GB1240890A - Apparatus for determining the position of the centre of gravity and/or the weight of an aircraft - Google Patents
Apparatus for determining the position of the centre of gravity and/or the weight of an aircraftInfo
- Publication number
- GB1240890A GB1240890A GB58145/68A GB5814568A GB1240890A GB 1240890 A GB1240890 A GB 1240890A GB 58145/68 A GB58145/68 A GB 58145/68A GB 5814568 A GB5814568 A GB 5814568A GB 1240890 A GB1240890 A GB 1240890A
- Authority
- GB
- United Kingdom
- Prior art keywords
- load
- centre
- gravity
- determined
- resistance
- 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.)
- Expired
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01G—WEIGHING
- G01G19/00—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups
- G01G19/02—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups for weighing wheeled or rolling bodies, e.g. vehicles
- G01G19/07—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups for weighing wheeled or rolling bodies, e.g. vehicles for weighing aircraft
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M1/00—Testing static or dynamic balance of machines or structures
- G01M1/12—Static balancing; Determining position of centre of gravity
- G01M1/122—Determining position of centre of gravity
- G01M1/125—Determining position of centre of gravity of aircraft
Abstract
1,240,890. Determining weight electrically. VDO LUFTFAHRTGERATE WERK ADOLF SCHINDLING G. m. b. H. Dec.6, 1968, No. 58145/68. Heading G1N. [Also in Division G4] In apparatus for determining the position of the centre of gravity and/or weight of an aircraft supported by its three wheels, a load gauge is provided at each support for converting the load at each support into a respective resistance, the resistances being provided in an analogue circuit. The circuit includes a negative feedback operational amplifier provided with an input resistance and a feedback resistance, which resistances are determined by the value of the resistances given by the load gauges. As shown, the centre of gravity is G 1 and the distance l 3 may be determined by using an analogue circuit in which the feedback resistance R H 2 is given by a load potentiometer at one of the main landing wheels, and the input resistance R H1 + R H2 is given by the series of another load potentiometer at this landing wheel and a load potentiometer at the other main landing wheel. The output voltage U l3 is then proportional to the distance l 3 for a fixed input voltage Ul 4 which is proportional to l 4 , as can be seen by comparison with the corresponding "moments of force" diagram in Fig.5. In a similar manner, the distance l 1 may be determined, Fig.4 (not shown). The total weight of the aircraft is determined by using a series of three load potentiometers i.e. one at each of the wheels, as the feedback resistance, the input resistance being a fixed resistor R. The position of the centre of gravity may be determined from any suitable point of reference. The two measurements of the position of the centre of gravity and the measurement of the total weight may be carried out simultaneously by using three amplifiers and the appropriate number of load gauges or may be carried out consecutively using one amplifier and a relay or electronic switch.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19661506121 DE1506121B2 (en) | 1966-04-30 | 1966-04-30 | On-board device for determining the center of gravity and / or the weight of the aircraft |
GB58145/68A GB1240890A (en) | 1966-04-30 | 1968-12-06 | Apparatus for determining the position of the centre of gravity and/or the weight of an aircraft |
FR177228A FR1594242A (en) | 1966-04-30 | 1968-12-09 |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEV0030961 | 1966-04-30 | ||
GB58145/68A GB1240890A (en) | 1966-04-30 | 1968-12-06 | Apparatus for determining the position of the centre of gravity and/or the weight of an aircraft |
FR177228 | 1968-12-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1240890A true GB1240890A (en) | 1971-07-28 |
Family
ID=27213342
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB58145/68A Expired GB1240890A (en) | 1966-04-30 | 1968-12-06 | Apparatus for determining the position of the centre of gravity and/or the weight of an aircraft |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE1506121B2 (en) |
FR (1) | FR1594242A (en) |
GB (1) | GB1240890A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2065689A1 (en) * | 2007-11-28 | 2009-06-03 | Iveco S.p.A. | Method and device for detecting the overload of a vehicle, in particular a commercial or industrial vehicle |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111207886B (en) * | 2020-01-19 | 2021-09-07 | 南京安科医疗科技有限公司 | Method for testing gravity center of mechanical part |
-
1966
- 1966-04-30 DE DE19661506121 patent/DE1506121B2/en active Pending
-
1968
- 1968-12-06 GB GB58145/68A patent/GB1240890A/en not_active Expired
- 1968-12-09 FR FR177228A patent/FR1594242A/fr not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2065689A1 (en) * | 2007-11-28 | 2009-06-03 | Iveco S.p.A. | Method and device for detecting the overload of a vehicle, in particular a commercial or industrial vehicle |
Also Published As
Publication number | Publication date |
---|---|
DE1506121A1 (en) | 1969-06-04 |
FR1594242A (en) | 1970-06-01 |
DE1506121B2 (en) | 1972-02-24 |
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