U.S. patent number 3,845,921 [Application Number 05/405,228] was granted by the patent office on 1974-11-05 for telescoping boom.
This patent grant is currently assigned to The United States of America as represented by the Secretary of the Army. Invention is credited to Leslie A. Hromas, Thomas R. Thompson.
United States Patent |
3,845,921 |
Thompson , et al. |
November 5, 1974 |
TELESCOPING BOOM
Abstract
A boom which is carried inside a reentry vehicle during launch
and flight ereof and extended from the aft of the reentry vehicle
during reentry of the vehicle into the atmosphere. Instrumentation
is carried by the boom for making certain experiments and for
making direct measurements of flow properties in the recirculation
region and hypersonic wake behind the reentry vehicle.
Inventors: |
Thompson; Thomas R. (Palos
Verdes Peninsula, CA), Hromas; Leslie A. (Rolling Hills,
CA) |
Assignee: |
The United States of America as
represented by the Secretary of the Army (Washington,
DC)
|
Family
ID: |
23602824 |
Appl.
No.: |
05/405,228 |
Filed: |
October 10, 1973 |
Current U.S.
Class: |
244/172.6;
248/333 |
Current CPC
Class: |
B64G
9/00 (20130101) |
Current International
Class: |
B64G
9/00 (20060101); B64g 001/10 () |
Field of
Search: |
;244/155,15A,15D,1N,1A,135A,158,161,167,173 ;212/55,144
;85/1R,DIG.1 ;248/333 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Blix; Trygve M.
Assistant Examiner: Kelmachter; Barry L.
Attorney, Agent or Firm: Neureither; Lawrence A. Beumer;
Joseph H. Hilton; Harold W.
Claims
We claim:
1. A telescoping boom comprising:
a. boom support means;
b. a guide member secured to said boom support means;
c. a boom carried in said guide member in telescoping relation
therewith;
d. releasable locking means for securing said boom in a nonextended
position and for release thereof for movement to an extended
position;
e. means for extending said boom out of said guide member and said
support means;
f. locking means for securing said boom in the extended position;
and;
g. an instrument package carried in said boom support means having
electric cables connected thereto and to said instruments, cable
tension mechanism carried in said boom guide to prevent
entanglement of said cables responsive to boom deployment, and,
means for guiding said electric cable from said instrument package
to said cable tension mechanism including adjacent longitudinally
extending lands provided in said boom and said guide member.
2. A telescoping boom as in claim 1 wherein said guide member is a
tubular member having said boom slidably mounted therein.
3. A telescoping boom as in claim 1 wherein said means for
extending said boom includes an electric motor driven boom actuator
drum and a wire connected to the forward end of said boom and said
drum whereby responsive to rotation of said drum said wire extends
said boom out of said guide member.
4. A telescoping boom as set forth in claim 3 wherein said means
for retention of said boom in the extended position includes an
annular groove disposed in said support member and ball lock means
carried on said boom at the forward end thereof, said ball lock
means including a plurality of balls carried in biased relation in
said boom for locked engagement in said annular groove responsive
to said boom reaching the extended position.
5. A telescoping boom as set forth in claim 4 wherein said support
means is a reentry vehicle and said boom is provided with
instrument support means for support of instruments thereon for
measurements of conditions in the wake of said reentry vehicle.
6. A telescoping boom as in claim 5 wherein said means for securing
said boom in the non-extended position and for release thereof for
movement to an extended position includes an explosive retaining
means extending through said boom guide in engagement with said
boom.
Description
BACKGROUND OF THE INVENTION
The boom is basically an instrument carrier which is stored inside
the reentry vehicle during the launch and is extended therefrom
after the reentry vehicle is separated from the launch vehicle, but
before it is spun up. The boom contains such instruments as
pressure gages, electrostatic probes, acoustic sensors,
radiometers, a wake seeding device, a spectrometer, a base
diffusion experiment, etc. The apparatus permits localized (point)
measurements over portions of near wake, recirculation region, and
expansion region for relatively long periods of time during
reentry, and at well fixed geometric points. It also permits direct
wake seeding experiments to be performed without involving the
recirculation region.
SUMMARY OF THE INVENTION
The boom structure includes a boom guide tube having the boom, with
its instrumentation carried thereon, carried in the guide tube. An
explosive "pin puller" retains the boom in the stowed position. At
the desired time a small electric motor extends the boom out of the
boom guide and the reentry vehicle. Electric cable secured to an
instrument package in the vehicle and the instruments on the boom
is extended with the boom and a cable drum and negator spring is
provided to insure that the electric cable does not become
entangled during deployment of the boom. The instrument package
receives signals, through the cables, from the instruments. The
signals are recorded or transmitted, as desired.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is an elevational view of the boom assembly in stowed
position in a reentry vehicle.
FIG. 2 is a sectional view along line 2--2 of FIG. 1.
FIG. 3 is a sectional view along line 3--3 of FIG. 1.
DESCRIPTION OF THE PREFERRED EMBODIMENT
As shown in FIG. 1, a boom 10 is carried in a cylindrical boom
guide 12 in stowed position in a reentry vehicle 14. The aft end 16
of the boom rests in a cylindrical bearing 18 in a support sleeve
20 which in turn is threaded into a structural member 21 of the
vehicle. A flange 22 of a structural support tube 24 of the
instrument package 26, for the experiments is secured to structural
member 21. The forward end 27 of the boom rests similarly in a
support tube 28. At the aft end 16, an explosive "pin puller" 30
extends through the boom guide 12 for engagement with the boom to
provide a stowed position lock.
Electrical wiring 34 extending from the instrument carried by the
boom 10 is molded together in a flat cable and is carried over a
rotating drum 36 and extends back to the instrument package 26,
running in an annular space 38 between boom 10 and support tube 12.
The cable 34 is guided by an arrangement of longitudinal lands 40
(FIGS. 2 and 3) in the supporting tube wall. Lands 40, together
with matching cut-outs 42 in the boom sliding surfaces, provide an
indexing feature which prevents the boom from rotating in the
support tube and thus makes the boom position in relation to the
reentry vehicle known even in the extended position.
The cable drum 36 is attached to a negator spring (not shown)
located in the forward end 27 of the support tube. The spring
provides a constant stretch load through the drum 36 onto the wire
cable 34 reglardless of the longitudinal position of the boom
during its deployment thus preventing tangling of the electrical
cable and slack in the actuating cable.
The instruments mounted inside the boom are supported on a central
fiber glass-epoxy one-piece shelf 44 (FIGS. 3 and 4) which runs
from end to end of the boom. The shelf slides on two parallel lands
46 and 48 brazed into the boom. Surface contact between shelf and
boom lands is minimized for heat conduction and function
considerations by small intermittant inserts of teflon 50 in the
groves on the shelf. Furthermore, the instruments on the shelf are
protected from radiant heat from the boom walls by thin half
cylinders of fiber glass epoxy sheet 52 on each side of the shelf.
Holes and windows 53 in the boom wall are required for all
instruments.
Deployment of the boom to the extended position takes place after
separation of the reentry vehicle from the launch vehicle in a near
zero g condition. A small electric motor (not shown) with a
reduction gear drives a cable drum 54 with a wire 56 running from
the drum to the forward end of the boom thus pulling the boom out
to the deployed position. When the boom reaches the fully deployed
position, three spring-loaded locks 58 (FIG. 2) in the forward end
of the boom snap into position in a grove 60 (FIG. 1) in the sleeve
20 forming a position lock. At the same time, two conical shoulders
62 (FIG. 1) on the boom end 27 come to rest against corresponding
shoulders 64 on the inside periphery of the sleeve forming a firm
seat for the boom which is now cantilevered out from the reentry
vehicle. A microswitch (not shown) shuts off the electric motor
drive at the end position.
* * * * *