 and the lobe follower 58, the fuel pump 44 further includes a deactivating element 70 to selectively deactivate the fuel pump 44. The illustrative deactivating element 70 includes an outer body 72 and an inner body 74, which may be arranged in the pump chamber 52 along the same longitudinal axis 56 as the pump piston 54. The outer body 72 may be keyed to the inner body 74 to prevent relative rotation therebetween. In
(15) The illustrative deactivating element 70 further includes one or more internal locking pins 80 contained in a throughbore 82 of the inner body 74. The locking pins 80 may be configured for movement in the throughbore 82 along an axis 84 that is transverse or perpendicular to the longitudinal axis 56.
(16) As shown in
(17) As shown in
(18) In
(19) Returning to
(20) The fuel pump 44 may be mechanically activated by placing the deactivating element 70 in the locked or rigid configuration (
(21) In use, controller 20 may control operation of the second fuel system 40 of
(22) While this invention has been described as having exemplary designs, the present invention can be further modified within the spirit and scope of this disclosure. This application is therefore intended to cover any variations, uses, or adaptations of the invention using its general principles. Further, this application is intended to cover such departures from the present disclosure as come within known or customary practice in the art to which this invention pertains and which fall within the limits of the appended claims.