U.S. patent number 3,667,703 [Application Number 05/005,520] was granted by the patent office on 1972-06-06 for auxiliary air intake for air and spacecraft engines.
This patent grant is currently assigned to Messerschmitt-Bolkow-Blohm GmbH. Invention is credited to Helmut Boek.
United States Patent |
3,667,703 |
Boek |
June 6, 1972 |
AUXILIARY AIR INTAKE FOR AIR AND SPACECRAFT ENGINES
Abstract
Auxiliary air intake construction for jet engines having a main
air intake enclosed in an engine cowling and leading to the engine
air inlet. The auxiliary air intake consists of a slot extending
through a portion of such cowling and defined by walls which form
an acute angle with the axis of the main air intake. A recess is
formed in one of said walls and a door structure for at least one
sliding door is arranged within said recess. Said door structure
includes operating means for retracting same within said recess to
open said auxiliary air intake and for extending same across said
slot to close same. Said door structure is so positioned and
arranged that when in extended position its outer surface is
substantially flush with the surface of the engine cowling and its
inner surface is substantially flush with the wall defining the
main air intake.
Inventors: |
Boek; Helmut (Munich,
DT) |
Assignee: |
Messerschmitt-Bolkow-Blohm GmbH
(Munchen, DT)
|
Family
ID: |
5724624 |
Appl.
No.: |
05/005,520 |
Filed: |
January 26, 1970 |
Foreign Application Priority Data
|
|
|
|
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Feb 7, 1969 [DT] |
|
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P 19 06 157.5 |
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Current U.S.
Class: |
244/53B |
Current CPC
Class: |
B64D
33/02 (20130101); F02C 7/042 (20130101); B64D
2033/0286 (20130101) |
Current International
Class: |
B64D
33/02 (20060101); B64D 33/00 (20060101); F02C
7/04 (20060101); F02C 7/042 (20060101); B64d
027/00 (); B64d 029/00 () |
Field of
Search: |
;244/53B,121,129D
;137/15.1,15.2 ;60/36LL ;239/265.29,265.17 |
References Cited
[Referenced By]
U.S. Patent Documents
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|
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2960281 |
November 1960 |
Jumelle et al. |
3503211 |
March 1970 |
Medawar et al. |
|
Primary Examiner: Blix; Trygve M.
Claims
The embodiments of the invention in which an exclusive property or
privilege is claimed are defined as follows:
1. An auxiliary air intake duct arrangement for air and spacecraft
jet engines which have an elongated air intake fairing, a main air
intake opening at one end of said fairing communicating with a main
air intake duct to said engine, comprising:
means defining an auxiliary air intake duct having a slot in said
air intake fairing aft of said main air intake opening but forward
of said engine and communicating with said main air intake
duct;
means defining a sliding door mounted for movement between open and
closed positions relative to said slot, said sliding door means
being substantially flush, both with the outer surface of said
fairing and with the internal wall of said main air intake duct
when in the closed position to thereby close said slot;
means defining a recess adapted to receive said sliding door means;
and
support means adapted to support said sliding door means for
movement into and out of said recess between said open and closed
positions and for maintaining said sliding door means equally
spaced from the axis of said aft portion of said main air intake
duct, said sliding door means, when in said recess, effecting an
opening in said slot to provide an auxiliary flow of air to said
engine.
2. An auxiliary air intake according to claim 1, wherein one edge
of said slot is formed by an abutting lip portion of said sliding
door means and that the opposite edge of said air intake fairing
has a form complementary to that of said lip.
3. An auxiliary air intake according to claim 2, wherein said
sliding door means is of a box type design and its path of movement
is parallel to the axis of said main air intake duct.
4. An auxiliary air intake according to claim 3, wherein the parts
of said box type sliding door are connected by means of hinged
joints.
5. An auxiliary air intake according to claim 1, wherein said
sliding door means has rollers mounted thereon and including roller
guide means in one of said engine cowling and air intake fairing
for receiving said rollers to support said sliding door for said
movement between said opened and closed positions.
6. An auxiliary air intake according to claim 1, wherein said
sliding door means includes means adapted to lock said door in any
position of its path of movement between said opened and closed
positions for controlling the flow rate of said auxiliary air.
7. An auxiliary air intake according to claim 1, wherein said
sliding door means includes means defining a formed part on the air
intake side and means defining a slide element on the engine side;
and
wherein said closing movement of said sliding door means is
effected simultaneously by said formed part and said slide
element.
8. An auxiliary air intake according to claim 7, wherein said
formed part and said slide element are commonly actuated by one
single actuator.
9. An auxiliary air intake according to claim 8, wherein said
actuator for effecting the movement of said sliding door means is
connected with the lateral edges of said door means by means of a
toggle mechanism that controls their operation.
10. An auxiliary air intake according to claim 1, wherein the edges
of the slot and the slide engage each other in said closed position
to thereby define a seal with respect to the surrounding
environment.
11. An auxiliary air intake according to claim 1, wherein the axis
of said auxiliary air intake duct is at an acute angle relative to
the axis of said main air intake duct.
12. An auxiliary air intake according to claim 1, wherein the path
of movement of said sliding door is substantially parallel to the
axis of the main intake duct.
13. An auxiliary air intake construction according to claim 1,
wherein the path of movement of said sliding door is substantially
circumferentially around the axis of said main intake duct.
14. An auxiliary air intake according to claim 1, wherein said
sliding door means comprises spaced inner and outer wall elements,
said elements being articulated for assuming one contour when said
door is in retracted position and for assuming a contour when said
door is in extended position substantially constituting a
continuation of the adjacent outer surface of said wall and inner
surface defining said air duct.
15. An auxiliary air intake according to claim 14 including
operating means having mechanical interconnection to said
articulated walls adapted for urging them into said last named
position as a direct consequence of urging same into extended
position.
16. An auxiliary air intake according to claim 1, wherein said
sliding door means comprises separate inner and outer elements,
guide means receiving each thereof for independently guiding each
thereof between retracted and extended positions and power operated
means for simultaneously moving each of said elements
simultaneously between retracted and extended positions.
Description
This invention relates to an auxiliary air intake for air and
spacecraft jet engines, preferably for VTOL/STOL aircraft, whose
air intake duct is at an acute angle with respect to the main duct
of the engine intake, for example, a Pitot-type air intake.
Auxiliary air intakes have already been disclosed, such as an air
intake for swivelling engines on jet aircraft, in which a movable
tube section located forward of the engine is hinged to a second,
fixed, tube section so that when the movable section is tilted
forward, a gap is created between the two sections, thus forming an
auxiliary air intake. However, devices of this kind are not
compatible with engines which are wholly contained within the
fuselage of an aircraft. Moreover, the components required to
construct such a device and the power needed to actuate the device
are too great.
It is also presently known, for engines required to operate only
occasionally, to have engine air intake doors which extend from
spaces located in the skin and cover the main air intake. This
device, however, would not solve the problem of providing auxiliary
air intakes.
It is the object of the present invention to provide an auxiliary
air intake for jet engines without affecting the aerodynamic
characteristics of the aircraft, thus eliminating the drawbacks of
conventional auxiliary air intakes.
The invention achieves this objective by having one or more slots
in the duct wall, aft of the main air intake opening, which can be
closed by means of sliding doors. In the closed position, the
sliding doors are flush with the skin and with the duct wall, or
nearly so. The sliding doors extend from recesses in the engine
cowling. The direction of motion of the sliding doors is either
radial with respect to the axis of the intake duct or is parallel
to said axis. These features of the invention thus ensure an
improvement of the aerodynamic characteristics of air and
spacecraft so as to achieve optimum results when the auxiliary air
intake is open.
Another feature of the present invention provides that one duct
wall be formed by the appropriately shaped forward lip of the
sliding door, that the latter be of box type design and that it be
extendable in a direction nearly parallel with respect to the main
duct axis.
In addition, the invention provides that the individual surfaces of
the box type sliding door be connected to each other at a hinged
joint and that the parts of the door be supported in roller guides.
This permits design simplicity, assuring, above all, that the
sliding doors will be flush, both with the skin and with the main
air intake ducts.
It is also suggested that the sliding doors be capable of being
locked at any position in their path of travel, so as to permit
control of air flow. These features provide an additional means of
controlling the air or spacecraft without the necessity for special
devices.
According to a special embodiment of the invention, closing of the
slot is effected by means of a formed part on the air intake side
and by means of a horizontally movable sliding element on the
engine side, both parts being actuated simultaneously by one
actuator.
These embodiments also assure rational construction and reduced
weight.
Other additional features and advantages of the invention will
become apparent through reference to the following description and
accompanying drawings which show illustrative embodiments of the
invention. The figures show:
FIG. 1 is a partial cross-section of an air intake duct with an
embodiment of this invention;
FIG. 2 is a plan view according to FIG. 1;
FIG. 3 is a cross-section along the line I--I in FIG. 1;
FIG. 4 is a cross-section along the line II--II in FIG. 1;
FIG. 5 is a cross-section along the line III--III in FIG. 1;
FIG. 6 is a partial cross-section of an embodiment with radial,
sliding control;
FIG. 7 is a partial cross-section of a second embodiment with
axial, sliding control;
FIG. 8 is a partial cross-section of another embodiment with axial,
sliding control;
FIG. 9 is a partial cross-section of still another embodiment with
axial, sliding control;
FIG. 10 is a cross-section along the line C--C in FIG. 9, closed
position;
FIG. 11 is a cross-section along the line C--C in FIG. 9, open
position.
FIGS. 1 through 5 show an illustrative embodiment of this
invention. An aircraft 10, preferably a STOL/VTOL aircraft, has its
engines 11 mounted in such a way that the air intake fairing 12 is
faired into the engine cowling 13 and into the skin of the fuselage
14. One or more slots 16, arranged aft of the inlet opening 15 but
a short distance forward of the engines, is/are oriented at an
acute angle with respect to the main air intake duct 17. These
slots 16 are closed by means of sliding doors 18 which can be
retracted into recesses 19 located in the engine cowling 13. The
embodiment described provides that the sliding doors 18 be movable
in a direction parallel with respect to the axis 20 of the main air
intake duct 17 by means of actuating devices 23 of any known kind,
such as hydraulic, which furnish the needed controllable
longitudinal motion and for locking same in a desired position. In
this case, the abutting lip 21 of sliding door 18 forms one duct
wall of air intake slot 16, the duct wall 22 of air intake fairing
12 having a form which will snugly conform to the abutting lip 21.
The box type sliding door 18 is designed in such a way that it is
flush with the air intake fairing and the engine cowling 12, 13 on
the one hand and with the main air intake duct 17 on the other
hand. The sliding doors 18 are supported and guided in any
conventional manner, which will preferably include roller guides
24.
Another embodiment of the invention, disclosed in FIG. 6, provides
that the auxiliary air duct or slot 16a, arranged in engine cowling
13, be opened and closed by means of a sliding door 18a moving in a
circumferential direction with respect to the axis of the main air
intake duct 17a. This sliding door 18a has four parts 25, 26, 27,
28 connected by means of hinged joints 29. The lateral edges of
parts 25, 26 are connected to a toggle mechanism 30 which in turn
is attached to rod 31 which moves in and out of actuator 23. Parts
25, 26 of sliding door 18a are appropriately shaped so as to match
the radius of engine cowling 13 as well as that of the main air
intake duct 17a, when the auxiliary air intake is opened, parts 25,
26 retract into a recess 19a located in engine cowling 13. Again
the precise manner of supporting and guiding the sliding door forms
no part of the invention and any presently known manner thereof may
be used.
FIGS. 7 and 8 show further embodiments of sliding door and its
associated actuator. In both cases, the sliding doors 18b each
consist of two individual sliding elements 32, 33 which, by means
of articulated links 34, or similar elements, are attached to rod
31 which moves in and out of actuator 23b. In both cases, one
single actuator 23b moves both sliding elements 32, 33, their
movement being simultaneous and uniform, with said doors being
supported and guided in any known manner.
A still further embodiment of the air intake according to the
invention is disclosed in FIGS. 9 through 11. Opening and closing
of slot 16c is effected by means of a single actuator 23c. Rod 31c,
which moves in and out of the actuator is attached, by means of
articulated links 34, to a formed part 35 for closure of the slot
on the side of the engine cowling 13, and to a sliding element 33
for closure of the slot 16c on the side of main engine duct 17c.
This formed part 35 consists of an angle 36, one side 37 of which
forms the abutting lip of the sliding door. When the sliding door
is open, lip 37 partially or completely forms one wall of slot 16c.
The lip surface is therefore formed appropriately. Formed parts 35
and sliding element 33 are both supported and guided in any known
manner, preferably one utilizing roller guides.
* * * * *